- append_restartFalseAppend existing file on restart
Default:False
C++ Type:bool
Controllable:No
Description:Append existing file on restart
- output_fileFalseOutput to the file. The default behavior is to write to file only from the head processor. If "--keep-cout" is passed to the executable, then each processor will write to its own file. The same parallel behaviour can also be achieved by passing "--keep-cout --redirect-stdout" to the executable without setting this parameter to true.
Default:False
C++ Type:bool
Controllable:No
Description:Output to the file. The default behavior is to write to file only from the head processor. If "--keep-cout" is passed to the executable, then each processor will write to its own file. The same parallel behaviour can also be achieved by passing "--keep-cout --redirect-stdout" to the executable without setting this parameter to true.
- output_screenTrueOutput to the screen
Default:True
C++ Type:bool
Controllable:No
Description:Output to the screen
- print_mesh_changed_infoFalseWhen true, each time the mesh is changed the mesh information is printed
Default:False
C++ Type:bool
Controllable:No
Description:When true, each time the mesh is changed the mesh information is printed
- use_displacedFalseEnable/disable the use of the displaced mesh for outputting
Default:False
C++ Type:bool
Controllable:No
Description:Enable/disable the use of the displaced mesh for outputting
Console
The Console object in MOOSE is a buffered ostringstream object that should be used to for all screen based output. Each MooseObject derived class has access to the _console member for screen writing. Output to this object can be controlled in various ways from the [Outputs] block. Information can be disabled, output at a lower frequency, colored, or color removed.
Multiapp Output
When using the MOOSE Multiapp system, Output to the _console object will be automatically indented and labeled according to the multiapp level. This can make it easier to identify where output is coming from in a more complex simulation.
Input Parameters
- additional_execute_onThe list of flag(s) indicating when this object should be executed, the available options include FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM.
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:The list of flag(s) indicating when this object should be executed, the available options include FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM.
- execute_onINITIAL TIMESTEP_BEGIN LINEAR NONLINEAR FAILEDThe list of flag(s) indicating when this object should be executed, the available options include FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM.
Default:INITIAL TIMESTEP_BEGIN LINEAR NONLINEAR FAILED
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:The list of flag(s) indicating when this object should be executed, the available options include FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM.
- output_linearFalseSpecifies whether output occurs on each PETSc linear residual evaluation
Default:False
C++ Type:bool
Controllable:No
Description:Specifies whether output occurs on each PETSc linear residual evaluation
- output_nonlinearFalseSpecifies whether output occurs on each PETSc nonlinear residual evaluation
Default:False
C++ Type:bool
Controllable:No
Description:Specifies whether output occurs on each PETSc nonlinear residual evaluation
Execution Scheduling Parameters
- all_variable_normsFalseIf true, all variable norms will be printed after each solve
Default:False
C++ Type:bool
Controllable:No
Description:If true, all variable norms will be printed after each solve
- outlier_multiplier0.8 2 Multiplier utilized to determine if a residual norm is an outlier. If the variable residual is less than multiplier[0] times the total residual it is colored red. If the variable residual is less than multiplier[1] times the average residual it is colored yellow.
Default:0.8 2
C++ Type:std::vector<double>
Controllable:No
Description:Multiplier utilized to determine if a residual norm is an outlier. If the variable residual is less than multiplier[0] times the total residual it is colored red. If the variable residual is less than multiplier[1] times the average residual it is colored yellow.
- outlier_variable_normsTrueIf true, outlier variable norms will be printed after each solve
Default:True
C++ Type:bool
Controllable:No
Description:If true, outlier variable norms will be printed after each solve
Variable And Residual Norms Parameters
- append_dateFalseWhen true the date and time are appended to the output filename.
Default:False
C++ Type:bool
Controllable:No
Description:When true the date and time are appended to the output filename.
- append_date_formatThe format of the date/time to append, if not given UTC format is used (see http://www.cplusplus.com/reference/ctime/strftime).
C++ Type:std::string
Controllable:No
Description:The format of the date/time to append, if not given UTC format is used (see http://www.cplusplus.com/reference/ctime/strftime).
- file_baseThe desired solution output name without an extension. If not provided, MOOSE sets it with Outputs/file_base when available. Otherwise, MOOSE uses input file name and this object name for a master input or uses master file_base, the subapp name and this object name for a subapp input to set it.
C++ Type:std::string
Controllable:No
Description:The desired solution output name without an extension. If not provided, MOOSE sets it with Outputs/file_base when available. Otherwise, MOOSE uses input file name and this object name for a master input or uses master file_base, the subapp name and this object name for a subapp input to set it.
- output_if_base_containsIf this is supplied then output will only be done in the case that the output base contains one of these strings. This is helpful in outputting only a subset of outputs when using MultiApps.
C++ Type:std::vector<std::string>
Controllable:No
Description:If this is supplied then output will only be done in the case that the output base contains one of these strings. This is helpful in outputting only a subset of outputs when using MultiApps.
- padding4The number of digits for the extension suffix (e.g., out.e-s002)
Default:4
C++ Type:unsigned int
Controllable:No
Description:The number of digits for the extension suffix (e.g., out.e-s002)
File Name Customization Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:Yes
Description:Set the enabled status of the MooseObject.
- show_multiapp_nameFalseIndent multiapp output using the multiapp name
Default:False
C++ Type:bool
Controllable:No
Description:Indent multiapp output using the multiapp name
- system_infoframework mesh aux nonlinear executionList of information types to display ('framework', 'mesh', 'aux', 'nonlinear', 'relationship', 'execution', 'output')
Default:framework mesh aux nonlinear execution
C++ Type:MultiMooseEnum
Options:framework, mesh, aux, nonlinear, relationship, execution, output
Controllable:No
Description:List of information types to display ('framework', 'mesh', 'aux', 'nonlinear', 'relationship', 'execution', 'output')
- verboseFalsePrint detailed diagnostics on timestep calculation
Default:False
C++ Type:bool
Controllable:No
Description:Print detailed diagnostics on timestep calculation
Advanced Parameters
- end_stepTime step at which this output object stop operating
C++ Type:int
Controllable:No
Description:Time step at which this output object stop operating
- end_timeTime at which this output object stop operating
C++ Type:double
Controllable:No
Description:Time at which this output object stop operating
- min_simulation_time_interval0The minimum simulation time between output steps
Default:0
C++ Type:double
Controllable:No
Description:The minimum simulation time between output steps
- simulation_time_interval1.79769e+308The target simulation time interval (in seconds) at which to output
Default:1.79769e+308
C++ Type:double
Controllable:No
Description:The target simulation time interval (in seconds) at which to output
- start_stepTime step at which this output object begins to operate
C++ Type:int
Controllable:No
Description:Time step at which this output object begins to operate
- start_timeTime at which this output object begins to operate
C++ Type:double
Controllable:No
Description:Time at which this output object begins to operate
- sync_onlyFalseOnly export results at sync times
Default:False
C++ Type:bool
Controllable:No
Description:Only export results at sync times
- sync_timesTimes at which the output and solution is forced to occur
C++ Type:std::vector<double>
Controllable:No
Description:Times at which the output and solution is forced to occur
- sync_times_objectTimes object providing the times at which the output and solution is forced to occur
C++ Type:TimesName
Controllable:No
Description:Times object providing the times at which the output and solution is forced to occur
- time_step_interval1The interval (number of time steps) at which output occurs. Unless explicitly set, the default value of this parameter is set to infinity if the wall_time_interval is explicitly set.
Default:1
C++ Type:unsigned int
Controllable:No
Description:The interval (number of time steps) at which output occurs. Unless explicitly set, the default value of this parameter is set to infinity if the wall_time_interval is explicitly set.
- time_tolerance1e-14Time tolerance utilized checking start and end times
Default:1e-14
C++ Type:double
Controllable:No
Description:Time tolerance utilized checking start and end times
- wall_time_interval1.79769e+308The target wall time interval (in seconds) at which to output
Default:1.79769e+308
C++ Type:double
Controllable:No
Description:The target wall time interval (in seconds) at which to output
Timing And Frequency Of Output Parameters
- execute_input_onEnable/disable the output of the input file
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:Enable/disable the output of the input file
- execute_postprocessors_onINITIAL TIMESTEP_ENDControl of when postprocessors are output
Default:INITIAL TIMESTEP_END
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:Control of when postprocessors are output
- execute_reporters_onINITIAL TIMESTEP_ENDControl of when Reporter values are output
Default:INITIAL TIMESTEP_END
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:Control of when Reporter values are output
- execute_scalars_onINITIAL TIMESTEP_ENDControl the output of scalar variables
Default:INITIAL TIMESTEP_END
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:Control the output of scalar variables
- execute_system_information_onINITIALControl when the output of the simulation information occurs
Default:INITIAL
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:Control when the output of the simulation information occurs
- execute_vector_postprocessors_onINITIAL TIMESTEP_ENDEnable/disable the output of VectorPostprocessors
Default:INITIAL TIMESTEP_END
C++ Type:ExecFlagEnum
Options:FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, FAILED, CUSTOM
Controllable:No
Description:Enable/disable the output of VectorPostprocessors
- hideA list of the variables and postprocessors that should NOT be output to the Exodus file (may include Variables, ScalarVariables, and Postprocessor names).
C++ Type:std::vector<VariableName>
Controllable:No
Description:A list of the variables and postprocessors that should NOT be output to the Exodus file (may include Variables, ScalarVariables, and Postprocessor names).
- showA list of the variables and postprocessors that should be output to the Exodus file (may include Variables, ScalarVariables, and Postprocessor names).
C++ Type:std::vector<VariableName>
Controllable:No
Description:A list of the variables and postprocessors that should be output to the Exodus file (may include Variables, ScalarVariables, and Postprocessor names).
Selection/Restriction Of Output Parameters
- fit_modeENVIRONMENTSpecifies the wrapping mode for post-processor tables that are printed to the screen (ENVIRONMENT: Read "MOOSE_PPS_WIDTH" for desired width (if not set, defaults to AUTO), AUTO: Attempt to determine width automatically (serial only),
: Desired width Default:ENVIRONMENT
C++ Type:MooseEnum
Options:ENVIRONMENT, AUTO, 80, 120, 160
Controllable:No
Description:Specifies the wrapping mode for post-processor tables that are printed to the screen (ENVIRONMENT: Read "MOOSE_PPS_WIDTH" for desired width (if not set, defaults to AUTO), AUTO: Attempt to determine width automatically (serial only),
: Desired width - max_rows15The maximum number of postprocessor/scalar values displayed on screen during a timestep (set to 0 for unlimited)
Default:15
C++ Type:unsigned int
Controllable:No
Description:The maximum number of postprocessor/scalar values displayed on screen during a timestep (set to 0 for unlimited)
- new_row_tolerance1e-12The independent variable tolerance for determining when a new row should be added to the table (Note: This value must be set independently for Postprocessor output to type=Console and type=CSV file separately.
Default:1e-12
C++ Type:double
Controllable:No
Description:The independent variable tolerance for determining when a new row should be added to the table (Note: This value must be set independently for Postprocessor output to type=Console and type=CSV file separately.
- time_columnTrueWhether or not the 'time' column should be written for Postprocessor CSV files
Default:True
C++ Type:bool
Controllable:No
Description:Whether or not the 'time' column should be written for Postprocessor CSV files
- time_dataFalseWhen true and VectorPostprocessor data exists, write a csv file containing the timestep and time information.
Default:False
C++ Type:bool
Controllable:No
Description:When true and VectorPostprocessor data exists, write a csv file containing the timestep and time information.
Table Formatting Parameters
- libmesh_logTruePrint the libMesh performance log, requires libMesh to be configured with --enable-perflog
Default:True
C++ Type:bool
Controllable:No
Description:Print the libMesh performance log, requires libMesh to be configured with --enable-perflog
- solve_logFalseToggles the printing of the 'Moose Test Performance' log
Default:False
C++ Type:bool
Controllable:No
Description:Toggles the printing of the 'Moose Test Performance' log
Perf Log Parameters
- linear_residual_dt_divisor1000Number of divisions applied to time step when outputting linear residuals
Default:1000
C++ Type:double
Controllable:No
Description:Number of divisions applied to time step when outputting linear residuals
- linear_residual_end_timeSpecifies an end time to begin output on each linear residual evaluation
C++ Type:double
Controllable:No
Description:Specifies an end time to begin output on each linear residual evaluation
- linear_residual_start_timeSpecifies a start time to begin output on each linear residual evaluation
C++ Type:double
Controllable:No
Description:Specifies a start time to begin output on each linear residual evaluation
- nonlinear_residual_dt_divisor1000Number of divisions applied to time step when outputting non-linear residuals
Default:1000
C++ Type:double
Controllable:No
Description:Number of divisions applied to time step when outputting non-linear residuals
- nonlinear_residual_end_timeSpecifies an end time to begin output on each nonlinear residual evaluation
C++ Type:double
Controllable:No
Description:Specifies an end time to begin output on each nonlinear residual evaluation
- nonlinear_residual_start_timeSpecifies a start time to begin output on each nonlinear residual evaluation
C++ Type:double
Controllable:No
Description:Specifies a start time to begin output on each nonlinear residual evaluation
Petsc Linear/Nonlinear Output Parameters
- postprocessors_as_reportersFalseOutput Postprocessors values as Reporter values.
Default:False
C++ Type:bool
Controllable:No
Description:Output Postprocessors values as Reporter values.
- vectorpostprocessors_as_reportersFalseOutput VectorsPostprocessors vectors as Reporter values.
Default:False
C++ Type:bool
Controllable:No
Description:Output VectorsPostprocessors vectors as Reporter values.
Conversions Before Output Parameters
- scientific_timeFalseControl the printing of time and dt in scientific notation
Default:False
C++ Type:bool
Controllable:No
Description:Control the printing of time and dt in scientific notation
- time_formatplainThe format for the printed times ('dtime' means a format like 1d 01:01:0.1)
Default:plain
C++ Type:MooseEnum
Options:plain, second, minute, hour, day, dtime
Controllable:No
Description:The format for the printed times ('dtime' means a format like 1d 01:01:0.1)
- time_precisionThe number of significant digits that are printed on time related outputs
C++ Type:unsigned int
Controllable:No
Description:The number of significant digits that are printed on time related outputs
Time Output Formatting Parameters
Input Files
- (test/tests/outputs/postprocessor/output_pps_hidden_shown_check.i)
- (modules/contact/test/tests/verification/patch_tests/brick_1/brick1_mu_0_2_pen.i)
- (modules/porous_flow/test/tests/sinks/s08.i)
- (modules/thermal_hydraulics/test/tests/components/heat_transfer_from_heat_structure_1phase/phy.energy_heatstructure_ss_1phase.i)
- (modules/solid_mechanics/test/tests/crystal_plasticity/cp_eigenstrains/thermal_eigenstrain_test.i)
- (test/tests/postprocessors/table_tolerance/table_tolerance_test.i)
- (modules/solid_mechanics/examples/coal_mining/cosserat_elastic.i)
- (test/tests/outputs/console/console_transient.i)
- (modules/xfem/test/tests/moving_interface/moving_level_set.i)
- (modules/richards/test/tests/gravity_head_2/gh18.i)
- (modules/porous_flow/test/tests/sinks/s04.i)
- (modules/xfem/test/tests/mechanical_constraint/glued_penalty.i)
- (modules/xfem/test/tests/corner_nodes_cut/corner_edge_cut.i)
- (test/tests/outputs/console/console_warning.i)
- (modules/contact/test/tests/verification/patch_tests/cyl_4/cyl4_mu_0_2_pen.i)
- (modules/contact/test/tests/verification/patch_tests/ring_2/ring2_template1.i)
- (modules/xfem/test/tests/corner_nodes_cut/corner_node_cut.i)
- (modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1_cycle.i)
- (modules/contact/test/tests/mechanical_constraint/frictionless_penalty.i)
- (modules/contact/test/tests/verification/patch_tests/brick_3/brick3_mu_0_2_pen.i)
- (modules/contact/test/tests/sliding_block/sliding/frictional_04_penalty.i)
- (test/tests/dgkernels/2d_diffusion_dg/no_mallocs_with_action.i)
- (modules/xfem/test/tests/moment_fitting/solid_mechanics_moment_fitting.i)
- (modules/contact/test/tests/verification/patch_tests/ring_2/ring2_template2.i)
- (modules/contact/test/tests/sliding_block/in_and_out/frictionless_kinematic.i)
- (modules/porous_flow/test/tests/sinks/s09.i)
- (modules/solid_mechanics/test/tests/dynamics/linear_constraint/disp_mid.i)
- (modules/xfem/test/tests/solid_mechanics_basic/edge_crack_2d_propagation.i)
- (test/tests/userobjects/toggle_mesh_adaptivity/toggle_mesh_adaptivity_gaussian_ic.i)
- (modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change.i)
- (test/tests/time_integrators/actually_explicit_euler_verification/ee-1d-quadratic-neumann.i)
- (modules/xfem/test/tests/moment_fitting/diffusion_moment_fitting_four_points.i)
- (modules/contact/test/tests/3d-mortar-contact/half_sphere_nodal_geometry.i)
- (modules/contact/test/tests/verification/patch_tests/ring_1/ring1_template1.i)
- (modules/contact/test/tests/pdass_problems/cylinder_friction_penalty.i)
- (modules/xfem/test/tests/moving_interface/moving_bimaterial.i)
- (modules/xfem/test/tests/solid_mechanics_basic/edge_crack_3d.i)
- (modules/contact/test/tests/mechanical_constraint/glued_kinematic.i)
- (modules/porous_flow/test/tests/sinks/s01.i)
- (test/tests/multiapps/picard_multilevel/2level_picard/mutilevel_app.i)
- (test/tests/postprocessors/nodal_var_value/screen_output_test.i)
- (modules/contact/test/tests/verification/patch_tests/ring_1/ring1_template2.i)
- (modules/contact/test/tests/verification/patch_tests/plane_1/plane1_template2.i)
- (test/tests/time_integrators/explicit-euler/ee-2d-linear-adapt.i)
- (modules/xfem/test/tests/corner_nodes_cut/corner_node_cut_twice.i)
- (modules/solid_mechanics/examples/coal_mining/cosserat_mc_wp.i)
- (modules/phase_field/examples/grain_growth/grain_growth_2D_voronoi.i)
- (modules/xfem/test/tests/moving_interface/moving_diffusion.i)
- (modules/heat_transfer/test/tests/gap_heat_transfer_htonly/cyl2D.i)
- (modules/contact/test/tests/verification/patch_tests/brick_1/brick1_aug.i)
- (test/tests/outputs/output_on/postprocessors.i)
- (modules/thermal_hydraulics/test/tests/components/shaft_connected_turbine_1phase/turbine_startup.i)
- (modules/contact/test/tests/verification/patch_tests/ring_4/ring4_template1.i)
- (modules/contact/test/tests/pdass_problems/cylinder_friction.i)
- (modules/porous_flow/test/tests/sinks/s06.i)
- (modules/porous_flow/test/tests/sinks/s07.i)
- (modules/contact/test/tests/verification/hertz_cyl/half_symm_q8/hertz_cyl_half_1deg_template1.i)
- (test/tests/time_integrators/explicit-euler/ee-1d-quadratic-neumann.i)
- (modules/phase_field/tutorials/spinodal_decomposition/s2_fasttest.i)
- (modules/richards/test/tests/gravity_head_1/gh23.i)
- (modules/navier_stokes/test/tests/finite_element/pins/channel-flow/pm_reverse_flow.i)
- (modules/thermal_hydraulics/tutorials/single_phase_flow/03_upper_loop.i)
- (test/tests/time_integrators/explicit-euler/ee-1d-linear.i)
- (test/tests/postprocessors/pps_interval/pps_bad_interval2.i)
- (modules/contact/test/tests/verification/patch_tests/plane_3/plane3_template2.i)
- (modules/heat_transfer/test/tests/gap_heat_transfer_htonly/sphere3D.i)
- (modules/xfem/test/tests/solid_mechanics_basic/test.i)
- (modules/contact/test/tests/verification/patch_tests/ring_3/ring3_template2.i)
- (modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d_frictional.i)
- (modules/contact/test/tests/verification/patch_tests/brick_1/brick1_template1.i)
- (test/tests/transfers/multiapp_conservative_transfer/sub_nearest_point.i)
- (test/tests/fvkernels/fv_adapt/steady-adapt.i)
- (modules/thermal_hydraulics/test/tests/components/heat_transfer_from_heat_flux_1phase/phy.energy_heatflux_ss_1phase.i)
- (modules/thermal_hydraulics/tutorials/single_phase_flow/04_loop.i)
- (modules/thermal_hydraulics/tutorials/single_phase_flow/05_secondary_side.i)
- (modules/xfem/test/tests/moving_interface/verification/1D_xy_discrete2mat.i)
- (modules/xfem/test/tests/corner_nodes_cut/notch.i)
- (modules/contact/test/tests/verification/patch_tests/brick_3/brick3_template2.i)
- (modules/xfem/test/tests/single_var_constraint_2d/stationary_jump.i)
- (modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d.i)
- (modules/porous_flow/test/tests/sinks/s09_fully_saturated.i)
- (modules/xfem/test/tests/diffusion_xfem/levelsetcut3d.i)
- (test/tests/outputs/console/console_print_toggles.i)
- (modules/contact/test/tests/fieldsplit/2blocks3d.i)
- (modules/porous_flow/test/tests/sinks/s03.i)
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Child Objects
References
No citations exist within this document.(test/tests/outputs/postprocessor/output_pps_hidden_shown_check.i)
# Computing two postprocessors and specifying one of them both in the
# show list and the hide list, which should throw an error message.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./lr_u]
type = DirichletBC
variable = u
boundary = '1 3'
value = 1
[../]
[]
[Postprocessors]
[./elem_56]
type = ElementalVariableValue
variable = u
elementid = 56
[../]
[./elem_12]
type = ElementalVariableValue
variable = u
elementid = 12
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
[./console]
type = Console
show = 'elem_56'
hide = 'elem_56'
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_1/brick1_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick1_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[./tang_force_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x8]
type = NodalVariableValue
nodeid = 7
variable = disp_x
[../]
[./disp_x13]
type = NodalVariableValue
nodeid = 12
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y8]
type = NodalVariableValue
nodeid = 7
variable = disp_y
[../]
[./disp_y13]
type = NodalVariableValue
nodeid = 12
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
file_base = brick1_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = brick1_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x5 disp_x8 disp_x13 disp_x16 disp_y5 disp_y8 disp_y13 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/porous_flow/test/tests/sinks/s08.i)
# apply a sink flux on just one component of a 3-component, 2-phase system and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pwater frac_ph0_c0 pgas'
number_fluid_phases = 2
number_fluid_components = 3
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1.1
[]
[]
[Variables]
[pwater]
[]
[frac_ph0_c0]
initial_condition = 0.3
[]
[pgas]
[]
[]
[ICs]
[pwater]
type = FunctionIC
variable = pwater
function = y
[]
[pgas]
type = FunctionIC
variable = pgas
function = y+3
[]
[]
[Kernels]
[mass_c0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = frac_ph0_c0
[]
[mass_c1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = pwater
[]
[mass_c2]
type = PorousFlowMassTimeDerivative
fluid_component = 2
variable = pgas
[]
[]
[FluidProperties]
[simple_fluid0]
type = SimpleFluidProperties
bulk_modulus = 2.3
density0 = 1.5
thermal_expansion = 0
viscosity = 2.1
[]
[simple_fluid1]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow2PhasePP
phase0_porepressure = pwater
phase1_porepressure = pgas
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = 'frac_ph0_c0 frac_ph0_c1 frac_ph1_c0 frac_ph1_c1'
[]
[simple_fluid0]
type = PorousFlowSingleComponentFluid
fp = simple_fluid0
phase = 0
[]
[simple_fluid1]
type = PorousFlowSingleComponentFluid
fp = simple_fluid1
phase = 1
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.2 0 0 0 0.1 0 0 0 0.1'
[]
[relperm0]
type = PorousFlowRelativePermeabilityCorey
n = 1
phase = 0
[]
[relperm1]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 1
[]
[]
[AuxVariables]
[flux_out]
[]
[frac_ph0_c1]
initial_condition = 0.35
[]
[frac_ph1_c0]
initial_condition = 0.1
[]
[frac_ph1_c1]
initial_condition = 0.8
[]
[]
[Functions]
[mass1_00]
type = ParsedFunction
expression = 'fgas*vol*por*dens0gas*exp(pgas/bulkgas)*(1-pow(1+pow(al*(pgas-pwater),1.0/(1-m)),-m))+fwater*vol*por*dens0water*exp(pwater/bulkwater)*(pow(1+pow(al*(pgas-pwater),1.0/(1-m)),-m))'
symbol_names = 'vol por dens0gas pgas pwater bulkgas al m dens0water bulkwater fgas fwater'
symbol_values = '0.25 0.1 1.1 pgas_00 pwater_00 1.3 1.1 0.5 1.5 2.3 frac_ph1_c1_00 frac_ph0_c1_00'
[]
[expected_mass_change1_00]
type = ParsedFunction
expression = 'frac*fcn*area*dt*pow(1-pow(1+pow(al*(pgas-pwater),1.0/(1-m)),-m), 2)'
symbol_names = 'frac fcn area dt pgas pwater al m'
symbol_values = 'frac_ph1_c1_00 100 0.5 1E-3 pgas_00 pwater_00 1.1 0.5'
[]
[mass1_00_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm1_00_prev del_m1_00'
[]
[]
[Postprocessors]
[total_mass_comp0]
type = PorousFlowFluidMass
fluid_component = 0
[]
[total_mass_comp1]
type = PorousFlowFluidMass
fluid_component = 1
[]
[total_mass_comp2]
type = PorousFlowFluidMass
fluid_component = 2
[]
[frac_ph1_c1_00]
type = PointValue
point = '0 0 0'
variable = frac_ph1_c1
execute_on = 'initial timestep_end'
[]
[frac_ph0_c1_00]
type = PointValue
point = '0 0 0'
variable = frac_ph0_c1
execute_on = 'initial timestep_end'
[]
[flux_00]
type = PointValue
point = '0 0 0'
variable = flux_out
execute_on = 'initial timestep_end'
[]
[pgas_00]
type = PointValue
point = '0 0 0'
variable = pgas
execute_on = 'initial timestep_end'
[]
[pwater_00]
type = PointValue
point = '0 0 0'
variable = pwater
execute_on = 'initial timestep_end'
[]
[m1_00]
type = FunctionValuePostprocessor
function = mass1_00
execute_on = 'initial timestep_end'
[]
[m1_00_prev]
type = FunctionValuePostprocessor
function = mass1_00
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m1_00]
type = FunctionValuePostprocessor
function = expected_mass_change1_00
execute_on = 'timestep_end'
outputs = 'console'
[]
[m1_00_expect]
type = FunctionValuePostprocessor
function = mass1_00_expect
execute_on = 'timestep_end'
[]
[]
[BCs]
[flux_ph1_c1]
type = PorousFlowSink
boundary = 'left'
variable = pwater # sink applied to the mass_c1 Kernel
use_mobility = false
use_relperm = true
mass_fraction_component = 1
fluid_phase = 1
flux_function = 100
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 100 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-3
end_time = 0.01
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s08
exodus = true
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
execute_on = 'timestep_end'
[]
[]
(modules/thermal_hydraulics/test/tests/components/heat_transfer_from_heat_structure_1phase/phy.energy_heatstructure_ss_1phase.i)
# This test tests conservation of energy at steady state for 1-phase flow when a
# heat structure is used. Conservation is checked by comparing the integral of
# the heat flux against the difference of the boundary fluxes.
[GlobalParams]
initial_p = 7.0e6
initial_vel = 0
initial_T = 513
gravity_vector = '0.0 0.0 0.0'
scaling_factor_1phase = '1 1 1e-4'
closures = simple_closures
[]
[FluidProperties]
[eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[SolidProperties]
[fuel-mat]
type = ThermalFunctionSolidProperties
k = 3.7
cp = 3.e2
rho = 10.42e3
[]
[gap-mat]
type = ThermalFunctionSolidProperties
k = 0.7
cp = 5e3
rho = 1.0
[]
[clad-mat]
type = ThermalFunctionSolidProperties
k = 16
cp = 356.
rho = 6.551400E+03
[]
[]
[Components]
[reactor]
type = TotalPower
power = 1e3
[]
[core:pipe]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 3.66
n_elems = 10
A = 1.907720E-04
D_h = 1.698566E-02
f = 0.0
fp = eos
[]
[core:solid]
type = HeatStructureCylindrical
position = '0 -0.0071501 0'
orientation = '0 0 1'
length = 3.66
n_elems = 10
names = 'FUEL GAP CLAD'
widths = '6.057900E-03 1.524000E-04 9.398000E-04'
n_part_elems = '5 1 2'
solid_properties = 'fuel-mat gap-mat clad-mat'
solid_properties_T_ref = '300 300 300'
initial_T = 513
[]
[core:hgen]
type = HeatSourceFromTotalPower
hs = core:solid
regions = 'FUEL'
power = reactor
power_fraction = 1
[]
[core:hx]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core:pipe
hs = core:solid
hs_side = outer
Hw = 1.0e4
P_hf = 4.4925e-2
[]
[inlet]
type = InletDensityVelocity1Phase
input = 'core:pipe:in'
rho = 817.382210128610836
vel = 2.4
[]
[outlet]
type = Outlet1Phase
input = 'core:pipe:out'
p = 7e6
[]
[]
[Postprocessors]
[E_in]
type = ADFlowBoundaryFlux1Phase
boundary = inlet
equation = energy
execute_on = 'initial timestep_end'
[]
[E_out]
type = ADFlowBoundaryFlux1Phase
boundary = outlet
equation = energy
execute_on = 'initial timestep_end'
[]
[hf_pipe]
type = ADHeatRateConvection1Phase
block = core:pipe
T_wall = T_wall
T = T
Hw = Hw
P_hf = P_hf
execute_on = 'initial timestep_end'
[]
[E_diff]
type = DifferencePostprocessor
value1 = E_in
value2 = E_out
execute_on = 'initial timestep_end'
[]
[E_conservation]
type = SumPostprocessor
values = 'E_diff hf_pipe'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
abort_on_solve_fail = true
dt = 5
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 50
l_tol = 1e-3
l_max_its = 60
start_time = 0
end_time = 260
[]
[Outputs]
[out]
type = CSV
execute_on = final
show = 'E_conservation'
[]
[console]
type = Console
show = 'E_conservation'
[]
[]
(modules/solid_mechanics/test/tests/crystal_plasticity/cp_eigenstrains/thermal_eigenstrain_test.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
elem_type = HEX8
[]
[AuxVariables]
[temperature]
order = FIRST
family = LAGRANGE
[]
[eth_xx]
order = CONSTANT
family = MONOMIAL
[]
[eth_yy]
order = CONSTANT
family = MONOMIAL
[]
[eth_zz]
order = CONSTANT
family = MONOMIAL
[]
[fth_xx]
order = CONSTANT
family = MONOMIAL
[]
[fth_yy]
order = CONSTANT
family = MONOMIAL
[]
[fth_zz]
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic/all]
strain = FINITE
incremental = true
add_variables = true
generate_output = stress_zz
[]
[AuxKernels]
[temperature]
type = FunctionAux
variable = temperature
function = '300+400*t' # temperature increases at a constant rate
execute_on = timestep_begin
[]
[eth_xx]
type = RankTwoAux
variable = eth_xx
rank_two_tensor = thermal_eigenstrain
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[eth_yy]
type = RankTwoAux
variable = eth_yy
rank_two_tensor = thermal_eigenstrain
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[eth_zz]
type = RankTwoAux
variable = eth_zz
rank_two_tensor = thermal_eigenstrain
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[fth_xx]
type = RankTwoAux
variable = fth_xx
rank_two_tensor = thermal_deformation_gradient
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[fth_yy]
type = RankTwoAux
variable = fth_yy
rank_two_tensor = thermal_deformation_gradient
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[fth_zz]
type = RankTwoAux
variable = fth_zz
rank_two_tensor = thermal_deformation_gradient
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[tdisp]
type = DirichletBC
variable = disp_z
boundary = front
value = 0
[]
[]
[Materials]
[elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '1.684e5 1.214e5 1.214e5 1.684e5 1.214e5 1.684e5 0.754e5 0.754e5 0.754e5'
fill_method = symmetric9
[]
[stress]
type = ComputeMultipleCrystalPlasticityStress
crystal_plasticity_models = 'trial_xtalpl'
eigenstrain_names = thermal_eigenstrain
tan_mod_type = exact
maximum_substep_iteration = 5
[]
[trial_xtalpl]
type = CrystalPlasticityKalidindiUpdate
number_slip_systems = 12
slip_sys_file_name = input_slip_sys.txt
[]
[thermal_eigenstrain]
type = ComputeCrystalPlasticityThermalEigenstrain
eigenstrain_name = thermal_eigenstrain
deformation_gradient_name = thermal_deformation_gradient
temperature = temperature
thermal_expansion_coefficients = '1e-05 2e-05 4e-05' # thermal expansion coefficients along three directions
[]
[]
[Postprocessors]
[stress_zz]
type = ElementAverageValue
variable = stress_zz
[]
[eth_xx]
type = ElementAverageValue
variable = eth_xx
[]
[eth_yy]
type = ElementAverageValue
variable = eth_yy
[]
[eth_zz]
type = ElementAverageValue
variable = eth_zz
[]
[fth_xx]
type = ElementAverageValue
variable = fth_xx
[]
[fth_yy]
type = ElementAverageValue
variable = fth_yy
[]
[fth_zz]
type = ElementAverageValue
variable = fth_zz
[]
[temperature]
type = ElementAverageValue
variable = temperature
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-10
nl_abs_step_tol = 1e-10
dt = 0.1
dtmin = 1e-4
end_time = 10
[]
[Outputs]
csv = true
[console]
type = Console
max_rows = 5
[]
[]
(test/tests/postprocessors/table_tolerance/table_tolerance_test.i)
# This test verifies that the row tolerance for outputting and displaying postprocessors
# can be controlled via the new_row_tolerance parameter. Normally new rows are only added
# if they are above a given tolerance.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[AuxVariables]
[./aux]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./func]
type = FunctionAux
function = 'sin(x + 1e12*t)'
variable = aux
execute_on = timestep_begin
[../]
[]
[Executioner]
type = Transient
num_steps = 20
# Very small timestep size
dt = 1e-13
dtmin = 1e-13
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[./integral]
type = ElementIntegralVariablePostprocessor
variable = aux
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Outputs]
exodus = false
[./out]
type = CSV
new_row_tolerance = 1e-14
[../]
[./console]
type = Console
new_row_tolerance = 1e-14
[../]
[]
(modules/solid_mechanics/examples/coal_mining/cosserat_elastic.i)
# Strata deformation and fracturing around a coal mine
#
# A 2D geometry is used that simulates a transverse section of
# the coal mine. The model is actually 3D, but the "x"
# dimension is only 10m long, meshed with 1 element, and
# there is no "x" displacement. The mine is 400m deep
# and just the roof is studied (0<=z<=400). The model sits
# between 0<=y<=450. The excavation sits in 0<=y<=150. This
# is a "half model": the boundary conditions are such that
# the model simulates an excavation sitting in -150<=y<=150
# inside a model of the region -450<=y<=450. The
# excavation height is 3m (ie, the excavation lies within
# 0<=z<=3).
#
# Time is meaningless in this example
# as quasi-static solutions are sought at each timestep, but
# the number of timesteps controls the resolution of the
# process.
#
# The boundary conditions for this elastic simulation are:
# - disp_x = 0 everywhere
# - disp_y = 0 at y=0 and y=450
# - disp_z = 0 for y>150
# - wc_x = 0 at y=0 and y=450.
# That is, rollers on the sides, free at top,
# and prescribed at bottom in the unexcavated portion.
#
# The small strain formulation is used.
#
# All stresses are measured in MPa. The initial stress is consistent with
# the weight force from density 2500 kg/m^3, ie, stress_zz = -0.025*(300-z) MPa
# where gravity = 10 m.s^-2 = 1E-5 MPa m^2/kg. The maximum and minimum
# principal horizontal stresses are assumed to be equal to 0.8*stress_zz.
#
# This is an elastic simulation, but the weak-plane and Drucker-Prager
# parameters and AuxVariables may be found below. They are irrelevant
# in this simulation. The weak-plane and Drucker-Prager cohesions,
# tensile strengths and compressive strengths have been set very high
#
# Material properties:
# Young's modulus = 8 GPa
# Poisson's ratio = 0.25
# Cosserat layer thickness = 1 m
# Cosserat-joint normal stiffness = large
# Cosserat-joint shear stiffness = 1 GPa
#
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
xmin = -5
xmax = 5
nz = 40
zmin = 0
zmax = 403.003
bias_z = 1.1
ny = 30 # make this a multiple of 3, so y=150 is at a node
ymin = 0
ymax = 450
[]
[left]
type = SideSetsAroundSubdomainGenerator
new_boundary = 11
normal = '0 -1 0'
input = generated_mesh
[]
[right]
type = SideSetsAroundSubdomainGenerator
new_boundary = 12
normal = '0 1 0'
input = left
[]
[front]
type = SideSetsAroundSubdomainGenerator
new_boundary = 13
normal = '-1 0 0'
input = right
[]
[back]
type = SideSetsAroundSubdomainGenerator
new_boundary = 14
normal = '1 0 0'
input = front
[]
[top]
type = SideSetsAroundSubdomainGenerator
new_boundary = 15
normal = '0 0 1'
input = back
[]
[bottom]
type = SideSetsAroundSubdomainGenerator
new_boundary = 16
normal = '0 0 -1'
input = top
[]
[excav]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-5 0 0'
top_right = '5 150 3'
input = bottom
[]
[roof]
type = SideSetsBetweenSubdomainsGenerator
new_boundary = 21
primary_block = 0
paired_block = 1
input = excav
[]
[hole]
type = BlockDeletionGenerator
block = 1
input = roof
[]
[]
[GlobalParams]
block = 0
perform_finite_strain_rotations = false
displacements = 'disp_x disp_y disp_z'
Cosserat_rotations = 'wc_x wc_y wc_z'
[]
[Variables]
[./disp_y]
[../]
[./disp_z]
[../]
[./wc_x]
[../]
[]
[Kernels]
[./cy_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_y
component = 1
[../]
[./cz_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_z
component = 2
[../]
[./x_couple]
type = StressDivergenceTensors
use_displaced_mesh = false
variable = wc_x
displacements = 'wc_x wc_y wc_z'
component = 0
base_name = couple
[../]
[./x_moment]
type = MomentBalancing
use_displaced_mesh = false
variable = wc_x
component = 0
[../]
[./gravity]
type = Gravity
use_displaced_mesh = false
variable = disp_z
value = -10E-6 # remember this is in MPa
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./wc_y]
[../]
[./wc_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./stress_xz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xz
index_i = 0
index_j = 2
[../]
[./stress_yx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yx
index_i = 1
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yz
index_i = 1
index_j = 2
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zx
index_i = 2
index_j = 0
[../]
[./stress_zy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zy
index_i = 2
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./dp_shear]
type = MaterialStdVectorAux
index = 0
property = dp_plastic_internal_parameter
variable = dp_shear
[../]
[./dp_tensile]
type = MaterialStdVectorAux
index = 1
property = dp_plastic_internal_parameter
variable = dp_tensile
[../]
[./wp_shear]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_internal_parameter
variable = wp_shear
[../]
[./wp_tensile]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_internal_parameter
variable = wp_tensile
[../]
[./dp_shear_f]
type = MaterialStdVectorAux
index = 0
property = dp_plastic_yield_function
variable = dp_shear_f
[../]
[./dp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = dp_plastic_yield_function
variable = dp_tensile_f
[../]
[./wp_shear_f]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_yield_function
variable = wp_shear_f
[../]
[./wp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_yield_function
variable = wp_tensile_f
[../]
[]
[BCs]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '11 12'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '16'
value = 0.0
[../]
[./no_wc_x]
type = DirichletBC
variable = wc_x
boundary = '11 12'
value = 0.0
[../]
[]
[Functions]
[./ini_xx]
type = ParsedFunction
expression = '-0.8*2500*10E-6*(403.003-z)'
[../]
[./ini_zz]
type = ParsedFunction
expression = '-2500*10E-6*(403.003-z)'
[../]
[]
[UserObjects]
[./dp_coh_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 2.9 # MPa
value_residual = 3.1 # MPa
rate = 1.0
[../]
[./dp_fric]
type = SolidMechanicsHardeningConstant
value = 0.65 # 37deg
[../]
[./dp_dil]
type = SolidMechanicsHardeningConstant
value = 0.65
[../]
[./dp_tensile_str_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 1.0 # MPa
value_residual = 1.4 # MPa
rate = 1.0
[../]
[./dp_compressive_str]
type = SolidMechanicsHardeningConstant
value = 1.0E3 # Large!
[../]
[./drucker_prager_model]
type = SolidMechanicsPlasticDruckerPrager
mc_cohesion = dp_coh_strong_harden
mc_friction_angle = dp_fric
mc_dilation_angle = dp_dil
internal_constraint_tolerance = 1 # irrelevant here
yield_function_tolerance = 1 # irrelevant here
[../]
[./wp_coh]
type = SolidMechanicsHardeningConstant
value = 1E12
[../]
[./wp_tan_fric]
type = SolidMechanicsHardeningConstant
value = 0.36 # 20deg
[../]
[./wp_tan_dil]
type = SolidMechanicsHardeningConstant
value = 0.18 # 10deg
[../]
[./wp_tensile_str]
type = SolidMechanicsHardeningConstant
value = 1E12
[../]
[./wp_compressive_str]
type = SolidMechanicsHardeningConstant
value = 1E12
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeLayeredCosseratElasticityTensor
young = 8E3 # MPa
poisson = 0.25
layer_thickness = 1.0
joint_normal_stiffness = 1E9 # huge
joint_shear_stiffness = 1E3 # MPa
[../]
[./strain]
type = ComputeCosseratIncrementalSmallStrain
eigenstrain_names = ini_stress
[../]
[./ini_stress]
type = ComputeEigenstrainFromInitialStress
initial_stress = 'ini_xx 0 0 0 ini_xx 0 0 0 ini_zz'
eigenstrain_name = ini_stress
[../]
[./stress]
# this is needed so as to correctly apply the initial stress
type = ComputeMultipleInelasticCosseratStress
block = 0
inelastic_models = ''
relative_tolerance = 2.0
absolute_tolerance = 1E6
max_iterations = 1
tangent_operator = nonlinear
perform_finite_strain_rotations = false
[../]
[./dp]
type = CappedDruckerPragerCosseratStressUpdate
block = 0
warn_about_precision_loss = false
host_youngs_modulus = 8E3
host_poissons_ratio = 0.25
base_name = dp
DP_model = drucker_prager_model
tensile_strength = dp_tensile_str_strong_harden
compressive_strength = dp_compressive_str
max_NR_iterations = 100000
tip_smoother = 0.1E1
smoothing_tol = 0.1E1 # MPa # Must be linked to cohesion
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0
[../]
[./wp]
type = CappedWeakPlaneCosseratStressUpdate
block = 0
warn_about_precision_loss = false
base_name = wp
cohesion = wp_coh
tan_friction_angle = wp_tan_fric
tan_dilation_angle = wp_tan_dil
tensile_strength = wp_tensile_str
compressive_strength = wp_compressive_str
max_NR_iterations = 10000
tip_smoother = 0.1
smoothing_tol = 0.1 # MPa # Note, this must be tied to cohesion, otherwise get no possible return at cone apex
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0E-3
[../]
[./density]
type = GenericConstantMaterial
prop_names = density
prop_values = 2500
[../]
[]
[Postprocessors]
[./subs_max]
type = PointValue
point = '0 0 403.003'
variable = disp_z
use_displaced_mesh = false
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'Linear'
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
line_search = bt
nl_abs_tol = 1e-3
nl_rel_tol = 1e-5
l_max_its = 30
nl_max_its = 1000
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
file_base = cosserat_elastic
time_step_interval = 1
print_linear_residuals = false
exodus = true
csv = true
console = true
#[./console]
# type = Console
# output_linear = false
#[../]
[]
(test/tests/outputs/console/console_transient.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
start_time = -1
end_time = 0
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
verbose = true
[]
[Outputs]
execute_on = 'timestep_end'
[./screen]
type = Console
verbose = true
time_precision = 6
execute_on = 'failed nonlinear linear timestep_begin timestep_end'
[../]
[]
(modules/xfem/test/tests/moving_interface/moving_level_set.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutSetUserObject
cut_data = '0.3 1.0 0.3 0.2 0 3'
heal_always = false
[../]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[./ls_func]
type = ParsedFunction
expression = 'x-0.7-0.07*(t-1)'
[../]
[]
[Constraints]
[./u_constraint]
type = XFEMSingleVariableConstraint
geometric_cut_userobject = 'level_set_cut_uo'
use_displaced_mesh = false
variable = u
use_penalty = true
alpha = 1e5
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-9
start_time = 0.0
dt = 1
end_time = 3.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/richards/test/tests/gravity_head_2/gh18.i)
# with immobile saturation
# unsaturated = true
# gravity = true
# supg = true
# transient = true
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmin = 0
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1E-2 1E-1 1E0 0.5E1 0.5E2 0.4E4 1E5 1E6 1E7'
x = '0 1E-1 1E0 1E1 1E2 1E3 1E4 1E5 1E6'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E2
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 0.5
bulk_mod = 0.5E2
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.4
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.3
n = 2
[../]
[./SatWater]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.15
[../]
[./SatGas]
type = RichardsSat
s_res = 0.05
sum_s_res = 0.15
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 1
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2
variable = pgas
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas'
[./richardstwater]
type = RichardsMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxVariables]
[./seffgas]
[../]
[./seffwater]
[../]
[]
[AuxKernels]
[./seffgas_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffGas
variable = seffgas
[../]
[./seffwater_kernel]
type = RichardsSeffAux
pressure_vars = 'pwater pgas'
seff_UO = SeffWater
variable = seffwater
[../]
[]
[Postprocessors]
[./mwater_init]
type = RichardsMass
variable = pwater
execute_on = timestep_begin
outputs = none
[../]
[./mgas_init]
type = RichardsMass
variable = pgas
execute_on = timestep_begin
outputs = none
[../]
[./mwater_fin]
type = RichardsMass
variable = pwater
execute_on = timestep_end
outputs = none
[../]
[./mgas_fin]
type = RichardsMass
variable = pgas
execute_on = timestep_end
outputs = none
[../]
[./mass_error_water]
type = FunctionValuePostprocessor
function = fcn_mass_error_w
[../]
[./mass_error_gas]
type = FunctionValuePostprocessor
function = fcn_mass_error_g
[../]
[./pw_left]
type = PointValue
point = '0 0 0'
variable = pwater
outputs = none
[../]
[./pw_right]
type = PointValue
point = '1 0 0'
variable = pwater
outputs = none
[../]
[./error_water]
type = FunctionValuePostprocessor
function = fcn_error_water
[../]
[./pg_left]
type = PointValue
point = '0 0 0'
variable = pgas
outputs = none
[../]
[./pg_right]
type = PointValue
point = '1 0 0'
variable = pgas
outputs = none
[../]
[./error_gas]
type = FunctionValuePostprocessor
function = fcn_error_gas
[../]
[]
[Functions]
[./fcn_mass_error_w]
type = ParsedFunction
expression = 'abs(0.5*(mi-mf)/(mi+mf))'
symbol_names = 'mi mf'
symbol_values = 'mwater_init mwater_fin'
[../]
[./fcn_mass_error_g]
type = ParsedFunction
expression = 'abs(0.5*(mi-mf)/(mi+mf))'
symbol_names = 'mi mf'
symbol_values = 'mgas_init mgas_fin'
[../]
[./fcn_error_water]
type = ParsedFunction
expression = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
symbol_names = 'b gdens0 p0 xval p1'
symbol_values = '1E2 -1 pw_left 1 pw_right'
[../]
[./fcn_error_gas]
type = ParsedFunction
expression = 'abs((-b*log(-(gdens0*xval+(-b*exp(-p0/b)))/b)-p1)/p1)'
symbol_names = 'b gdens0 p0 xval p1'
symbol_values = '0.5E2 -0.5 pg_left 1 pg_right'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
viscosity = '1E-3 0.5E-3'
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-10 1E-10 10'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
end_time = 1E6
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh18
execute_on = 'timestep_end final'
time_step_interval = 100000
exodus = true
[./console]
type = Console
time_step_interval = 1
[../]
[]
(modules/porous_flow/test/tests/sinks/s04.i)
# apply a piecewise-linear sink flux and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = y+1
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[xval]
[]
[yval]
[]
[pt_shift]
initial_condition = 0.3
[]
[]
[ICs]
[xval]
type = FunctionIC
variable = xval
function = x
[]
[yval]
type = FunctionIC
variable = yval
function = y
[]
[]
[Functions]
[mass10]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)'
symbol_names = 'vol por dens0 pp bulk'
symbol_values = '0.25 0.1 1.1 p10 1.3'
[]
[rate10]
type = ParsedFunction
expression = 'fcn*if(pp>0.8,1,if(pp<0.3,0.5,0.2+pp))'
symbol_names = 'fcn pp'
symbol_values = '8 p10'
[]
[mass10_expect]
type = ParsedFunction
expression = 'mass_prev-rate*area*dt'
symbol_names = 'mass_prev rate area dt'
symbol_values = 'm10_prev m10_rate 0.5 1E-3'
[]
[mass11]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)'
symbol_names = 'vol por dens0 pp bulk'
symbol_values = '0.25 0.1 1.1 p11 1.3'
[]
[rate11]
type = ParsedFunction
expression = 'fcn*if(pp>0.8,1,if(pp<0.3,0.5,0.2+pp))'
symbol_names = 'fcn pp'
symbol_values = '8 p11'
[]
[mass11_expect]
type = ParsedFunction
expression = 'mass_prev-rate*area*dt'
symbol_names = 'mass_prev rate area dt'
symbol_values = 'm11_prev m11_rate 0.5 1E-3'
[]
[]
[Postprocessors]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p10]
type = PointValue
point = '1 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m10]
type = FunctionValuePostprocessor
function = mass10
execute_on = 'initial timestep_end'
[]
[m10_prev]
type = FunctionValuePostprocessor
function = mass10
execute_on = 'timestep_begin'
outputs = 'console'
[]
[m10_rate]
type = FunctionValuePostprocessor
function = rate10
execute_on = 'timestep_end'
[]
[m10_expect]
type = FunctionValuePostprocessor
function = mass10_expect
execute_on = 'timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m11]
type = FunctionValuePostprocessor
function = mass11
execute_on = 'initial timestep_end'
[]
[m11_prev]
type = FunctionValuePostprocessor
function = mass11
execute_on = 'timestep_begin'
outputs = 'console'
[]
[m11_rate]
type = FunctionValuePostprocessor
function = rate11
execute_on = 'timestep_end'
[]
[m11_expect]
type = FunctionValuePostprocessor
function = mass11_expect
execute_on = 'timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowPiecewiseLinearSink
boundary = 'right'
PT_shift = pt_shift
pt_vals = '0.0 0.5'
multipliers = '0.5 1'
variable = pp
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 8
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-3
end_time = 1E-2
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s04
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
execute_on = 'timestep_end'
[]
[]
(modules/xfem/test/tests/mechanical_constraint/glued_penalty.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.0 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50 100'
y='0 0.02 0.1'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Constraints]
[./disp_x]
type = XFEMSingleVariableConstraint
variable = disp_x
use_penalty = true
alpha = 1.0e8
use_displaced_mesh = true
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[./disp_y]
type = XFEMSingleVariableConstraint
variable = disp_y
use_penalty = true
alpha = 1.0e8
use_displaced_mesh = true
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 0
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 5000
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/corner_nodes_cut/corner_edge_cut.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo1]
type = LineSegmentCutUserObject
cut_data = '-0.0 0.5 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./line_seg_cut_uo2]
type = LineSegmentCutUserObject
cut_data = '0.5 0.5 1.0 0.7'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[BCs]
[./top_x]
type = DirichletBC
boundary = 2
variable = disp_x
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.1
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = -0.1
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/outputs/console/console_warning.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./screen]
type = Console
[../]
[./screen2]
type = Console
[../]
[./screen3]
type = Console
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_4/cyl4_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl4_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = cyl4_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = cyl4_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_2/ring2_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring2_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/xfem/test/tests/corner_nodes_cut/corner_node_cut.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.5 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[BCs]
[./top_x]
type = DirichletBC
boundary = 2
variable = disp_x
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.1
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# max_xfem_update = 1
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1_cycle.i)
#
# Test for effective strain calculation.
# Boundary conditions from NAFEMS test NL1
#
#
# This is not a verification test. The boundary conditions are applied such
# that the first step generates only elastic stresses. The rest of the load
# steps generate cycles of tension and compression in the axial (i.e., y-axis)
# direction. The axial stresses and strains also cycle, however the effective
# plastic strain increases in value throughout the analysis.
#
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = one_elem2.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./eff_plastic_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
execute_on = timestep_end
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain_zz]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./plastic_strain_xx]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./plastic_strain_yy]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./plastic_strain_zz]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./tot_strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./tot_strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./eff_plastic_strain]
type = MaterialRealAux
property = effective_plastic_strain
variable = eff_plastic_strain
[../]
[]
[Functions]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 12.0'
y = '0.0 0.208e-4 0.50e-4 1.00e-4 0.784e-4 0.50e-4 0.0 0.216e-4 0.5e-4 1.0e-4 0.785e-4 0.50e-4 0.0'
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
block = 1
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 5e6
hardening_constant = 0.0
relative_tolerance = 1e-20
absolute_tolerance = 1e-8
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
dt = 1.0
start_time = 0.0
num_steps = 100
end_time = 12.0
[]
[Postprocessors]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./stress_xy]
type = ElementAverageValue
variable = stress_xy
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./el_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./el_strain_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[./pl_strain_xx]
type = ElementAverageValue
variable = plastic_strain_xx
[../]
[./pl_strain_yy]
type = ElementAverageValue
variable = plastic_strain_yy
[../]
[./pl_strain_zz]
type = ElementAverageValue
variable = plastic_strain_zz
[../]
[./eff_plastic_strain]
type = ElementAverageValue
variable = eff_plastic_strain
[../]
[./tot_strain_xx]
type = ElementAverageValue
variable = tot_strain_xx
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./tot_strain_zz]
type = ElementAverageValue
variable = tot_strain_zz
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/mechanical_constraint/frictionless_penalty.i)
[Mesh]
file = blocks_2d.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
#Initial gap is 0.01
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e7
poissons_ratio = 0.3
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.10
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = frictionless
formulation = penalty
penalty = 1e+7
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_3/brick3_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick3_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[./tang_force_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x28]
type = NodalVariableValue
nodeid = 27
variable = disp_x
[../]
[./disp_x33]
type = NodalVariableValue
nodeid = 32
variable = disp_x
[../]
[./disp_y28]
type = NodalVariableValue
nodeid = 27
variable = disp_y
[../]
[./disp_y33]
type = NodalVariableValue
nodeid = 32
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
file_base = brick3_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = brick3_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x28 disp_y28 disp_x33 disp_y33 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+6
[../]
[]
(modules/contact/test/tests/sliding_block/sliding/frictional_04_penalty.i)
# This is a benchmark test that checks constraint based frictional
# contact using the penalty method. In this test a constant
# displacement is applied in the horizontal direction to simulate
# a small block come sliding down a larger block.
#
# A friction coefficient of 0.4 is used. The gold file is run on one processor
# and the benchmark case is run on a minimum of 4 processors to ensure no
# parallel variability in the contact pressure and penetration results.
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[penetration]
[]
[inc_slip_x]
[]
[inc_slip_y]
[]
[accum_slip_x]
[]
[accum_slip_y]
[]
[]
[Functions]
[vertical_movement]
type = ParsedFunction
expression = -t
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
[]
[]
[AuxKernels]
[zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[]
[accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[]
[penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[]
[]
[Postprocessors]
[nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[]
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[]
[]
[BCs]
[left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[]
[left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[]
[right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[]
[]
[Materials]
[left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 14.99999
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Outputs]
time_step_interval = 10
[out]
type = Exodus
elemental_as_nodal = true
[]
[console]
type = Console
max_rows = 5
[]
[]
[Contact]
[leftright]
secondary = 3
primary = 2
model = coulomb
penalty = 1e+6
friction_coefficient = 0.4
formulation = penalty
normal_smoothing_distance = 0.1
[]
[]
(test/tests/dgkernels/2d_diffusion_dg/no_mallocs_with_action.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[AuxVariables]
[v]
order = FIRST
family = MONOMIAL
[]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
expression = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
expression = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGDiffusionAction]
variable = u
epsilon = -1
sigma = 6
# We couple in an auxiliary variable in order to ensure that we've properly
# ghosted both non-linear and auxiliary solution vectors
coupled_var = v
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Postprocessors]
active = 'num_rm'
[num_rm]
type = NumRelationshipManagers
[]
[num_internal_sides]
type = NumInternalSides
[]
[]
(modules/xfem/test/tests/moment_fitting/solid_mechanics_moment_fitting.i)
# Test for a mechanics problem which uses four points moment_fitting approach.
# See this paper (https://doi.org/10.1007/s00466-018-1544-2) for more details about moment_fitting approach.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo0]
type = LineSegmentCutUserObject
cut_data = '0.0000e+00 6.3330e-01 3.9000e-01 6.3330e-01'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./line_seg_cut_uo1]
type = LineSegmentCutUserObject
cut_data = '3.9000e-01 6.3330e-01 6.8000e-01 6.3330e-01'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[Functions]
[./right_trac_x]
type = ParsedFunction
expression = '-(t*M*y)/I'
symbol_names = 'M E I'
symbol_values = '2e4 1e6 0.666666667'
[../]
[./bottom_disp_y]
type = ParsedFunction
expression = '((t*M)/(2*E*I))*(1-nu*nu)*(x*x-0.25*l*l)'
symbol_names = 'M E I l nu'
symbol_values = '2e4 1e6 0.666666667 2.0 0.3'
[../]
[./soln_x]
type = ParsedFunction
expression = '-(M/(E*I))*(1-nu*nu)*x*y'
symbol_names = 'M E I nu'
symbol_values = '2e4 1e6 0.666666667 0.3'
[../]
[./soln_y]
type = ParsedFunction
expression = '(M/(2*E*I))*(1-nu*nu)*(x*x-0.25*l*l+(nu/(1-nu))*y*y)'
symbol_names = 'M E I l nu'
symbol_values = '2e4 1e6 0.666666667 2.0 0.3'
[../]
[]
[BCs]
[./right_x]
type = FunctionNeumannBC
boundary = 1
variable = disp_x
function = right_trac_x
[../]
[./bottom_y]
type = FunctionDirichletBC
boundary = 0
variable = disp_y
function = bottom_disp_y
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
# [./Quadrature]
# order = FOURTH
# type = MONOMIAL
# [../]
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 0.5
end_time = 1.0
num_steps = 5000
[]
[Postprocessors]
[./numel]
type = NumElems
execute_on = timestep_end
[../]
[./integral]
type = ElementVectorL2Error
var_x = disp_x
var_y = disp_y
function_x = soln_x
function_y = soln_y
execute_on = timestep_end
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_2/ring2_template2.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring2_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/contact/test/tests/sliding_block/in_and_out/frictionless_kinematic.i)
# This is a benchmark test that checks constraint based frictionless
# contact using the kinematic method. In this test a sinusoidal
# displacement is applied in the horizontal direction to simulate
# a small block come in and out of contact as it slides down a larger block.
#
# The sinusoid is of the form 0.4sin(4t)+0.2. The gold file is run
# on one processor and the benchmark
# case is run on a minimum of 4 processors to ensure no parallel variability
# in the contact pressure and penetration results. Further documentation can
# found in moose/modules/contact/doc/sliding_block/
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[./horizontal_movement]
type = ParsedFunction
expression = -0.04*sin(4*t)+0.02
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 20 101'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
time_step_interval = 10
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = frictionless
penalty = 1e+6
normal_smoothing_distance = 0.1
[../]
[]
(modules/porous_flow/test/tests/sinks/s09.i)
# Apply a piecewise-linear sink flux to the right-hand side and watch fluid flow to it
#
# This test has a single phase with two components. The test initialises with
# the porous material fully filled with component=1. The left-hand side is fixed
# at porepressure=1 and mass-fraction of the zeroth component being unity.
# The right-hand side has a very strong piecewise-linear flux that keeps the
# porepressure~0 at that side. Fluid mass is extracted by this flux in proportion
# to the fluid component mass fraction.
#
# Therefore, the zeroth fluid component will flow from left to right (down the
# pressure gradient).
#
# The important DE is
# porosity * dc/dt = (perm / visc) * grad(P) * grad(c)
# which is true for c = mass-fraction, and very large bulk modulus of the fluid.
# For grad(P) constant in time and space (as in this example) this is just the
# advection equation for c, with velocity = perm / visc / porosity. The parameters
# are chosen to velocity = 1 m/s.
# In the numerical world, and especially with full upwinding, the advection equation
# suffers from diffusion. In this example, the diffusion is obvious when plotting
# the mass-fraction along the line, but the average velocity of the front is still
# correct at 1 m/s.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = 0
xmax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp frac'
number_fluid_phases = 1
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Variables]
[pp]
[]
[frac]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = 1-x
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = frac
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = pp
[]
[flux0]
type = PorousFlowAdvectiveFlux
fluid_component = 0
gravity = '0 0 0'
variable = frac
[]
[flux1]
type = PorousFlowAdvectiveFlux
fluid_component = 1
gravity = '0 0 0'
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e10 # need large in order for constant-velocity advection
density0 = 1 # almost irrelevant, except that the ability of the right BC to keep P fixed at zero is related to density_P0
thermal_expansion = 0
viscosity = 11
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = frac
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.1 0 0 0 1.1 0 0 0 1.1'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2 # irrelevant in this fully-saturated situation
phase = 0
[]
[]
[BCs]
[lhs_fixed_a]
type = DirichletBC
boundary = 'left'
variable = frac
value = 1
[]
[lhs_fixed_b]
type = DirichletBC
boundary = 'left'
variable = pp
value = 1
[]
[flux0]
type = PorousFlowPiecewiseLinearSink
boundary = 'right'
pt_vals = '-100 100'
multipliers = '-1 1'
variable = frac # the zeroth comonent
mass_fraction_component = 0
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1E4
[]
[flux1]
type = PorousFlowPiecewiseLinearSink
boundary = 'right'
pt_vals = '-100 100'
multipliers = '-1 1'
variable = pp # comonent 1
mass_fraction_component = 1
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1E4
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-2
end_time = 1
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[VectorPostprocessors]
[mf]
type = LineValueSampler
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 100
sort_by = x
variable = frac
[]
[]
[Outputs]
file_base = s09
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
sync_times = '0.1 0.5 1'
sync_only = true
[]
time_step_interval = 10
[]
(modules/solid_mechanics/test/tests/dynamics/linear_constraint/disp_mid.i)
# Constraining secondary nodes to move a linear combination of primary nodes
#
# The test consists of a 2D rectangular block divided into two Quad elements
# (along its height) which have different material properties.
# A displacement of 2 m is applied to the top surface of the block in x direction and the
# bottom surface is held fixed.
# The nodes of the interface between the two elements will tend to move as
# dictated by the material models of the two elements.
# LinearNodalConstraint forces the interface nodes to move as a linear combination
# of the nodes on the top and bottom of the block.
# primary node ids and the corresponding weights are taken as input by the LinearNodalConstraint
# along with the secondary node set or secondary node ids.
# The constraint can be applied using either penalty or kinematic formulation.
# In this example, the final x displacement of the top surface is 2m and bottom surface is 0m.
# Therefore, the final x displacement of the interface nodes would be 0.25*top+0.75*bottom = 0.5m
[Mesh]
file=rect_mid.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Kernels]
[SolidMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[BCs]
[./top_2x]
type = DirichletBC
variable = disp_x
boundary = 10
value = 2.0
[../]
[./top_2y]
type = DirichletBC
variable = disp_y
boundary = 10
value = 0.0
[../]
[./bottom_1]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./bottom_2]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[]
[Materials]
[./Elasticity_tensor_1]
type = ComputeElasticityTensor
block = 1
fill_method = 'symmetric_isotropic'
C_ijkl = '400. 200.'
[../]
[./strain_1]
type = ComputeSmallStrain
block = 1
displacements = 'disp_x disp_y'
[../]
[./stress_1]
type = ComputeLinearElasticStress
block = 1
[../]
[./density_1]
type = GenericConstantMaterial
block = 1
prop_names = 'density'
prop_values = '10.'
[../]
[./Elasticity_tensor_2]
type = ComputeElasticityTensor
block = 2
fill_method = 'symmetric_isotropic'
C_ijkl = '1000. 500.'
[../]
[./strain_2]
type = ComputeSmallStrain
block = 2
displacements = 'disp_x disp_y'
[../]
[./stress_2]
type = ComputeLinearElasticStress
block = 2
[../]
[./density_2]
type = GenericConstantMaterial
block = 2
prop_names = 'density'
prop_values = '10.'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = ''
petsc_options_value = ''
line_search = 'none'
[]
[Constraints]
[./disp_x_1]
type = LinearNodalConstraint
variable = disp_x
primary = '0 5'
weights = '0.25 0.75'
# secondary_node_set = '2'
secondary_node_ids = '2 3'
penalty = 1e8
formulation = kinematic
[../]
[./disp_y_1]
type = LinearNodalConstraint
variable = disp_y
primary = '0 5'
weights = '0.25 0.75'
# secondary_node_set = '2'
secondary_node_ids = '2 3'
penalty = 1e8
formulation = kinematic
[../]
[]
[Postprocessors]
[./_dt]
type = TimestepSize
[../]
[./disp_1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_3]
type = NodalVariableValue
nodeid = 2
variable = disp_x
[../]
[./disp_4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_6]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/edge_crack_2d_propagation.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
[block]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[]
[UserObjects]
[./cut_mesh]
type = MeshCut2DFunctionUserObject
mesh_file = 2D_edge_crack.e
growth_direction_x = growth_func_x
growth_direction_y = growth_func_y
growth_rate = growth_func_v
[../]
[]
[Functions]
[./growth_func_x]
type = ParsedFunction
expression = 0.4*t
[../]
[./growth_func_y]
type = ParsedFunction
expression = 1.8*(t-1)
[../]
[./growth_func_v]
type = ParsedFunction
expression = 0.1*t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
generate_output = 'stress_xx stress_yy vonmises_stress'
[../]
[]
[Functions]
[./top_trac_y]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_y]
type = FunctionNeumannBC
boundary = top
variable = disp_y
function = top_trac_y
[../]
[./bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
max_xfem_update = 2
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[xfemcutter]
type=XFEMCutMeshOutput
xfem_cutter_uo=cut_mesh
[]
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/userobjects/toggle_mesh_adaptivity/toggle_mesh_adaptivity_gaussian_ic.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./gaussian_ic]
type = FunctionIC
variable = u
function = gaussian_2d
[../]
[]
[Functions]
[./gaussian_2d]
type = ParsedFunction
expression = exp(-((x-x0)*(x-x0)+(y-y0)*(y-y0))/2.0/sigma/sigma)
symbol_names = 'sigma x0 y0'
symbol_values = '0.05 0.35 0.25'
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.02
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Transient
num_steps = 4
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
initial_steps = 1
initial_marker = marker
cycles_per_step = 1
marker = marker
max_h_level = 2
[./Markers]
[./marker]
type = CircleMarker
point = '0.35 0.25 0'
radius = 0.2
inside = refine
outside = coarsen
[../]
[../]
[]
[UserObjects]
[./mesh_adaptivity_off]
type = ToggleMeshAdaptivity
mesh_adaptivity = 'off'
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
order = FIRST
family = LAGRANGE
block = 1
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
x = '0 1e6 2e6 2.001e6 2.002e6'
y = '0 3e8 3e8 12e8 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 300.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
volumetric_locking_correction = true
incremental = true
eigenstrain_names = thermal_expansion
decomposition_method = EigenSolution
add_variables = true
generate_output = 'vonmises_stress'
temperature = temp
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
start_time = 0.0
num_steps = 50000
end_time = 2.002e6
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e7
dt = 1e6
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[]
(test/tests/time_integrators/actually_explicit_euler_verification/ee-1d-quadratic-neumann.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 10
elem_type = EDGE3
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = x*x-2*t+t*x*x
[../]
[./exact_fn]
type = ParsedFunction
expression = t*x*x
[../]
[./left_bc_fn]
type = ParsedFunction
expression = -t*2*x
[../]
[./right_bc_fn]
type = ParsedFunction
expression = t*2*x
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./td]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./abs]
type = Reaction
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./left]
type = FunctionNeumannBC
variable = u
boundary = '0'
function = left_bc_fn
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = '1'
function = right_bc_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
l_tol = 1e-12
start_time = 0.0
num_steps = 10
dt = 0.001
[./TimeIntegrator]
type = ActuallyExplicitEuler
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/xfem/test/tests/moment_fitting/diffusion_moment_fitting_four_points.i)
# Test for a diffusion problem which uses four points moment_fitting approach.
# See this paper (https://doi.org/10.1007/s00466-018-1544-2) for more details about moment_fitting approach.
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/3d-mortar-contact/half_sphere_nodal_geometry.i)
[Mesh]
[generated_mesh]
type = FileMeshGenerator
file = half_sphere.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 2002
new_block_name = 'secondary_lower'
sidesets = '202'
input = generated_mesh
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 1002
sidesets = '102'
new_block_name = 'primary_lower'
input = secondary
[]
patch_size = 20
patch_update_strategy = always
uniform_refine = 0
[]
[Problem]
kernel_coverage_check = false
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
order = FIRST
family = LAGRANGE
[]
[Variables]
[frictional_normal_lm]
block = 'secondary_lower'
use_dual = true
[]
[frictional_tangential_lm]
block = 'secondary_lower'
use_dual = true
[]
[frictional_tangential_dir_lm]
block = 'secondary_lower'
use_dual = true
[]
[]
[AuxVariables]
[saved_x]
[]
[saved_y]
[]
[saved_z]
[]
[tangent_x]
family = LAGRANGE
order = FIRST
[]
[tangent_y]
family = LAGRANGE
order = FIRST
[]
[tangent_z]
family = LAGRANGE
order = FIRST
[]
[]
[AuxKernels]
[friction_x_component]
type = MortarFrictionalPressureVectorAux
primary_boundary = 102
secondary_boundary = 202
tangent_one = frictional_tangential_lm
tangent_two = frictional_tangential_dir_lm
variable = tangent_x
component = 0
boundary = 202
[]
[friction_y_component]
type = MortarFrictionalPressureVectorAux
primary_boundary = 102
secondary_boundary = 202
tangent_one = frictional_tangential_lm
tangent_two = frictional_tangential_dir_lm
variable = tangent_y
component = 1
boundary = 202
[]
[friction_z_component]
type = MortarFrictionalPressureVectorAux
primary_boundary = 102
secondary_boundary = 202
tangent_one = frictional_tangential_lm
tangent_two = frictional_tangential_dir_lm
variable = tangent_z
component = 2
boundary = 202
[]
[]
[Functions]
[push_down]
type = ParsedFunction
expression = 'if(t < 1.5, -t, t-3.0)'
[]
[force_z]
type = ParsedFunction
expression = 'if(t < 0.008, 0.0, (-t)*2.0e2 -t*t*100.0)' # 4.0e5
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
block = '1 2'
use_automatic_differentiation = true
generate_output = 'stress_xx stress_xy stress_xz stress_yy stress_zz'
save_in = 'saved_x saved_y saved_z'
use_finite_deform_jacobian = true
[]
[]
[BCs]
[botz]
type = ADDirichletBC
variable = disp_z
boundary = 101
value = 0.0
[]
[boty]
type = ADDirichletBC
variable = disp_y
boundary = 101
value = 0.0
[]
[botx]
type = ADDirichletBC
variable = disp_x
boundary = 101
value = 0.0
[]
[topz]
type = ADFunctionDirichletBC
variable = disp_z
boundary = '201'
function = push_down
[]
[topy]
type = ADDirichletBC
variable = disp_y
boundary = '201 202'
value = 0.0
[]
[topx]
type = ADDirichletBC
variable = disp_x
boundary = '201 202'
value = 0.0
[]
[]
[Materials]
[tensor]
type = ADComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.40625e7
poissons_ratio = 0.25
[]
[stress]
type = ADComputeFiniteStrainElasticStress
block = '1'
[]
[tensor_1000]
type = ADComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e5
poissons_ratio = 0.0
[]
[stress_1000]
type = ADComputeFiniteStrainElasticStress
block = '2'
[]
[]
[Postprocessors]
[stress_zz]
type = ElementAverageValue
variable = stress_zz
block = 1
[]
[resid_z]
type = NodalSum
variable = saved_z
boundary = 201
[]
[disp_z]
type = NodalExtremeValue
variable = disp_z
boundary = 201
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -pc_factor_shift_type '
'-pc_factor_shift_amount -mat_mffd_err'
petsc_options_value = 'lu superlu_dist nonzero 1e-14 1e-5'
line_search = 'none'
l_max_its = 60
nl_max_its = 50
dt = 0.004
dtmin = 0.00001
# end_time = 1.8
end_time = 0.000
nl_rel_tol = 1.0e-6 #1e-7 # -8, -6 to avoid many iterations. Switch it March 2021
nl_abs_tol = 1e-6 # 6 if no friction
l_tol = 1e-4
[]
[Outputs]
exodus = true
csv = true
print_linear_residuals = true
perf_graph = true
[console]
type = Console
max_rows = 5
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[UserObjects]
[weighted_vel_uo]
type = LMWeightedVelocitiesUserObject
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
lm_variable_normal = frictional_normal_lm
lm_variable_tangential_one = frictional_tangential_lm
lm_variable_tangential_two = frictional_tangential_dir_lm
secondary_variable = disp_x
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
debug_mesh = true
[]
[]
[Constraints]
[weighted_gap_lm]
type = ComputeFrictionalForceLMMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_normal_lm
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
use_displaced_mesh = true
friction_lm = frictional_tangential_lm
friction_lm_dir = frictional_tangential_dir_lm
c = 7.0e4
c_t = 7.0e4
mu = 0.4
debug_mesh = true
weighted_gap_uo = weighted_vel_uo
weighted_velocities_uo = weighted_vel_uo
[]
[normal_x]
type = NormalMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_normal_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_gap_uo = weighted_vel_uo
[]
[normal_y]
type = NormalMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_normal_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_gap_uo = weighted_vel_uo
[]
[normal_z]
type = NormalMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_normal_lm
secondary_variable = disp_z
component = z
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_gap_uo = weighted_vel_uo
[]
[tangential_x]
type = TangentialMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_tangential_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_y]
type = TangentialMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_tangential_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_z]
type = TangentialMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_tangential_lm
secondary_variable = disp_z
component = z
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_x_dir]
type = TangentialMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_tangential_dir_lm
secondary_variable = disp_x
component = x
direction = direction_2
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_y_dir]
type = TangentialMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_tangential_dir_lm
secondary_variable = disp_y
component = y
direction = direction_2
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_z_dir]
type = TangentialMortarMechanicalContact
primary_boundary = 102
secondary_boundary = 202
primary_subdomain = 1002
secondary_subdomain = 2002
variable = frictional_tangential_dir_lm
secondary_variable = disp_z
component = z
direction = direction_2
use_displaced_mesh = true
compute_lm_residuals = false
debug_mesh = true
weighted_velocities_uo = weighted_vel_uo
[]
[]
[Debug]
show_var_residual_norms = true
[]
(modules/contact/test/tests/verification/patch_tests/ring_1/ring1_template1.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring1_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/pdass_problems/cylinder_friction_penalty.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '3'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '2'
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[penalty_normal_pressure]
order = FIRST
family = LAGRANGE
[]
[penalty_frictional_pressure]
order = FIRST
family = LAGRANGE
[]
[accumulated_slip_one]
order = FIRST
family = LAGRANGE
[]
[tangential_vel_one]
order = FIRST
family = LAGRANGE
[]
[weighted_gap]
order = FIRST
family = LAGRANGE
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[react_x]
[]
[react_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
[]
[]
[AuxKernels]
[penalty_normal_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_normal_pressure
user_object = friction_uo
contact_quantity = normal_pressure
[]
[penalty_frictional_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_frictional_pressure
user_object = friction_uo
contact_quantity = tangential_pressure_one
[]
[penalty_accumulated_slip_auxk]
type = PenaltyMortarUserObjectAux
variable = accumulated_slip_one
user_object = friction_uo
contact_quantity = accumulated_slip_one
[]
[penalty_tangential_vel_auxk]
type = PenaltyMortarUserObjectAux
variable = tangential_vel_one
user_object = friction_uo
contact_quantity = tangential_velocity_one
[]
[penalty_weighted_gap_auxk]
type = PenaltyMortarUserObjectAux
variable = weighted_gap
user_object = friction_uo
contact_quantity = normal_gap
[]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[react_x]
type = TagVectorAux
vector_tag = 'ref'
v = 'disp_x'
variable = 'react_x'
[]
[react_y]
type = TagVectorAux
vector_tag = 'ref'
v = 'disp_y'
variable = 'react_y'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = react_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = react_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = react_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = react_y
boundary = 4
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '2 3 4 5 6 7'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type '
'-pc_factor_shift_amount -mat_mffd_err'
petsc_options_value = 'lu superlu_dist NONZERO 1e-15 '
' 1e-5'
line_search = 'none'
nl_abs_tol = 1e-14
nl_rel_tol = 1e-10
start_time = 0.0
end_time = 0.3 # 3.5
l_tol = 1e-4
dt = 0.1
dtmin = 0.001
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3'
sort_by = id
[]
[y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3'
sort_by = id
[]
[cont_press]
type = NodalValueSampler
variable = penalty_normal_pressure
boundary = '3'
sort_by = id
[]
[friction]
type = NodalValueSampler
variable = penalty_frictional_pressure
boundary = '3'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = false
[console]
type = Console
max_rows = 5
[]
[chkfile]
type = CSV
show = 'x_disp y_disp cont_press friction'
file_base = cylinder_friction_penalty_check
create_final_symlink = true
execute_on = 'FINAL'
[]
[]
[UserObjects]
[friction_uo]
type = PenaltyFrictionUserObject
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
disp_x = disp_x
disp_y = disp_y
friction_coefficient = 0.4 # with 2.0 works
secondary_variable = disp_x
penalty = 5e9
penalty_friction = 1e7
[]
[]
[Constraints]
[x]
type = NormalMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[tangential_x]
type = TangentialMortarMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[tangential_y]
type = TangentialMortarMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[]
(modules/xfem/test/tests/moving_interface/moving_bimaterial.i)
# This test is for two layer materials with different youngs modulus
# The global stress is determined by switching the stress based on level set values
# The material interface is marked by a level set function
# The two layer materials are glued together
# This case is also meant to test for a bug in moving interfaces on displaced meshes
# It should fail during the healing step of the 2nd timestep if the bug is present.
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Mesh]
displacements = 'disp_x disp_y'
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
[]
[./left_bottom]
type = ExtraNodesetGenerator
new_boundary = 'left_bottom'
coord = '0.0 0.0'
input = generated_mesh
[../]
[./left_top]
type = ExtraNodesetGenerator
new_boundary = 'left_top'
coord = '0.0 5.'
input = left_bottom
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'y-3.153 + t'
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./a_strain_xx]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
boundary = top
variable = disp_x
function = 0.03*t
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ComputeSmallStrain
base_name = A
displacements = 'disp_x disp_y'
[../]
[./stress_A]
type = ComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e7
poissons_ratio = 0.3
[../]
[./strain_B]
type = ComputeSmallStrain
base_name = B
displacements = 'disp_x disp_y'
[../]
[./stress_B]
type = ComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = LevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[./combined_dstressdstrain]
type = LevelSetBiMaterialRankFour
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = Jacobian_mult
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'bt'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 0.15
num_steps = 3
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/edge_crack_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX8
[]
[UserObjects]
[./square_cut_uo]
type = RectangleCutUserObject
cut_data = ' -0.001 0.5 -0.001
0.401 0.5 -0.001
0.401 0.5 0.201
-0.001 0.5 0.201'
[../]
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[DomainIntegral]
integrals = 'Jintegral InteractionIntegralKI'
crack_front_points = '0.4 0.5 0.0
0.4 0.5 0.1
0.4 0.5 0.2'
crack_direction_method = CrackDirectionVector
crack_direction_vector = '1 0 0'
radius_inner = '0.2'
radius_outer = '0.4'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
incremental = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 0
[../]
[]
[Functions]
[./top_trac_y]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_y]
type = FunctionNeumannBC
boundary = top
variable = disp_y
function = top_trac_y
[../]
[./bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
file_base = edge_crack_3d_out
execute_on = 'timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/mechanical_constraint/glued_kinematic.i)
[Mesh]
file = blocks_2d_nogap.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
#Initial gap is 0.01
value = -0.01
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e7
poissons_ratio = 0.3
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.10
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = glued
penalty = 1e+6
[../]
[]
(modules/porous_flow/test/tests/sinks/s01.i)
# apply a sink flux and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = y+1
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[xval]
[]
[yval]
[]
[]
[ICs]
[xval]
type = FunctionIC
variable = xval
function = x
[]
[yval]
type = FunctionIC
variable = yval
function = y
[]
[]
[Functions]
[mass00]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)'
symbol_names = 'vol por dens0 pp bulk'
symbol_values = '0.25 0.1 1.1 p00 1.3'
[]
[mass01]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)'
symbol_names = 'vol por dens0 pp bulk'
symbol_values = '0.25 0.1 1.1 p01 1.3'
[]
[expected_mass_change00]
type = ParsedFunction
expression = 'fcn*perm*dens0*exp(pp/bulk)/visc*area*dt'
symbol_names = 'fcn perm dens0 pp bulk visc area dt'
symbol_values = '6 1 1 0 1.3 1 0.5 1E-3'
[]
[]
[Postprocessors]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m00]
type = FunctionValuePostprocessor
function = mass00
execute_on = 'initial timestep_end'
[]
[del_m00]
type = FunctionValuePostprocessor
function = expected_mass_change00
execute_on = 'timestep_end'
[]
[p10]
type = PointValue
point = '1 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m01]
type = FunctionValuePostprocessor
function = mass01
execute_on = 'initial timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowSink
boundary = 'left'
variable = pp
use_mobility = false
use_relperm = true
fluid_phase = 0
flux_function = 6
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-3
end_time = 1E-2
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s01
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
execute_on = 'initial timestep_end'
[]
[]
(test/tests/multiapps/picard_multilevel/2level_picard/mutilevel_app.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[v]
initial_condition = 50
[]
[]
[Kernels]
[diffusion]
type = Diffusion
variable = u
[]
[source]
type = CoupledForce
variable = u
v = v
[]
[]
[BCs]
[dirichlet0]
type = DirichletBC
variable = u
boundary = '3'
value = 0
[]
[dirichlet]
type = DirichletBC
variable = u
boundary = '1'
value = 100
[]
[]
[Postprocessors]
[avg_u]
type = ElementAverageValue
variable = u
execute_on = 'initial timestep_begin timestep_end'
[]
[avg_v]
type = ElementAverageValue
variable = v
execute_on = 'initial timestep_begin timestep_end'
[]
[]
[Executioner]
type = Steady
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
fixed_point_rel_tol = 1E-3
fixed_point_abs_tol = 1.0e-05
fixed_point_max_its = 2
accept_on_max_fixed_point_iteration = true
[]
[MultiApps]
[level1-]
type = FullSolveMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_level1.i
execute_on = 'timestep_end'
keep_solution_during_restore = true
[]
[]
[Transfers]
[u_to_sub]
type = MultiAppGeneralFieldShapeEvaluationTransfer
source_variable = u
variable = u
to_multi_app = level1-
execute_on = 'timestep_end'
[]
[v_from_sub]
type = MultiAppGeneralFieldShapeEvaluationTransfer
source_variable = v
variable = v
from_multi_app = level1-
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
perf_graph = true
[screen]
type = Console
execute_postprocessors_on = "timestep_end timestep_begin"
[]
[]
(test/tests/postprocessors/nodal_var_value/screen_output_test.i)
[Mesh]
file = square-2x2-nodeids.e
# This test can only be run with renumering disabled, so the
# NodalVariableValue postprocessor's node id is well-defined.
allow_renumbering = false
[]
[Variables]
active = 'u v'
[./u]
order = SECOND
family = LAGRANGE
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Functions]
active = 'force_fn exact_fn left_bc'
[./force_fn]
type = ParsedFunction
expression = '1-x*x+2*t'
[../]
[./exact_fn]
type = ParsedFunction
expression = '(1-x*x)*t'
[../]
[./left_bc]
type = ParsedFunction
expression = t
[../]
[]
[Kernels]
active = '
time_u diff_u ffn_u
time_v diff_v'
[./time_u]
type = TimeDerivative
variable = u
[../]
[./diff_u]
type = Diffusion
variable = u
[../]
[./ffn_u]
type = BodyForce
variable = u
function = force_fn
[../]
[./time_v]
type = TimeDerivative
variable = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'all_u left_v right_v'
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = exact_fn
[../]
[./left_v]
type = FunctionDirichletBC
variable = v
boundary = '3'
function = left_bc
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = '2'
value = 0
[../]
[]
[Postprocessors]
active = 'l2 node1 node4'
[./l2]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[./node1]
type = NodalVariableValue
variable = u
nodeid = 15
[../]
[./node4]
type = NodalVariableValue
variable = v
nodeid = 10
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
dt = 0.1
start_time = 0
end_time = 1
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[./console]
type = Console
max_rows = 2
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_1/ring1_template2.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring1_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-8
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_1/plane1_template2.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane1_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 200
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(test/tests/time_integrators/explicit-euler/ee-2d-linear-adapt.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = (x+y)
[../]
[./exact_fn]
type = ParsedFunction
expression = t*(x+y)
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
lumping = true
implicit = true
[../]
[./diff]
type = Diffusion
variable = u
implicit = false
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
implicit = false
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
implicit = true
[../]
[]
[Adaptivity]
steps = 1
marker = box
max_h_level = 2
[./Markers]
[./box]
bottom_left = '-0.4 -0.4 0'
inside = refine
top_right = '0.4 0.4 0'
outside = do_nothing
type = BoxMarker
[../]
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
scheme = 'explicit-euler'
start_time = 0.0
num_steps = 4
dt = 0.005
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/xfem/test/tests/corner_nodes_cut/corner_node_cut_twice.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '-0.0 0.3 1.0 0.7'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[BCs]
[./top_x]
type = DirichletBC
boundary = 2
variable = disp_x
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.1
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = -0.1
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/solid_mechanics/examples/coal_mining/cosserat_mc_wp.i)
# Strata deformation and fracturing around a coal mine
#
# A 2D geometry is used that simulates a transverse section of
# the coal mine. The model is actually 3D, but the "x"
# dimension is only 10m long, meshed with 1 element, and
# there is no "x" displacement. The mine is 300m deep
# and just the roof is studied (0<=z<=300). The model sits
# between 0<=y<=450. The excavation sits in 0<=y<=150. This
# is a "half model": the boundary conditions are such that
# the model simulates an excavation sitting in -150<=y<=150
# inside a model of the region -450<=y<=450. The
# excavation height is 3m (ie, the excavation lies within
# 0<=z<=3). Mining is simulated by moving the excavation's
# roof down, until disp_z=-3 at t=1.
# Time is meaningless in this example
# as quasi-static solutions are sought at each timestep, but
# the number of timesteps controls the resolution of the
# process.
#
# The boundary conditions are:
# - disp_x = 0 everywhere
# - disp_y = 0 at y=0 and y=450
# - disp_z = 0 for y>150
# - disp_z = -3 at maximum, for 0<=y<=150. See excav function.
# That is, rollers on the sides, free at top, and prescribed at bottom.
#
# The small strain formulation is used.
#
# All stresses are measured in MPa. The initial stress is consistent with
# the weight force from density 2500 kg/m^3, ie, stress_zz = -0.025*(300-z) MPa
# where gravity = 10 m.s^-2 = 1E-5 MPa m^2/kg. The maximum and minimum
# principal horizontal stresses are assumed to be equal to 0.8*stress_zz.
#
# Material properties:
# Young's modulus = 8 GPa
# Poisson's ratio = 0.25
# Cosserat layer thickness = 1 m
# Cosserat-joint normal stiffness = large
# Cosserat-joint shear stiffness = 1 GPa
# MC cohesion = 3 MPa
# MC friction angle = 37 deg
# MC dilation angle = 8 deg
# MC tensile strength = 1 MPa
# MC compressive strength = 100 MPa, varying down to 1 MPa when tensile strain = 1
# WeakPlane cohesion = 0.1 MPa
# WeakPlane friction angle = 30 deg
# WeakPlane dilation angle = 10 deg
# WeakPlane tensile strength = 0.1 MPa
# WeakPlane compressive strength = 100 MPa softening to 1 MPa at strain = 1
#
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
xmin = -5
xmax = 5
nz = 40
zmin = 0
zmax = 400.0
bias_z = 1.1
ny = 30 # make this a multiple of 3, so y=150 is at a node
ymin = 0
ymax = 450
[]
[left]
type = SideSetsAroundSubdomainGenerator
new_boundary = 11
normal = '0 -1 0'
input = generated_mesh
[]
[right]
type = SideSetsAroundSubdomainGenerator
new_boundary = 12
normal = '0 1 0'
input = left
[]
[front]
type = SideSetsAroundSubdomainGenerator
new_boundary = 13
normal = '-1 0 0'
input = right
[]
[back]
type = SideSetsAroundSubdomainGenerator
new_boundary = 14
normal = '1 0 0'
input = front
[]
[top]
type = SideSetsAroundSubdomainGenerator
new_boundary = 15
normal = '0 0 1'
input = back
[]
[bottom]
type = SideSetsAroundSubdomainGenerator
new_boundary = 16
normal = '0 0 -1'
input = top
[]
[excav]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-5 0 0'
top_right = '5 150 3'
input = bottom
[]
[roof]
type = SideSetsBetweenSubdomainsGenerator
new_boundary = 21
primary_block = 0
paired_block = 1
input = excav
[]
[hole]
type = BlockDeletionGenerator
block = 1
input = roof
[]
[]
[GlobalParams]
block = 0
perform_finite_strain_rotations = false
displacements = 'disp_x disp_y disp_z'
Cosserat_rotations = 'wc_x wc_y wc_z'
[]
[Variables]
[./disp_y]
[../]
[./disp_z]
[../]
[./wc_x]
[../]
[]
[Kernels]
[./cy_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_y
component = 1
[../]
[./cz_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_z
component = 2
[../]
[./x_couple]
type = StressDivergenceTensors
use_displaced_mesh = false
variable = wc_x
displacements = 'wc_x wc_y wc_z'
component = 0
base_name = couple
[../]
[./x_moment]
type = MomentBalancing
use_displaced_mesh = false
variable = wc_x
component = 0
[../]
[./gravity]
type = Gravity
use_displaced_mesh = false
variable = disp_z
value = -10E-6
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./wc_y]
[../]
[./wc_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./mc_shear]
type = MaterialStdVectorAux
index = 0
property = mc_plastic_internal_parameter
variable = mc_shear
[../]
[./mc_tensile]
type = MaterialStdVectorAux
index = 1
property = mc_plastic_internal_parameter
variable = mc_tensile
[../]
[./wp_shear]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_internal_parameter
variable = wp_shear
[../]
[./wp_tensile]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_internal_parameter
variable = wp_tensile
[../]
[./mc_shear_f]
type = MaterialStdVectorAux
index = 6
property = mc_plastic_yield_function
variable = mc_shear_f
[../]
[./mc_tensile_f]
type = MaterialStdVectorAux
index = 0
property = mc_plastic_yield_function
variable = mc_tensile_f
[../]
[./wp_shear_f]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_yield_function
variable = wp_shear_f
[../]
[./wp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_yield_function
variable = wp_tensile_f
[../]
[]
[BCs]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '11 12 16 21' # note addition of 16 and 21
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '16'
value = 0.0
[../]
[./no_wc_x]
type = DirichletBC
variable = wc_x
boundary = '11 12'
value = 0.0
[../]
[./roof]
type = FunctionDirichletBC
variable = disp_z
boundary = 21
function = excav_sideways
[../]
[]
[Functions]
[./ini_xx]
type = ParsedFunction
expression = '-0.8*2500*10E-6*(400-z)'
[../]
[./ini_zz]
type = ParsedFunction
expression = '-2500*10E-6*(400-z)'
[../]
[./excav_sideways]
type = ParsedFunction
symbol_names = 'end_t ymin ymax e_h closure_dist'
symbol_values = '1.0 0 150.0 -3.0 15.0'
expression = 'e_h*max(min((min(t/end_t,1)*(ymax-ymin)+ymin-y)/closure_dist,1),0)'
[../]
[./excav_downwards]
type = ParsedFunction
symbol_names = 'end_t ymin ymax e_h closure_dist'
symbol_values = '1.0 0 150.0 -3.0 15.0'
expression = 'e_h*min(t/end_t,1)*max(min(((ymax-ymin)+ymin-y)/closure_dist,1),0)'
[../]
[]
[UserObjects]
[./mc_coh_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 2.99 # MPa
value_residual = 3.01 # MPa
rate = 1.0
[../]
[./mc_fric]
type = SolidMechanicsHardeningConstant
value = 0.65 # 37deg
[../]
[./mc_dil]
type = SolidMechanicsHardeningConstant
value = 0.15 # 8deg
[../]
[./mc_tensile_str_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 1.0 # MPa
value_residual = 1.0 # MPa
rate = 1.0
[../]
[./mc_compressive_str]
type = SolidMechanicsHardeningCubic
value_0 = 100 # Large!
value_residual = 100
internal_limit = 0.1
[../]
[./wp_coh_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_tan_fric]
type = SolidMechanicsHardeningConstant
value = 0.36 # 20deg
[../]
[./wp_tan_dil]
type = SolidMechanicsHardeningConstant
value = 0.18 # 10deg
[../]
[./wp_tensile_str_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_compressive_str_soften]
type = SolidMechanicsHardeningCubic
value_0 = 100
value_residual = 1
internal_limit = 1.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeLayeredCosseratElasticityTensor
young = 8E3 # MPa
poisson = 0.25
layer_thickness = 1.0
joint_normal_stiffness = 1E9 # huge
joint_shear_stiffness = 1E3
[../]
[./strain]
type = ComputeCosseratIncrementalSmallStrain
eigenstrain_names = ini_stress
[../]
[./ini_stress]
type = ComputeEigenstrainFromInitialStress
initial_stress = 'ini_xx 0 0 0 ini_xx 0 0 0 ini_zz'
eigenstrain_name = ini_stress
[../]
[./stress]
type = ComputeMultipleInelasticCosseratStress
block = 0
inelastic_models = 'mc wp'
cycle_models = true
relative_tolerance = 2.0
absolute_tolerance = 1E6
max_iterations = 1
tangent_operator = nonlinear
perform_finite_strain_rotations = false
[../]
[./mc]
type = CappedMohrCoulombCosseratStressUpdate
block = 0
warn_about_precision_loss = false
host_youngs_modulus = 8E3
host_poissons_ratio = 0.25
base_name = mc
tensile_strength = mc_tensile_str_strong_harden
compressive_strength = mc_compressive_str
cohesion = mc_coh_strong_harden
friction_angle = mc_fric
dilation_angle = mc_dil
max_NR_iterations = 10000
smoothing_tol = 0.1 # MPa # Must be linked to cohesion
yield_function_tol = 1E-9 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0
[../]
[./wp]
type = CappedWeakPlaneCosseratStressUpdate
block = 0
warn_about_precision_loss = false
base_name = wp
cohesion = wp_coh_harden
tan_friction_angle = wp_tan_fric
tan_dilation_angle = wp_tan_dil
tensile_strength = wp_tensile_str_harden
compressive_strength = wp_compressive_str_soften
max_NR_iterations = 10000
tip_smoother = 0.1
smoothing_tol = 0.1 # MPa # Note, this must be tied to cohesion, otherwise get no possible return at cone apex
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0
[../]
[./density]
type = GenericConstantMaterial
prop_names = density
prop_values = 2500
[../]
[]
[Postprocessors]
[./subsidence]
type = PointValue
point = '0 0 400'
variable = disp_z
use_displaced_mesh = false
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
line_search = bt
nl_abs_tol = 1e-3
nl_rel_tol = 1e-5
l_max_its = 30
nl_max_its = 1000
start_time = 0.0
dt = 0.2
end_time = 0.2
[]
[Outputs]
file_base = cosserat_mc_wp
time_step_interval = 1
print_linear_residuals = false
csv = true
exodus = true
[./console]
type = Console
output_linear = false
[../]
[]
(modules/phase_field/examples/grain_growth/grain_growth_2D_voronoi.i)
# This simulation predicts GB migration of a 2D copper polycrystal with 15 grains
# Mesh adaptivity and time step adaptivity are used
# An AuxVariable is used to calculate the grain boundary locations
# Postprocessors are used to record time step and the number of grains
# We are not using the GrainTracker in this example so the number
# of order paramaters must match the number of grains.
[Mesh]
# Mesh block. Meshes can be read in or automatically generated
type = GeneratedMesh
dim = 2 # Problem dimension
nx = 12 # Number of elements in the x-direction
ny = 12 # Number of elements in the y-direction
nz = 0 # Number of elements in the z-direction
xmin = 0 # minimum x-coordinate of the mesh
xmax = 1000 # maximum x-coordinate of the mesh
ymin = 0 # minimum y-coordinate of the mesh
ymax = 1000 # maximum y-coordinate of the mesh
zmin = 0
zmax = 0
elem_type = QUAD4 # Type of elements used in the mesh
uniform_refine = 3 # Initial uniform refinement of the mesh
parallel_type = replicated # Periodic BCs
[]
[GlobalParams]
# Parameters used by several kernels that are defined globally to simplify input file
op_num = 15 # Number of grains
var_name_base = gr # Base name of grains
[]
[UserObjects]
[./voronoi]
type = PolycrystalVoronoi
grain_num = 15
rand_seed = 42
coloring_algorithm = bt # We must use bt to force the UserObject to assign one grain to each op
[../]
[]
[ICs]
[./PolycrystalICs]
[./PolycrystalColoringIC]
polycrystal_ic_uo = voronoi
[../]
[../]
[]
[Variables]
# Variable block, where all variables in the simulation are declared
[./PolycrystalVariables]
# Custom action that created all of the grain variables
order = FIRST # element type used by each grain variable
family = LAGRANGE
[../]
[]
[AuxVariables]
#active = ''
# Dependent variables
[./bnds]
# Variable used to visualize the grain boundaries in the simulation
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
# Kernel block, where the kernels defining the residual equations are set up.
[./PolycrystalKernel]
# Custom action creating all necessary kernels for grain growth. All input parameters are up in GlobalParams
[../]
[]
[AuxKernels]
#active = ''
# AuxKernel block, defining the equations used to calculate the auxvars
[./bnds_aux]
# AuxKernel that calculates the GB term
type = BndsCalcAux
variable = bnds
execute_on = timestep_end
[../]
[]
[BCs]
# Boundary Condition block
[./Periodic]
[./top_bottom]
auto_direction = 'x y' # Makes problem periodic in the x and y directions
[../]
[../]
[]
[Materials]
[./CuGrGr]
# Material properties
type = GBEvolution # Quantitative material properties for copper grain growth. Dimensions are nm and ns
GBmob0 = 2.5e-6 #Mobility prefactor for Cu from schonfelder1997molecular bibtex entry
GBenergy = 0.708 #GB energy for Cu from schonfelder1997molecular bibtex entry
Q = 0.23 #Activation energy for grain growth from Schonfelder 1997
T = 450 # K #Constant temperature of the simulation (for mobility calculation)
wGB = 14 # nm #Width of the diffuse GB
[../]
[]
[Postprocessors]
active = 'dt '
# Scalar postprocessors
[./dt]
# Outputs the current time step
type = TimestepSize
[../]
[]
[Executioner]
type = Transient # Type of executioner, here it is transient with an adaptive time step
scheme = bdf2 # Type of time integration (2nd order backward euler), defaults to 1st order backward euler
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -mat_mffd_type'
petsc_options_value = 'hypre boomeramg 101 ds'
l_max_its = 30 # Max number of linear iterations
l_tol = 1e-4 # Relative tolerance for linear solves
nl_max_its = 40 # Max number of nonlinear iterations
nl_abs_tol = 1e-11 # Relative tolerance for nonlienar solves
nl_rel_tol = 1e-8 # Absolute tolerance for nonlienar solves
start_time = 0.0
end_time = 4000
[./TimeStepper]
type = IterationAdaptiveDT
dt = 25 # Initial time step. In this simulation it changes.
optimal_iterations = 6 #Time step will adapt to maintain this number of nonlinear iterations
[../]
[./Adaptivity]
# Block that turns on mesh adaptivity. Note that mesh will never coarsen beyond initial mesh (before uniform refinement)
initial_adaptivity = 2 # Number of times mesh is adapted to initial condition
refine_fraction = 0.7 # Fraction of high error that will be refined
coarsen_fraction = 0.1 # Fraction of low error that will coarsened
max_h_level = 4 # Max number of refinements used, starting from initial mesh (before uniform refinement)
[../]
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
max_rows = 20
[../]
[]
(modules/xfem/test/tests/moving_interface/moving_diffusion.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 3
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
elem_type = QUAD4
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'x-0.76+0.21*t'
[../]
[]
[Kernels]
[./diff]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./time_deriv]
type = TimeDerivative
variable = u
[../]
[]
[Constraints]
[./u_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = u
jump = 0
use_penalty = true
alpha = 1e5
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./diffusivity_A]
type = GenericConstantMaterial
prop_names = A_diffusion_coefficient
prop_values = 5
[../]
[./diffusivity_B]
type = GenericConstantMaterial
prop_names = B_diffusion_coefficient
prop_values = 0.5
[../]
[./diff_combined]
type = LevelSetBiMaterialReal
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = diffusion_coefficient
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
l_max_its = 20
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-6
nl_abs_tol = 1e-5
start_time = 0.0
dt = 1
end_time = 2
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_htonly/cyl2D.i)
#
# 2D Cylindrical Gap Heat Transfer Test.
#
# This test exercises 2D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid cylinder of radius = 1 unit, and outer
# hollow cylinder with an inner radius of 2 in the x-y plane. In other words,
# the gap between them is 1 radial unit in length.
#
# The conductivity of both cylinders is set very large to achieve a uniform
# temperature in each cylinder. The temperature of the center node of the
# inner cylinder is ramped from 100 to 200 over one time unit. The temperature
# of the outside of the outer, hollow cylinder is held fixed at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer cylinders:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r*ln(r2/r1))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 2 * pi * h * r, where h is the height of the cylinder.
#
# The integrated heat flux across the gap at time 1 is then:
#
# 2*pi*h*k*delta_T/(ln(r2/r1))
# 2*pi*1*1*100/(ln(2/1)) = 906.5 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/4 of the cylinders is meshed
# As such, the integrated flux from the post processors is 1/4 of the total,
# or 226.6 watts.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
# Note that the 2D and 3D results are the same.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = cyl2D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = CYLINDER
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 0 1'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_1/brick1_aug.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick1_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 100
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x8]
type = NodalVariableValue
nodeid = 7
variable = disp_x
[../]
[./disp_x13]
type = NodalVariableValue
nodeid = 12
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y8]
type = NodalVariableValue
nodeid = 7
variable = disp_y
[../]
[./disp_y13]
type = NodalVariableValue
nodeid = 12
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_x8 disp_x13 disp_x16 disp_y5 disp_y8 disp_y13 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
tangential_tolerance = 1e-3
formulation = augmented_lagrange
normalize_penalty = true
penalty = 1e8
model = frictionless
al_penetration_tolerance = 1e-8
[../]
[]
(test/tests/outputs/output_on/postprocessors.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./sum]
type = PerfGraphData
section_name = "Root"
data_type = total
execute_on = 'initial nonlinear timestep_end'
[../]
[]
[Executioner]
type = Transient
num_steps = 2
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = false
[./console]
type = Console
execute_postprocessors_on = 'initial nonlinear timestep_end'
[../]
[]
(modules/thermal_hydraulics/test/tests/components/shaft_connected_turbine_1phase/turbine_startup.i)
# This test tests that the turbine can startup from rest and reach full power.
# The mass flow rate for the inlet component is ramped up over 10s. The dyno
# component and pid_ctrl controler are used to maintain the turbine's rated shaft
# speed. The turbine should supply ~1e6 W of power to the shaft by the end of the test.
omega_rated = 450
mdot = 5.0
T_in = 1000.0
p_out = 1e6
[GlobalParams]
f = 1
scaling_factor_1phase = '0.04 0.04 0.04e-5'
closures = simple_closures
n_elems = 20
initial_T = ${T_in}
initial_p = ${p_out}
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
[]
[FluidProperties]
[eos]
type = IdealGasFluidProperties
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[ch_in]
type = FlowChannel1Phase
position = '-1 0 0'
orientation = '1 0 0'
length = 1
A = 0.1
D_h = 1
fp = eos
[]
[inlet]
type = InletMassFlowRateTemperature1Phase
input = 'ch_in:in'
m_dot = 0
T = ${T_in}
[]
[turbine]
type = ShaftConnectedTurbine1Phase
inlet = 'ch_in:out'
outlet = 'ch_out:in'
position = '0 0 0'
scaling_factor_rhoEV = 1e-5
A_ref = 0.1
volume = 0.0002
inertia_coeff = '1 1 1 1'
inertia_const = 1.61397
speed_cr_I = 1e12
speed_cr_fr = 0
tau_fr_coeff = '0 0 0 0'
tau_fr_const = 0
omega_rated = ${omega_rated}
D_wheel = 0.4
head_coefficient = head
power_coefficient = power
[]
[ch_out]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
A = 0.1
D_h = 1
fp = eos
[]
[outlet]
type = Outlet1Phase
input = 'ch_out:out'
p = ${p_out}
[]
[dyno]
type = ShaftConnectedMotor
inertia = 10
torque = -450
[]
[shaft]
type = Shaft
connected_components = 'turbine dyno'
initial_speed = ${omega_rated}
[]
[]
[Functions]
[head]
type = PiecewiseLinear
x = '0 7e-3 1e-2'
y = '0 15 20'
[]
[power]
type = PiecewiseLinear
x = '0 6e-3 1e-2'
y = '0 0.05 0.18'
[]
[mfr_fn]
type = PiecewiseLinear
x = '0 10'
y = '1e-6 ${mdot}'
[]
[dts]
type = PiecewiseConstant
y = '5e-3 1e-2 5e-2 5e-1'
x = '0 0.5 1 10'
[]
[]
[ControlLogic]
[mfr_cntrl]
type = TimeFunctionComponentControl
component = inlet
parameter = m_dot
function = mfr_fn
[]
[speed_set_point]
type = GetFunctionValueControl
function = ${omega_rated}
[]
[pid_ctrl]
type = PIDControl
input = omega
set_point = speed_set_point:value
K_i = 2
K_p = 5
K_d = 5
initial_value = -450
[]
[set_torque_value]
type = SetComponentRealValueControl
component = dyno
parameter = torque
value = pid_ctrl:output
[]
[]
[Postprocessors]
[omega]
type = ScalarVariable
variable = shaft:omega
execute_on = 'initial timestep_end'
[]
[flow_coefficient]
type = ScalarVariable
variable = turbine:flow_coeff
execute_on = 'initial timestep_end'
[]
[delta_p]
type = ScalarVariable
variable = turbine:delta_p
execute_on = 'initial timestep_end'
[]
[power]
type = ScalarVariable
variable = turbine:power
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'implicit-euler'
start_time = 0
[TimeStepper]
type = FunctionDT
function = dts
[]
end_time = 20
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-4
nl_max_its = 30
l_tol = 1e-4
l_max_its = 20
[Quadrature]
type = GAUSS
order = SECOND
[]
[]
[Outputs]
[console]
type = Console
max_rows = 1
[]
print_linear_residuals = false
[]
(modules/contact/test/tests/verification/patch_tests/ring_4/ring4_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring4_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/pdass_problems/cylinder_friction.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '3'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '2'
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[frictionless_normal_lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
use_dual = true
[]
[tangential_lm]
block = 'secondary_lower'
use_dual = true
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[]
[_dt]
type = TimestepSize
[]
[num_lin_it]
type = NumLinearIterations
[]
[num_nonlin_it]
type = NumNonlinearIterations
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '2 3 4 5 6 7'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type -pc_factor_shift_amount -mat_mffd_err'
petsc_options_value = 'lu superlu_dist NONZERO 1e-15 1e-5'
line_search = 'none'
nl_abs_tol = 1e-7
start_time = 0.0
end_time = 0.3 # 3.5
l_tol = 1e-4
dt = 0.1
dtmin = 0.001
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[]
[y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[]
[cont_press]
type = NodalValueSampler
variable = frictionless_normal_lm
boundary = '3'
sort_by = id
[]
[friction]
type = NodalValueSampler
variable = frictionless_normal_lm
boundary = '3'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = false
csv = false
[console]
type = Console
max_rows = 5
[]
[chkfile]
type = CSV
show = 'x_disp y_disp cont_press friction'
file_base = cylinder_friction_check
create_final_symlink = true
execute_on = 'FINAL'
[]
[]
[UserObjects]
[weighted_vel_uo]
type = LMWeightedVelocitiesUserObject
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
lm_variable_normal = frictionless_normal_lm
lm_variable_tangential_one = tangential_lm
secondary_variable = disp_x
disp_x = disp_x
disp_y = disp_y
[]
[]
[Constraints]
[weighted_gap_lm]
type = ComputeFrictionalForceLMMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
variable = frictionless_normal_lm
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
friction_lm = tangential_lm
mu = 0.4
c_t = 1.0e5
c = 1.0e6
weighted_gap_uo = weighted_vel_uo
weighted_velocities_uo = weighted_vel_uo
[]
[x]
type = NormalMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = frictionless_normal_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = weighted_vel_uo
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = frictionless_normal_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = weighted_vel_uo
[]
[tangential_x]
type = TangentialMortarMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
variable = tangential_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_y]
type = TangentialMortarMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
variable = tangential_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = weighted_vel_uo
[]
[]
(modules/porous_flow/test/tests/sinks/s06.i)
# apply a half-cubic sink flux and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1.1
[]
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = x*(y+1)
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[]
[Functions]
[mass10]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)*if(pp>=0,1,pow(1+pow(-al*pp,1.0/(1-m)),-m))'
symbol_names = 'vol por dens0 pp bulk al m'
symbol_values = '0.25 0.1 1.1 p10 1.3 1.1 0.5'
[]
[rate10]
type = ParsedFunction
expression = 'fcn*if(pp>center,m,if(pp<themin,0,m/c/c/c*(2*(pp-center)+c)*((pp-center)-c)*((pp-center)-c)))'
symbol_names = 'm fcn pp center sd themin c'
symbol_values = '2 3 p10 0.9 0.5 0.1 -0.8'
[]
[mass10_expect]
type = ParsedFunction
expression = 'mass_prev-rate*area*dt'
symbol_names = 'mass_prev rate area dt'
symbol_values = 'm10_prev m10_rate 0.5 2E-3'
[]
[mass11]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)*if(pp>=0,1,pow(1+pow(-al*pp,1.0/(1-m)),-m))'
symbol_names = 'vol por dens0 pp bulk al m'
symbol_values = '0.25 0.1 1.1 p11 1.3 1.1 0.5'
[]
[rate11]
type = ParsedFunction
expression = 'fcn*if(pp>center,m,if(pp<themin,0,m/c/c/c*(2*(pp-center)+c)*((pp-center)-c)*((pp-center)-c)))'
symbol_names = 'm fcn pp center sd themin c'
symbol_values = '2 3 p11 0.9 0.5 0.1 -0.8'
[]
[mass11_expect]
type = ParsedFunction
expression = 'mass_prev-rate*area*dt'
symbol_names = 'mass_prev rate area dt'
symbol_values = 'm11_prev m11_rate 0.5 2E-3'
[]
[]
[Postprocessors]
[flux00]
type = PointValue
variable = flux_out
point = '0 0 0'
[]
[flux01]
type = PointValue
variable = flux_out
point = '0 1 0'
[]
[flux10]
type = PointValue
variable = flux_out
point = '1 0 0'
[]
[flux11]
type = PointValue
variable = flux_out
point = '1 1 0'
[]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p10]
type = PointValue
point = '1 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m10]
type = FunctionValuePostprocessor
function = mass10
execute_on = 'initial timestep_end'
[]
[m10_prev]
type = FunctionValuePostprocessor
function = mass10
execute_on = 'timestep_begin'
outputs = 'console'
[]
[m10_rate]
type = FunctionValuePostprocessor
function = rate10
execute_on = 'timestep_end'
[]
[m10_expect]
type = FunctionValuePostprocessor
function = mass10_expect
execute_on = 'timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m11]
type = FunctionValuePostprocessor
function = mass11
execute_on = 'initial timestep_end'
[]
[m11_prev]
type = FunctionValuePostprocessor
function = mass11
execute_on = 'timestep_begin'
outputs = 'console'
[]
[m11_rate]
type = FunctionValuePostprocessor
function = rate11
execute_on = 'timestep_end'
[]
[m11_expect]
type = FunctionValuePostprocessor
function = mass11_expect
execute_on = 'timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowHalfCubicSink
boundary = 'left right'
max = 2
cutoff = -0.8
center = 0.9
variable = pp
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 3
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 2E-3
end_time = 6E-2
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s06
[console]
type = Console
execute_on = 'nonlinear linear'
time_step_interval = 5
[]
[csv]
type = CSV
execute_on = 'timestep_end'
time_step_interval = 3
[]
[]
(modules/porous_flow/test/tests/sinks/s07.i)
# apply a sink flux on just one component of a 3-component system and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp frac0 frac1'
number_fluid_phases = 1
number_fluid_components = 3
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1.1
[]
[]
[Variables]
[pp]
[]
[frac0]
initial_condition = 0.1
[]
[frac1]
initial_condition = 0.6
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = y
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = frac0
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = frac1
[]
[mass2]
type = PorousFlowMassTimeDerivative
fluid_component = 2
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = 'frac0 frac1'
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.2 0 0 0 0.1 0 0 0 0.1'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[]
[Functions]
[mass1_00]
type = ParsedFunction
expression = 'frac*vol*por*dens0*exp(pp/bulk)*pow(1+pow(-al*pp,1.0/(1-m)),-m)'
symbol_names = 'frac vol por dens0 pp bulk al m'
symbol_values = 'f1_00 0.25 0.1 1.1 p00 1.3 1.1 0.5'
[]
[expected_mass_change1_00]
type = ParsedFunction
expression = 'frac*fcn*area*dt'
symbol_names = 'frac fcn area dt'
symbol_values = 'f1_00 6 0.5 1E-3'
[]
[mass1_00_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm1_00_prev del_m1_00'
[]
[mass1_01]
type = ParsedFunction
expression = 'frac*vol*por*dens0*exp(pp/bulk)*pow(1+pow(-al*pp,1.0/(1-m)),-m)'
symbol_names = 'frac vol por dens0 pp bulk al m'
symbol_values = 'f1_01 0.25 0.1 1.1 p01 1.3 1.1 0.5'
[]
[expected_mass_change1_01]
type = ParsedFunction
expression = 'frac*fcn*area*dt'
symbol_names = 'frac fcn area dt'
symbol_values = 'f1_01 6 0.5 1E-3'
[]
[mass1_01_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm1_01_prev del_m1_01'
[]
[]
[Postprocessors]
[f1_00]
type = PointValue
point = '0 0 0'
variable = frac1
execute_on = 'initial timestep_end'
[]
[flux_00]
type = PointValue
point = '0 0 0'
variable = flux_out
execute_on = 'initial timestep_end'
[]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m1_00]
type = FunctionValuePostprocessor
function = mass1_00
execute_on = 'initial timestep_end'
[]
[m1_00_prev]
type = FunctionValuePostprocessor
function = mass1_00
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m1_00]
type = FunctionValuePostprocessor
function = expected_mass_change1_00
execute_on = 'timestep_end'
outputs = 'console'
[]
[m1_00_expect]
type = FunctionValuePostprocessor
function = mass1_00_expect
execute_on = 'timestep_end'
[]
[f1_01]
type = PointValue
point = '0 1 0'
variable = frac1
execute_on = 'initial timestep_end'
[]
[flux_01]
type = PointValue
point = '0 1 0'
variable = flux_out
execute_on = 'initial timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m1_01]
type = FunctionValuePostprocessor
function = mass1_01
execute_on = 'initial timestep_end'
[]
[m1_01_prev]
type = FunctionValuePostprocessor
function = mass1_01
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m1_01]
type = FunctionValuePostprocessor
function = expected_mass_change1_01
execute_on = 'timestep_end'
outputs = 'console'
[]
[m1_01_expect]
type = FunctionValuePostprocessor
function = mass1_01_expect
execute_on = 'timestep_end'
[]
[f1_11]
type = PointValue
point = '1 1 0'
variable = frac1
execute_on = 'initial timestep_end'
[]
[flux_11]
type = PointValue
point = '1 1 0'
variable = flux_out
execute_on = 'initial timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowSink
boundary = 'left'
variable = frac1
use_mobility = false
use_relperm = false
mass_fraction_component = 1
fluid_phase = 0
flux_function = 6
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-3
end_time = 0.01
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s07
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
execute_on = 'timestep_end'
[]
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q8/hertz_cyl_half_1deg_template1.i)
[GlobalParams]
order = SECOND
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x639]
type = NodalVariableValue
nodeid = 638
variable = disp_x
[../]
[./disp_y639]
type = NodalVariableValue
nodeid = 638
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-5
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 3.5
l_tol = 1e-3
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x639 disp_y639 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
(test/tests/time_integrators/explicit-euler/ee-1d-quadratic-neumann.i)
[GlobalParams]
implicit = false
[]
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 10
elem_type = EDGE3
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = x*x-2*t+t*x*x
[../]
[./exact_fn]
type = ParsedFunction
expression = t*x*x
[../]
[./left_bc_fn]
type = ParsedFunction
expression = -t*2*x
[../]
[./right_bc_fn]
type = ParsedFunction
expression = t*2*x
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./td]
type = TimeDerivative
variable = u
implicit = true
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./abs]
type = Reaction
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./left]
type = FunctionNeumannBC
variable = u
boundary = '0'
function = left_bc_fn
[../]
[./right]
type = FunctionNeumannBC
variable = u
boundary = '1'
function = right_bc_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
scheme = 'explicit-euler'
solve_type = 'LINEAR'
l_tol = 1e-12
start_time = 0.0
num_steps = 10
dt = 0.001
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/phase_field/tutorials/spinodal_decomposition/s2_fasttest.i)
#
# Simulation of an iron-chromium alloy using simple code and a test set of
# initial conditions.
#
[Mesh]
# generate a 2D, 25nm x 25nm mesh
type = GeneratedMesh
dim = 2
elem_type = QUAD4
nx = 100
ny = 100
nz = 0
xmin = 0
xmax = 25
ymin = 0
ymax = 25
zmin = 0
zmax = 0
[]
[Variables]
[./c] # Mole fraction of Cr (unitless)
order = FIRST
family = LAGRANGE
[../]
[./w] # Chemical potential (eV/mol)
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
# Use a bounding box IC at equilibrium concentrations to make sure the
# model behaves as expected.
[./testIC]
type = BoundingBoxIC
variable = c
x1 = 5
x2 = 20
y1 = 5
y2 = 20
inside = 0.823
outside = 0.236
[../]
[]
[BCs]
# periodic BC as is usually done on phase-field models
[./Periodic]
[./c_bcs]
auto_direction = 'x y'
[../]
[../]
[]
[Kernels]
# See wiki page "Developing Phase Field Models" for more information on Split
# Cahn-Hilliard equation kernels.
# http://mooseframework.org/wiki/PhysicsModules/PhaseField/DevelopingModels/
[./w_dot]
variable = w
v = c
type = CoupledTimeDerivative
[../]
[./coupled_res]
variable = w
type = SplitCHWRes
mob_name = M
[../]
[./coupled_parsed]
variable = c
type = SplitCHParsed
f_name = f_loc
kappa_name = kappa_c
w = w
[../]
[]
[Materials]
# d is a scaling factor that makes it easier for the solution to converge
# without changing the results. It is defined in each of the materials and
# must have the same value in each one.
[./constants]
# Define constant values kappa_c and M. Eventually M will be replaced with
# an equation rather than a constant.
type = GenericFunctionMaterial
prop_names = 'kappa_c M'
prop_values = '8.125e-16*6.24150934e+18*1e+09^2*1e-27
2.2841e-26*1e+09^2/6.24150934e+18/1e-27'
# kappa_c*eV_J*nm_m^2*d
# M*nm_m^2/eV_J/d
[../]
[./local_energy]
# Defines the function for the local free energy density as given in the
# problem, then converts units and adds scaling factor.
type = DerivativeParsedMaterial
property_name = f_loc
coupled_variables = c
constant_names = 'A B C D E F G eV_J d'
constant_expressions = '-2.446831e+04 -2.827533e+04 4.167994e+03 7.052907e+03
1.208993e+04 2.568625e+03 -2.354293e+03
6.24150934e+18 1e-27'
expression = 'eV_J*d*(A*c+B*(1-c)+C*c*log(c)+D*(1-c)*log(1-c)+
E*c*(1-c)+F*c*(1-c)*(2*c-1)+G*c*(1-c)*(2*c-1)^2)'
derivative_order = 2
[../]
[]
[Postprocessors]
[./evaluations] # Cumulative residual calculations for simulation
type = NumResidualEvaluations
[../]
[./elapsed]
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[]
[Preconditioning]
# Preconditioning is required for Newton's method. See wiki page "Solving
# Phase Field Models" for more information.
# http://mooseframework.org/wiki/PhysicsModules/PhaseField/SolvingModels/
[./coupled]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 30
l_tol = 1e-6
nl_max_its = 50
nl_abs_tol = 1e-9
end_time = 86400 # 1 day. We only need to run this long enough to verify
# the model is working properly.
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type
-sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly
ilu 1'
[./TimeStepper]
# Turn on time stepping
type = IterationAdaptiveDT
dt = 10
cutback_factor = 0.8
growth_factor = 1.5
optimal_iterations = 7
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
exodus = true
console = true
csv = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/richards/test/tests/gravity_head_1/gh23.i)
# investigating validity of immobile saturation
# 50 elements, with SUPG
[Mesh]
type = GeneratedMesh
dim = 1
nx = 50
xmin = -1
xmax = 1
[]
[GlobalParams]
richardsVarNames_UO = PPNames
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '1 10 100 1000 10000'
x = '0 10 100 1000 10000'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = pressure
[../]
[./DensityConstBulk]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 1.0E3
[../]
[./SeffVG]
type = RichardsSeff1VG
m = 0.8
al = 1
[../]
[./RelPermPower]
type = RichardsRelPermPower
simm = 0.3
n = 2
[../]
[./Saturation]
type = RichardsSat
s_res = 0.1
sum_s_res = 0.1
[../]
[./SUPGstandard]
type = RichardsSUPGstandard
p_SUPG = 1.0E-6
[../]
[]
[Variables]
[./pressure]
order = FIRST
family = LAGRANGE
initial_condition = -1.0
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsf richardst'
[./richardst]
type = RichardsMassChange
variable = pressure
[../]
[./richardsf]
type = RichardsFlux
variable = pressure
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffVG
pressure_vars = pressure
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
density_UO = DensityConstBulk
relperm_UO = RelPermPower
SUPG_UO = SUPGstandard
sat_UO = Saturation
seff_UO = SeffVG
viscosity = 1E-3
gravity = '-1 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E0
end_time = 1E5
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = gh23
execute_on = 'timestep_end final'
time_step_interval = 10000
exodus = true
[./console]
time_step_interval = 1
type = Console
[../]
[]
(modules/navier_stokes/test/tests/finite_element/pins/channel-flow/pm_reverse_flow.i)
# This test case tests the porous-medium flow when flow reversal happens
[GlobalParams]
gravity = '0 0 0'
order = FIRST
family = LAGRANGE
u = vel_x
v = vel_y
pressure = p
temperature = T
porosity = porosity
eos = eos
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
nx = 10
ny = 4
elem_type = QUAD4
[]
[FluidProperties]
[eos]
type = SimpleFluidProperties
density0 = 100 # kg/m^3
thermal_expansion = 0 # K^{-1}
cp = 100
viscosity = 0.1 # Pa-s, Re=rho*u*L/mu = 100*1*0.1/0.1 = 100
thermal_conductivity = 0.1
[]
[]
[Functions]
[v_in]
type = PiecewiseLinear
x = '0 5 10 1e5'
y = '1 0 -1 -1'
[]
[T_in]
type = PiecewiseLinear
x = '0 1e5'
y = '630 630'
[]
[]
[Variables]
# velocity
[vel_x]
initial_condition = 1
[]
[vel_y]
initial_condition = 0
[]
[p]
initial_condition = 1e5
[]
[T]
scaling = 1e-3
initial_condition = 630
[]
[]
[AuxVariables]
[rho]
initial_condition = 100
[]
[porosity]
initial_condition = 0.4
[]
[vol_heat]
initial_condition = 1e6
[]
[T_out_scalar]
family = SCALAR
order = FIRST
initial_condition = 630
[]
[]
[Materials]
[mat]
type = PINSFEMaterial
alpha = 1000
beta = 100
[]
[]
[Kernels]
[mass_time]
type = PINSFEFluidPressureTimeDerivative
variable = p
[]
[mass_space]
type = INSFEFluidMassKernel
variable = p
[]
[x_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_x
[]
[x_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_x
component = 0
[]
[y_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_y
[]
[y_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_y
component = 1
[]
[temperature_time]
type = PINSFEFluidTemperatureTimeDerivative
variable = T
[../]
[temperature_space]
type = INSFEFluidEnergyKernel
variable = T
power_density = vol_heat
[]
[]
[AuxKernels]
[rho_aux]
type = FluidDensityAux
variable = rho
p = p
T = T
fp = eos
[]
[]
[BCs]
# BCs for mass equation
# Inlet
[mass_inlet]
type = INSFEFluidMassBC
variable = p
boundary = 'left'
v_fn = v_in
[]
# Outlet
[./pressure_out]
type = DirichletBC
variable = p
boundary = 'right'
value = 1e5
[../]
# BCs for x-momentum equation
# Inlet
[vx_in]
type = FunctionDirichletBC
variable = vel_x
boundary = 'left'
function = v_in
[]
# Outlet (no BC is needed)
# BCs for y-momentum equation
# Both Inlet and Outlet, and Top and Bottom
[vy]
type = DirichletBC
variable = vel_y
boundary = 'left right bottom top'
value = 0
[]
# BCs for energy equation
[T_in]
type = INSFEFluidEnergyDirichletBC
variable = T
boundary = 'left'
out_norm = '-1 0 0'
T_fn = 630
[]
[T_out]
type = INSFEFluidEnergyDirichletBC
variable = T
boundary = 'right'
out_norm = '1 0 0'
T_scalar = T_out_scalar
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
solve_type = 'PJFNK'
[]
[]
[Postprocessors]
[p_in]
type = SideAverageValue
variable = p
boundary = left
[]
[p_out]
type = SideAverageValue
variable = p
boundary = right
[]
[T_in]
type = SideAverageValue
variable = T
boundary = left
[]
[T_out]
type = SideAverageValue
variable = T
boundary = right
[]
[]
[Executioner]
type = Transient
dt = 0.5
dtmin = 1.e-3
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
nl_max_its = 20
l_tol = 1e-5
l_max_its = 100
start_time = 0.0
end_time = 10
num_steps = 20
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
time_step_interval = 1
execute_on = 'initial timestep_end'
[console]
type = Console
output_linear = false
[]
[out]
type = Exodus
use_displaced = false
hide = 'T_out_scalar'
[]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/03_upper_loop.i)
T_in = 300. # K
m_dot_in = 1e-2 # kg/s
press = 10e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 25
core_dia = '${units 2. cm -> m}'
core_pitch = '${units 8.7 cm -> m}'
A_core = '${fparse core_pitch^2 - 0.25 *pi * core_dia^2}'
P_wet_core = '${fparse 4*core_pitch + pi * core_dia}'
Dh_core = '${fparse 4 * A_core / P_wet_core}'
# pipe parameters
pipe_dia = '${units 10. cm -> m}'
A_pipe = '${fparse 0.25 * pi * pipe_dia^2}'
tot_power = 2000 # W
[GlobalParams]
initial_p = ${press}
initial_vel = 0.0001
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
gravity_vector = '0 0 0'
rdg_slope_reconstruction = minmod
scaling_factor_1phase = '1 1e-2 1e-4'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1e-2
scaling_factor_rhovV = 1e-2
scaling_factor_rhowV = 1e-2
scaling_factor_rhoEV = 1e-4
closures = thm_closures
fp = he
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[]
[Closures]
[thm_closures]
type = Closures1PhaseTHM
[]
[]
[SolidProperties]
[steel]
type = ThermalFunctionSolidProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[inlet]
type = InletMassFlowRateTemperature1Phase
input = 'up_pipe_1:in'
m_dot = ${m_dot_in}
T = ${T_in}
[]
[up_pipe_1]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 0.5
n_elems = 15
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 0.5'
connections = 'up_pipe_1:out core_chan:in'
volume = 1e-5
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
roughness = .0001
A = '${A_core}'
D_h = ${Dh_core}
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
solid_properties = 'steel'
solid_properties_T_ref = '300'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = '${fparse pi * core_dia}'
[]
[jct2]
type = JunctionParallelChannels1Phase
position = '0 0 1.5'
connections = 'core_chan:out up_pipe_2:in'
volume = 1e-5
[]
[up_pipe_2]
type = FlowChannel1Phase
position = '0 0 1.5'
orientation = '0 0 1'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct3]
type = JunctionOneToOne1Phase
connections = 'up_pipe_2:out top_pipe:in'
[]
[top_pipe]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 1
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct4]
type = JunctionOneToOne1Phase
connections = 'top_pipe:out down_pipe_1:in'
[]
[down_pipe_1]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = 0.25
A = ${A_pipe}
n_elems = 5
[]
[jct5]
type = JunctionOneToOne1Phase
connections = 'down_pipe_1:out cooling_pipe:in'
[]
[cooling_pipe]
type = FlowChannel1Phase
position = '1 0 1.75'
orientation = '0 0 -1'
length = 1.5
n_elems = 25
A = ${A_pipe}
[]
[cold_wall]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = cooling_pipe
T_wall = 300
P_hf = '${fparse pi * pipe_dia}'
[]
[jct6]
type = JunctionOneToOne1Phase
connections = 'cooling_pipe:out down_pipe_2:in'
[]
[down_pipe_2]
type = FlowChannel1Phase
position = '1 0 0.25'
orientation = '0 0 -1'
length = 0.25
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[outlet]
type = Outlet1Phase
input = 'down_pipe_2:out'
p = ${press}
[]
[]
[Postprocessors]
[power_to_coolant]
type = ADHeatRateConvection1Phase
block = core_chan
P_hf = '${fparse pi *core_dia}'
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[core_p_in]
type = SideAverageValue
boundary = core_chan:in
variable = p
[]
[core_p_out]
type = SideAverageValue
boundary = core_chan:out
variable = p
[]
[core_delta_p]
type = ParsedPostprocessor
pp_names = 'core_p_in core_p_out'
expression = 'core_p_in - core_p_out'
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = cooling_pipe:out
variable = T
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = IterationAdaptiveDT
dt = 1
[]
end_time = 500
line_search = basic
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 25
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(test/tests/time_integrators/explicit-euler/ee-1d-linear.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 200
elem_type = EDGE2
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = x
[../]
[./exact_fn]
type = ParsedFunction
expression = t*x
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
lumping = true
implicit = true
[../]
[./diff]
type = Diffusion
variable = u
implicit = false
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
implicit = false
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1'
function = exact_fn
implicit = true
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
scheme = 'explicit-euler'
solve_type = 'LINEAR'
start_time = 0.0
num_steps = 20
dt = 0.00005
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(test/tests/postprocessors/pps_interval/pps_bad_interval2.i)
[Mesh]
file = square-2x2-nodeids.e
# This test can only be run with renumering disabled, so the
# NodalVariableValue postprocessor's node id is well-defined.
allow_renumbering = false
[]
[Variables]
active = 'u v'
[./u]
order = SECOND
family = LAGRANGE
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Functions]
active = 'force_fn exact_fn left_bc'
[./force_fn]
type = ParsedFunction
expression = '1-x*x+2*t'
[../]
[./exact_fn]
type = ParsedFunction
expression = '(1-x*x)*t'
[../]
[./left_bc]
type = ParsedFunction
expression = t
[../]
[]
[Kernels]
active = '
time_u diff_u ffn_u
time_v diff_v'
[./time_u]
type = TimeDerivative
variable = u
[../]
[./diff_u]
type = Diffusion
variable = u
[../]
[./ffn_u]
type = BodyForce
variable = u
function = force_fn
[../]
[./time_v]
type = TimeDerivative
variable = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'all_u left_v right_v'
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = exact_fn
[../]
[./left_v]
type = FunctionDirichletBC
variable = v
boundary = '3'
function = left_bc
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = '2'
value = 0
[../]
[]
[Postprocessors]
active = 'l2 node1 node4'
[./l2]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[./node1]
type = NodalVariableValue
variable = u
nodeid = 15
[../]
[./node4]
type = NodalVariableValue
variable = v
nodeid = 10
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
dt = 0.1
start_time = 0
end_time = 1
[]
[Outputs]
file_base = ignore_bad
exodus = true
[./console]
type = Console
time_step_interval = 2
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_3/plane3_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane3_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 200
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-8
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_htonly/sphere3D.i)
#
# 3D Spherical Gap Heat Transfer Test.
#
# This test exercises 3D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid sphere of radius = 1 unit, and outer
# hollow sphere with an inner radius of 2. In other words, the gap between
# them is 1 radial unit in length.
#
# The conductivity of both spheres is set very large to achieve a uniform
# temperature in each sphere. The temperature of the center node of the
# inner sphere is ramped from 100 to 200 over one time unit. The
# temperature of the outside of the outer, hollow sphere is held fixed
# at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer spheres:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r^2*((1/r1)-(1/r2)))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 4 * pi * 1^2 (4*pi*r^2)
#
# The integrated heat flux across the gap at time 1 is then:
#
# 4*pi*k*delta_T/((1/r1)-(1/r2))
# 4*pi*1*100/((1/1) - (1/2)) = 2513.3 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/8 of the spheres is meshed
# As such, the integrated flux from the post processors is 1/8 of the total,
# or 314.159 watts... i.e. 100*pi.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = sphere3D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 100000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 5
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/test.i)
[GlobalParams]
#displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
use_crack_growth_increment = true
crack_growth_increment = 0.2
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.3 0.5'
time_start_cut = 0.0
time_end_cut = 2.0
heal_always = true
[../]
[]
[Modules/TensorMechanics/Master]
displacements = 'disp_x disp_y'
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
displacements = 'disp_x disp_y'
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50 100'
y='0 0.02 0.1'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 0
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
block = 0
displacements = 'disp_x disp_y'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 5000
max_xfem_update = 1
[]
[Outputs]
file_base = crack_propagation_2d_out
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_3/ring3_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring3_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
# petsc_options = '-mat_superlu_dist_iterrefine -mat_superlu_dist_replacetinypivot'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d_frictional.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = single_point_2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./appl_disp]
type = PiecewiseLinear
x = '0 0.001 0.101'
y = '0 0.0 -0.10'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = appl_disp
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.002001
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputePlaneFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputePlaneFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[./disp_y]
type = NodalVariableValue
nodeid = 5
variable = disp_y
[../]
[./inc_slip_x]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_x
[../]
[./inc_slip_y]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_y
[../]
[./accum_slip_x]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_x
[../]
[./accum_slip_y]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.001
num_steps = 10000
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
file_base = single_point_2d_out_frictional_0_2_kin
print_linear_residuals = true
perf_graph = true
csv = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = coulomb
formulation = kinematic
penalty = 1e12
normalize_penalty = true
friction_coefficient = '0.2'
tangential_tolerance = 1e-3
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_1/brick1_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick1_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x8]
type = NodalVariableValue
nodeid = 7
variable = disp_x
[../]
[./disp_x13]
type = NodalVariableValue
nodeid = 12
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y8]
type = NodalVariableValue
nodeid = 7
variable = disp_y
[../]
[./disp_y13]
type = NodalVariableValue
nodeid = 12
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_x8 disp_x13 disp_x16 disp_y5 disp_y8 disp_y13 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(test/tests/transfers/multiapp_conservative_transfer/sub_nearest_point.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0.01 # to make sure the meshes don't align
xmax = 0.49 # to make sure the meshes don't align
ymax = 1
nx = 10
ny = 10
[]
[block1]
input = gen
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '0.2 0.2 0'
top_right = '0.3 0.8 0'
[]
[]
[Variables]
[sink]
family = MONOMIAL
order = CONSTANT
[]
[]
[Functions]
[sink_func]
type = ParsedFunction
expression = '5e2*x*(0.5-x)+5e1'
[]
[]
[Kernels]
[reaction]
type = Reaction
variable = sink
[]
[coupledforce]
type = BodyForce
variable = sink
function = sink_func
[]
[]
[AuxVariables]
[from_parent]
block = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Postprocessors]
[sink]
type = ElementIntegralVariablePostprocessor
block = 1
variable = sink
[]
[from_parent_pp]
type = ElementIntegralVariablePostprocessor
block = 1
variable = from_parent
execute_on = 'transfer'
[]
[]
[Outputs]
exodus = true
[console]
type = Console
execute_on = 'timestep_end timestep_begin'
[]
[]
(test/tests/fvkernels/fv_adapt/steady-adapt.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 2
ny = 1
elem_type = QUAD4
[]
[]
[Variables]
[u]
order = CONSTANT
family = MONOMIAL
fv = true
type = MooseVariableFVReal
[]
[]
[Functions]
[exact-quadratic]
type = ParsedFunction
expression = '-(x-1)^2+1'
[]
[exact-linear]
type = ParsedFunction
expression = 'x'
[]
[]
[FVKernels]
inactive = 'source'
[diff]
type = FVDiffusion
variable = u
coeff = coeff
use_point_neighbors = true
[]
[source]
type = FVBodyForce
variable = u
function = 2
[]
[]
[FVBCs]
[right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[]
[left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[]
[]
[Materials]
[diff]
type = ADGenericFunctorMaterial
prop_names = 'coeff'
prop_values = '1'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type'
petsc_options_value = 'hypre'
[]
[Adaptivity]
marker = box
initial_steps = 1
[Markers]
[box]
bottom_left = '0.5 0 0'
inside = refine
top_right = '1 1 0'
outside = do_nothing
type = BoxMarker
[]
[]
[]
[Outputs]
exodus = true
csv = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
[Postprocessors]
[error]
type = ElementL2Error
variable = u
function = exact-linear
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/thermal_hydraulics/test/tests/components/heat_transfer_from_heat_flux_1phase/phy.energy_heatflux_ss_1phase.i)
# This test tests conservation of energy at steady state for 1-phase flow when a
# heat flux is specified. Conservation is checked by comparing the integral of
# the heat flux against the difference of the boundary fluxes.
[GlobalParams]
initial_p = 7.0e6
initial_vel = 0
initial_T = 513
gravity_vector = '0.0 0.0 0.0'
closures = simple_closures
[]
[FluidProperties]
[eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 3.66
n_elems = 10
A = 1.907720E-04
D_h = 1.698566E-02
f = 0.0
fp = eos
[]
[ht_pipe]
type = HeatTransferFromHeatFlux1Phase
flow_channel = pipe
q_wall = 1.0e5
Hw = 1.0e4
P_hf = 4.4925e-2
[]
[inlet]
type = SolidWall1Phase
input = 'pipe:in'
[]
[outlet]
type = SolidWall1Phase
input = 'pipe:out'
[]
[]
[Postprocessors]
[E]
type = ElementIntegralVariablePostprocessor
variable = rhoEA
execute_on = 'initial timestep_end'
[]
[E_change]
type = ChangeOverTimePostprocessor
postprocessor = E
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
abort_on_solve_fail = true
dt = 1
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-7
nl_max_its = 50
l_tol = 1e-3
l_max_its = 60
start_time = 0
num_steps = 10
[]
[Outputs]
[out]
type = CSV
show = 'E_change'
[]
[console]
type = Console
show = 'E_change'
[]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/04_loop.i)
T_in = 300. # K
m_dot_in = 1e-2 # kg/s
press = 10e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 25
core_dia = '${units 2. cm -> m}'
core_pitch = '${units 8.7 cm -> m}'
# pipe parameters
pipe_dia = '${units 10. cm -> m}'
A_pipe = '${fparse 0.25 * pi * pipe_dia^2}'
A_core = '${fparse core_pitch^2 - 0.25 *pi * core_dia^2}'
P_wet_core = '${fparse 4*core_pitch + pi * core_dia}'
Dh_core = '${fparse 4 * A_core / P_wet_core}'
tot_power = 2000 # W
[GlobalParams]
initial_p = ${press}
initial_vel = 0.0001
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
gravity_vector = '0 0 0'
rdg_slope_reconstruction = minmod
scaling_factor_1phase = '1 1e-2 1e-4'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1e-2
scaling_factor_rhovV = 1e-2
scaling_factor_rhowV = 1e-2
scaling_factor_rhoEV = 1e-4
closures = simple_closures
fp = he
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseTHM
[]
[]
[SolidProperties]
[steel]
type = ThermalFunctionSolidProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[up_pipe_1]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 0.5
n_elems = 15
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 0.5'
connections = 'up_pipe_1:out core_chan:in'
volume = 1e-5
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
roughness = .0001
A = '${A_core}'
D_h = ${Dh_core}
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
solid_properties = 'steel'
solid_properties_T_ref = '300'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = '${fparse pi * core_dia}'
[]
[jct2]
type = JunctionParallelChannels1Phase
position = '0 0 1.5'
connections = 'core_chan:out up_pipe_2:in'
volume = 1e-5
[]
[up_pipe_2]
type = FlowChannel1Phase
position = '0 0 1.5'
orientation = '0 0 1'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct3]
type = JunctionOneToOne1Phase
connections = 'up_pipe_2:out top_pipe_1:in'
[]
[top_pipe_1]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[top_pipe_2]
type = FlowChannel1Phase
position = '0.5 0 2'
orientation = '1 0 0'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct4]
type = VolumeJunction1Phase
position = '0.5 0 2'
volume = 1e-5
connections = 'top_pipe_1:out top_pipe_2:in press_pipe:in'
[]
[press_pipe]
type = FlowChannel1Phase
position = '0.5 0 2'
orientation = '0 0 1'
length = 0.2
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[pressurizer]
type = InletStagnationPressureTemperature1Phase
p0 = ${press}
T0 = ${T_in}
input = press_pipe:out
[]
[jct5]
type = JunctionOneToOne1Phase
connections = 'top_pipe_2:out down_pipe_1:in'
[]
[down_pipe_1]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = 0.25
A = ${A_pipe}
n_elems = 5
[]
[jct6]
type = JunctionOneToOne1Phase
connections = 'down_pipe_1:out cooling_pipe:in'
[]
[cooling_pipe]
type = FlowChannel1Phase
position = '1 0 1.75'
orientation = '0 0 -1'
length = 1.5
n_elems = 25
A = ${A_pipe}
[]
[cold_wall]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = cooling_pipe
T_wall = 300
P_hf = '${fparse pi * pipe_dia}'
[]
[jct7]
type = JunctionOneToOne1Phase
connections = 'cooling_pipe:out down_pipe_2:in'
[]
[down_pipe_2]
type = FlowChannel1Phase
position = '1 0 0.25'
orientation = '0 0 -1'
length = 0.25
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct8]
type = JunctionOneToOne1Phase
connections = 'down_pipe_2:out bottom_1:in'
[]
[bottom_1]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[pump]
type = Pump1Phase
position = '0.5 0 0'
connections = 'bottom_1:out bottom_2:in'
volume = 1e-4
A_ref = ${A_pipe}
head = 0
[]
[bottom_2]
type = FlowChannel1Phase
position = '0.5 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct10]
type = JunctionOneToOne1Phase
connections = 'bottom_2:out up_pipe_1:in'
[]
[]
[ControlLogic]
[set_point]
type = GetFunctionValueControl
function = ${m_dot_in}
[]
[pid]
type = PIDControl
initial_value = 0
set_point = set_point:value
input = m_dot_pump
K_p = 1.
K_i = 4.
K_d = 0
[]
[set_pump_head]
type = SetComponentRealValueControl
component = pump
parameter = head
value = pid:output
[]
[]
[Postprocessors]
[power_to_coolant]
type = ADHeatRateConvection1Phase
block = core_chan
P_hf = '${fparse pi *core_dia}'
[]
[m_dot_pump]
type = ADFlowJunctionFlux1Phase
boundary = core_chan:in
connection_index = 1
equation = mass
junction = jct7
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[core_p_in]
type = SideAverageValue
boundary = core_chan:in
variable = p
[]
[core_p_out]
type = SideAverageValue
boundary = core_chan:out
variable = p
[]
[core_delta_p]
type = ParsedPostprocessor
pp_names = 'core_p_in core_p_out'
expression = 'core_p_in - core_p_out'
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = cooling_pipe:out
variable = T
[]
[pump_head]
type = RealComponentParameterValuePostprocessor
component = pump
parameter = head
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = IterationAdaptiveDT
dt = 1
[]
dtmax = 5
end_time = 500
line_search = basic
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 25
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/05_secondary_side.i)
T_in = 300. # K
m_dot_in = 1e-2 # kg/s
press = 10e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 25
core_dia = '${units 2. cm -> m}'
core_pitch = '${units 8.7 cm -> m}'
A_core = '${fparse core_pitch^2 - 0.25 *pi * core_dia^2}'
P_wet_core = '${fparse 4*core_pitch + pi * core_dia}'
Dh_core = '${fparse 4 * A_core / P_wet_core}'
# pipe parameters
pipe_dia = '${units 10. cm -> m}'
A_pipe = '${fparse 0.25 * pi * pipe_dia^2}'
tot_power = 2000 # W
# heat exchanger parameters
hx_dia_inner = '${units 12. cm -> m}'
hx_wall_thickness = '${units 5. mm -> m}'
hx_dia_outer = '${units 50. cm -> m}'
hx_radius_wall = '${fparse hx_dia_inner / 2. + hx_wall_thickness}'
hx_length = 1.5 # m
hx_n_elems = 25
m_dot_sec_in = 1. # kg/s
[GlobalParams]
initial_p = ${press}
initial_vel = 0.0001
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
gravity_vector = '0 0 0'
rdg_slope_reconstruction = minmod
scaling_factor_1phase = '1 1e-2 1e-4'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1e-2
scaling_factor_rhovV = 1e-2
scaling_factor_rhowV = 1e-2
scaling_factor_rhoEV = 1e-4
closures = thm_closures
fp = he
[]
[Functions]
[m_dot_sec_fn]
type = PiecewiseLinear
xy_data = '
0 0
10 ${m_dot_sec_in}'
[]
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[water]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[thm_closures]
type = Closures1PhaseTHM
[]
[]
[SolidProperties]
[steel]
type = ThermalFunctionSolidProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[up_pipe_1]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 0.5
n_elems = 15
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 0.5'
connections = 'up_pipe_1:out core_chan:in'
volume = 1e-5
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
roughness = .0001
A = ${A_core}
D_h = ${Dh_core}
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
solid_properties = 'steel'
solid_properties_T_ref = '300'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = '${fparse pi * core_dia}'
[]
[jct2]
type = JunctionParallelChannels1Phase
position = '0 0 1.5'
connections = 'core_chan:out up_pipe_2:in'
volume = 1e-5
[]
[up_pipe_2]
type = FlowChannel1Phase
position = '0 0 1.5'
orientation = '0 0 1'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct3]
type = JunctionOneToOne1Phase
connections = 'up_pipe_2:out top_pipe_1:in'
[]
[top_pipe_1]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[top_pipe_2]
type = FlowChannel1Phase
position = '0.5 0 2'
orientation = '1 0 0'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct4]
type = VolumeJunction1Phase
position = '0.5 0 2'
volume = 1e-5
connections = 'top_pipe_1:out top_pipe_2:in press_pipe:in'
[]
[press_pipe]
type = FlowChannel1Phase
position = '0.5 0 2'
orientation = '0 1 0'
length = 0.2
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[pressurizer]
type = InletStagnationPressureTemperature1Phase
p0 = ${press}
T0 = ${T_in}
input = press_pipe:out
[]
[jct5]
type = JunctionOneToOne1Phase
connections = 'top_pipe_2:out down_pipe_1:in'
[]
[down_pipe_1]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = 0.25
A = ${A_pipe}
n_elems = 5
[]
[jct6]
type = JunctionParallelChannels1Phase
position = '1 0 1.75'
connections = 'down_pipe_1:out hx/pri:in'
volume = 1e-5
[]
[hx]
[pri]
type = FlowChannel1Phase
position = '1 0 1.75'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
roughness = 1e-5
A = '${fparse pi * hx_dia_inner * hx_dia_inner / 4.}'
D_h = ${hx_dia_inner}
[]
[ht_pri]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = inner
flow_channel = hx/pri
P_hf = '${fparse pi * hx_dia_inner}'
[]
[wall]
type = HeatStructureCylindrical
position = '1 0 1.75'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
widths = '${hx_wall_thickness}'
n_part_elems = '3'
solid_properties = 'steel'
solid_properties_T_ref = '300'
names = '0'
inner_radius = '${fparse hx_dia_inner / 2.}'
[]
[ht_sec]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = outer
flow_channel = hx/sec
P_hf = '${fparse 2 * pi * hx_radius_wall}'
[]
[sec]
type = FlowChannel1Phase
position = '${fparse 1 + hx_wall_thickness} 0 0.25'
orientation = '0 0 1'
length = ${hx_length}
n_elems = ${hx_n_elems}
A = '${fparse pi * (hx_dia_outer * hx_dia_outer / 4. - hx_radius_wall * hx_radius_wall)}'
D_h = '${fparse hx_dia_outer - (2 * hx_radius_wall)}'
fp = water
initial_T = 300
[]
[]
[jct7]
type = JunctionParallelChannels1Phase
position = '1 0 0.5'
connections = 'hx/pri:out down_pipe_2:in'
volume = 1e-5
[]
[down_pipe_2]
type = FlowChannel1Phase
position = '1 0 0.25'
orientation = '0 0 -1'
length = 0.25
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct8]
type = JunctionOneToOne1Phase
connections = 'down_pipe_2:out bottom_1:in'
[]
[bottom_1]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[pump]
type = Pump1Phase
position = '0.5 0 0'
connections = 'bottom_1:out bottom_2:in'
volume = 1e-4
A_ref = ${A_pipe}
head = 0
[]
[bottom_2]
type = FlowChannel1Phase
position = '0.5 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct9]
type = JunctionOneToOne1Phase
connections = 'bottom_2:out up_pipe_1:in'
[]
[inlet_sec]
type = InletMassFlowRateTemperature1Phase
input = 'hx/sec:in'
m_dot = 0
T = 300
[]
[outlet_sec]
type = Outlet1Phase
input = 'hx/sec:out'
p = 1e5
[]
[]
[ControlLogic]
[set_point]
type = GetFunctionValueControl
function = ${m_dot_in}
[]
[pid]
type = PIDControl
initial_value = 0.0
set_point = set_point:value
input = m_dot_pump
K_p = 1.
K_i = 4.
K_d = 0
[]
[set_pump_head]
type = SetComponentRealValueControl
component = pump
parameter = head
value = pid:output
[]
[m_dot_sec_inlet_ctrl]
type = GetFunctionValueControl
function = m_dot_sec_fn
[]
[set_m_dot_sec_ctrl]
type = SetComponentRealValueControl
component = inlet_sec
parameter = m_dot
value = m_dot_sec_inlet_ctrl:value
[]
[]
[Postprocessors]
[power_to_coolant]
type = ADHeatRateConvection1Phase
block = core_chan
P_hf = '${fparse pi *core_dia}'
[]
[m_dot_pump]
type = ADFlowJunctionFlux1Phase
boundary = core_chan:in
connection_index = 1
equation = mass
junction = jct7
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[core_p_in]
type = SideAverageValue
boundary = core_chan:in
variable = p
[]
[core_p_out]
type = SideAverageValue
boundary = core_chan:out
variable = p
[]
[core_delta_p]
type = ParsedPostprocessor
pp_names = 'core_p_in core_p_out'
expression = 'core_p_in - core_p_out'
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = hx/pri:out
variable = T
[]
[hx_sec_T_in]
type = SideAverageValue
boundary = inlet_sec
variable = T
[]
[hx_sec_T_out]
type = SideAverageValue
boundary = outlet_sec
variable = T
[]
[m_dot_sec]
type = ADFlowBoundaryFlux1Phase
boundary = inlet_sec
equation = mass
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = IterationAdaptiveDT
dt = 1
[]
dtmax = 5
end_time = 500
line_search = basic
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 25
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/xfem/test/tests/moving_interface/verification/1D_xy_discrete2mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: quasi-1D
# Coordinate System: xy
# Material Numbers/Types:discrete homog 2 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description
# A transient heat transfer problem in Cartesian coordinates designed with
# the Method of Manufactured Solutions. This problem was developed to verify
# XFEM performance in the presence of a moving interface separating two
# discrete material regions for linear element models. Both the temperature
# solution and level set function are designed to be linear to attempt to
# minimize error between the exact solution and XFEM results. Thermal
# conductivity, density, and heat capacity are homogeneous in each material
# region with a discontinuous jump in thermal flux between the two material
# regions.
# Results:
# The temperature at the left boundary is determined by the analytical
# solution, so temperature at the right boundary (x=1) should exhibit the
# largest difference between the analytical solution and XFEM results. We
# present the analytical and XFEM results at the material interface position
# and right side boundary at various times.
# Interface:
# Time Expected Temperature XFEM Calculated Temperature
# 20 746.75 746.7235521
# 40 893.05 893.0379081
# 60 1040.15 1040.1527530
#
# Right Boundary (x=1):
# Time Expected Temperature XFEM Calculated Temperature
# 20 720 719.9708681
# 40 840 839.9913293
# 60 960 960.0100886
#
# IMPORTANT NOTE:
# When running this input file, add the --allow-test-objects tag!!!
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 0.5
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = phi
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./phi]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = 'diffusion_coefficient'
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = phi
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
jump_flux = jump_flux_func
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = 'phi:=(0.75-x-0.001*t);
i:=(0.75-0.001*t);
if (phi>=0,
10*(8-x),
(7/(1-i))*((i-2)*x + (8-7*i)) )'
[../]
[./right_du_func]
type = ParsedFunction
expression = 'i:=(0.75-0.001*t);
(2.0/(1-i))*(-5+5*i+i*t-2*t)'
[../]
[./exact_u_func]
type = ParsedFunction
expression = 'phi:=(0.75-x-0.001*t);
i:=(0.75-0.001*t);
if (phi>=0,
605 - 5*x + t*(8-x),
(1/(1-i))*((-5+5*i+i*t-2*t)*x + (605-605*i+8*t-7*t*i)) )'
[../]
[./jump_flux_func]
type = ParsedFunction
expression = 'i:=(0.75-0.001*t);
k_1:=(20.0);
k_2:=(2.0);
k_1*(5+t) + (k_2/(1-i))*(-5+5*i+i*t-2*t)'
[../]
[./ls_func]
type = ParsedFunction
expression = '0.75 - x - 0.001*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'A_rhoCp B_rhoCp'
prop_values = '10 7'
[../]
[./therm_cond_prop]
type = GenericConstantMaterial
prop_names = 'A_diffusion_coefficient B_diffusion_coefficient'
prop_values = '20.0 2.0'
[../]
[./combined_rhoCp]
type = LevelSetBiMaterialReal
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = phi
prop_name = rhoCp
[../]
[./combined_diffusion_coefficient]
type = LevelSetBiMaterialReal
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = phi
prop_name = diffusion_coefficient
[../]
[]
[BCs]
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 'left'
function = exact_u_func
[../]
[./right_du]
type = FunctionNeumannBC
variable = u
boundary = 'right'
function = right_du_func
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 600
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
# petsc_options_iname = '-pc_type -pc_hypre_type'
# petsc_options_value = 'hypre boomeramg'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 20
end_time = 60.0
max_xfem_update = 2
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/corner_nodes_cut/notch.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '-0.26 0.0 0.0 0.1'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Mesh]
file = notch.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[BCs]
[./top_x]
type = DirichletBC
boundary = 102
variable = disp_x
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 102
variable = disp_y
value = 0.1
[../]
[./bottom_y]
type = DirichletBC
boundary = 101
variable = disp_y
value = -0.1
[../]
[./bottom_x]
type = DirichletBC
boundary = 101
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_3/brick3_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick3_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x28]
type = NodalVariableValue
nodeid = 27
variable = disp_x
[../]
[./disp_x33]
type = NodalVariableValue
nodeid = 32
variable = disp_x
[../]
[./disp_y28]
type = NodalVariableValue
nodeid = 27
variable = disp_y
[../]
[./disp_y33]
type = NodalVariableValue
nodeid = 32
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-7
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x28 disp_y28 disp_x33 disp_y33 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+7
al_penetration_tolerance = 1e-8
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/stationary_jump.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0.5
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = single_point_2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./appl_disp]
type = PiecewiseLinear
x = '0 0.001 0.101'
y = '0 0.0 -0.10'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = appl_disp
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.002001
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputePlaneFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputePlaneFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[./disp_y]
type = NodalVariableValue
nodeid = 5
variable = disp_y
[../]
[./inc_slip_x]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_x
[../]
[./inc_slip_y]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_y
[../]
[./accum_slip_x]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_x
[../]
[./accum_slip_y]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -mat_superlu_dist_iterrefine'
petsc_options_value = 'lu superlu_dist 1'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.001
num_steps = 10000
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
file_base = single_point_2d_out_glued_kin
print_linear_residuals = true
perf_graph = true
csv = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = glued
formulation = kinematic
penalty = 1e12
normalize_penalty = true
tangential_tolerance = 1e-3
[../]
[]
(modules/porous_flow/test/tests/sinks/s09_fully_saturated.i)
# Apply a piecewise-linear sink flux to the right-hand side and watch fluid flow to it
#
# This test has a single phase with two components. The test initialises with
# the porous material fully filled with component=1. The left-hand side is fixed
# at porepressure=1 and mass-fraction of the zeroth component being unity.
# The right-hand side has a very strong piecewise-linear flux that keeps the
# porepressure~0 at that side. Fluid mass is extracted by this flux in proportion
# to the fluid component mass fraction.
#
# Therefore, the zeroth fluid component will flow from left to right (down the
# pressure gradient).
#
# The important DE is
# porosity * dc/dt = (perm / visc) * grad(P) * grad(c)
# which is true for c = mass-fraction, and very large bulk modulus of the fluid.
# For grad(P) constant in time and space (as in this example) this is just the
# advection equation for c, with velocity = perm / visc / porosity. The parameters
# are chosen to velocity = 1 m/s.
# In the numerical world, and especially with full upwinding, the advection equation
# suffers from diffusion. In this example, the diffusion is obvious when plotting
# the mass-fraction along the line, but the average velocity of the front is still
# correct at 1 m/s.
# This test uses the FullySaturated version of the flow Kernel. This does not
# suffer from as much numerical diffusion as the standard PorousFlow Kernel since
# it does not employ any upwinding.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = 0
xmax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp frac'
number_fluid_phases = 1
number_fluid_components = 2
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Variables]
[pp]
[]
[frac]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = 1-x
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = frac
[]
[mass1]
type = PorousFlowMassTimeDerivative
fluid_component = 1
variable = pp
[]
[flux0]
type = PorousFlowFullySaturatedDarcyFlow
fluid_component = 0
gravity = '0 0 0'
variable = frac
[]
[flux1]
type = PorousFlowFullySaturatedDarcyFlow
fluid_component = 1
gravity = '0 0 0'
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e10 # need large in order for constant-velocity advection
density0 = 1 # almost irrelevant, except that the ability of the right BC to keep P fixed at zero is related to density_P0
thermal_expansion = 0
viscosity = 11
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
mass_fraction_vars = frac
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.1 0 0 0 1.1 0 0 0 1.1'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2 # irrelevant in this fully-saturated situation
phase = 0
[]
[]
[BCs]
[lhs_fixed_a]
type = DirichletBC
boundary = 'left'
variable = frac
value = 1
[]
[lhs_fixed_b]
type = DirichletBC
boundary = 'left'
variable = pp
value = 1
[]
[flux0]
type = PorousFlowPiecewiseLinearSink
boundary = 'right'
pt_vals = '-100 100'
multipliers = '-1 1'
variable = frac # the zeroth comonent
mass_fraction_component = 0
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1E4
[]
[flux1]
type = PorousFlowPiecewiseLinearSink
boundary = 'right'
pt_vals = '-100 100'
multipliers = '-1 1'
variable = pp # comonent 1
mass_fraction_component = 1
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1E4
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-2
end_time = 1
nl_rel_tol = 1E-11
nl_abs_tol = 1E-11
[]
[VectorPostprocessors]
[mf]
type = LineValueSampler
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 100
sort_by = x
variable = frac
[]
[]
[Outputs]
file_base = s09_fully_saturated
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
sync_times = '0.1 0.5 1'
sync_only = true
[]
time_step_interval = 10
[]
(modules/xfem/test/tests/diffusion_xfem/levelsetcut3d.i)
# 3D: Mesh is cut by level set based cutter
# The level set is a MOOSE auxvariable
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 1.0
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[./ls_func]
type = ParsedFunction
expression = 'sqrt(x*x + y*y + z*z) - 0.5'
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 2
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/outputs/console/console_print_toggles.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
# This block is needed so cli_args in the tests files is available
[./console]
type = Console
[../]
[]
(modules/contact/test/tests/fieldsplit/2blocks3d.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[Mesh]
file = 2blocks3d.e
patch_size = 5
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
add_variables = true
[../]
[]
[AuxVariables]
[./penetration]
order = FIRST
family = LAGRANGE
[../]
[]
[Functions]
[./horizontal_movement]
type = ParsedFunction
expression = t/10.0
[../]
[]
[AuxKernels]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 2
paired_boundary = 3
order = FIRST
[../]
[]
[BCs]
[./push_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 1
function = horizontal_movement
[../]
[./fix_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = 0.0
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = '1 4'
value = 0.0
[../]
[./fix_z]
type = DirichletBC
variable = disp_z
boundary = '1 4'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor_left]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stress_left]
type = ComputeFiniteStrainElasticStress
block = 1
[../]
[./elasticity_tensor_right]
type = ComputeIsotropicElasticityTensor
block = 2
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stress_right]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Contact]
[./leftright]
secondary = 2
primary = 3
model = frictionless
penalty = 1e+6
normalize_penalty = true
formulation = kinematic
normal_smoothing_distance = 0.1
[../]
[]
[Preconditioning]
[./FSP]
type = FSP
# It is the starting point of splitting
topsplit = 'contact_interior' # 'contact_interior' should match the following block name
[./contact_interior]
splitting = 'contact interior'
splitting_type = multiplicative
[../]
[./interior]
type = ContactSplit
vars = 'disp_x disp_y disp_z'
uncontact_primary = '3'
uncontact_secondary = '2'
uncontact_displaced = '1'
blocks = '1 2'
include_all_contact_nodes = 1
petsc_options_iname = '-ksp_type -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = 'preonly hypre boomeramg 1 0.25'
[../]
[./contact]
type = ContactSplit
vars = 'disp_x disp_y disp_z'
contact_primary = '3'
contact_secondary = '2'
contact_displaced = '1'
include_all_contact_nodes = 1
petsc_options_iname = '-ksp_type -pc_type -pc_asm_overlap -sub_pc_type'
petsc_options_value = 'preonly asm 1 lu'
[../]
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
dt = 0.1
dtmin = 0.1
end_time = 0.1
l_tol = 1e-4
l_max_its = 100
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
nl_max_its = 100
[]
[Outputs]
file_base = 2blocks3d_out
[./exodus]
type = Exodus
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
(modules/porous_flow/test/tests/sinks/s03.i)
# apply a sink flux with use_relperm=true and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1.1
[]
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = -y
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.2 0 0 0 0.1 0 0 0 0.1'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[xval]
[]
[yval]
[]
[]
[ICs]
[xval]
type = FunctionIC
variable = xval
function = x
[]
[yval]
type = FunctionIC
variable = yval
function = y
[]
[]
[Functions]
[mass00]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)*pow(1+pow(-al*pp,1.0/(1-m)),-m)'
symbol_names = 'vol por dens0 pp bulk al m'
symbol_values = '0.25 0.1 1.1 p00 1.3 1.1 0.5'
[]
[sat00]
type = ParsedFunction
expression = 'pow(1+pow(-al*pp,1.0/(1-m)),-m)'
symbol_names = 'pp al m'
symbol_values = 'p00 1.1 0.5'
[]
[mass01]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)*pow(1+pow(-al*pp,1.0/(1-m)),-m)'
symbol_names = 'vol por dens0 pp bulk al m'
symbol_values = '0.25 0.1 1.1 p01 1.3 1.1 0.5'
[]
[expected_mass_change00]
type = ParsedFunction
expression = 'fcn*pow(pow(1+pow(-al*pp,1.0/(1-m)),-m),2)*area*dt'
symbol_names = 'fcn perm dens0 pp bulk visc area dt al m'
symbol_values = '6 0.2 1.1 p00 1.3 1.1 0.5 1E-3 1.1 0.5'
[]
[expected_mass_change01]
type = ParsedFunction
expression = 'fcn*pow(pow(1+pow(-al*pp,1.0/(1-m)),-m),2)*area*dt'
symbol_names = 'fcn perm dens0 pp bulk visc area dt al m'
symbol_values = '6 0.2 1.1 p01 1.3 1.1 0.5 1E-3 1.1 0.5'
[]
[mass00_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm00_prev del_m00'
[]
[mass01_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm01_prev del_m01'
[]
[sat01]
type = ParsedFunction
expression = 'pow(1+pow(-al*pp,1.0/(1-m)),-m)'
symbol_names = 'pp al m'
symbol_values = 'p01 1.1 0.5'
[]
[expected_mass_change_rate]
type = ParsedFunction
expression = 'fcn*pow(pow(1+pow(-al*pp,1.0/(1-m)),-m),2)*area'
symbol_names = 'fcn perm dens0 pp bulk visc area dt al m'
symbol_values = '6 0.2 1.1 p00 1.3 1.1 0.5 1E-3 1.1 0.5'
[]
[]
[Postprocessors]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m00]
type = FunctionValuePostprocessor
function = mass00
execute_on = 'initial timestep_end'
[]
[m00_prev]
type = FunctionValuePostprocessor
function = mass00
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m00]
type = FunctionValuePostprocessor
function = expected_mass_change00
execute_on = 'timestep_end'
outputs = 'console'
[]
[m00_expect]
type = FunctionValuePostprocessor
function = mass00_expect
execute_on = 'timestep_end'
[]
[p10]
type = PointValue
point = '1 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m01]
type = FunctionValuePostprocessor
function = mass01
execute_on = 'initial timestep_end'
[]
[m01_prev]
type = FunctionValuePostprocessor
function = mass01
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m01]
type = FunctionValuePostprocessor
function = expected_mass_change01
execute_on = 'timestep_end'
outputs = 'console'
[]
[m01_expect]
type = FunctionValuePostprocessor
function = mass01_expect
execute_on = 'timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[s00]
type = FunctionValuePostprocessor
function = sat00
execute_on = 'initial timestep_end'
[]
[mass00_rate]
type = FunctionValuePostprocessor
function = expected_mass_change_rate
execute_on = 'initial timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowSink
boundary = 'left'
variable = pp
use_mobility = false
use_relperm = true
fluid_phase = 0
flux_function = 6
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-3
end_time = 0.018
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s03
[console]
type = Console
execute_on = 'nonlinear linear'
time_step_interval = 5
[]
[csv]
type = CSV
execute_on = 'timestep_end'
time_step_interval = 2
[]
[]
(test/tests/time_integrators/actually_explicit_euler_verification/ee-2d-linear-adapt.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = (x+y)
[../]
[./exact_fn]
type = ParsedFunction
expression = t*(x+y)
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Adaptivity]
steps = 1
marker = box
max_h_level = 2
[./Markers]
[./box]
bottom_left = '-0.4 -0.4 0'
inside = refine
top_right = '0.4 0.4 0'
outside = do_nothing
type = BoxMarker
[../]
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
start_time = 0.0
num_steps = 4
dt = 0.005
l_tol = 1e-12
[./TimeIntegrator]
type = ActuallyExplicitEuler
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/1D_rz_lsdep1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: quasi-1D
# Coordinate System: rz
# Material Numbers/Types: level set dep 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# A simple transient heat transfer problem in cylindrical coordinates designed
# with the Method of Manufactured Solutions. This problem was developed to
# verify XFEM performance in the presence of a moving interface for linear
# element models that can be exactly evaluated by FEM/Moose. Both the
# temperature solution and level set function are designed to be linear to
# attempt to minimize error between the Moose/exact solution and XFEM results.
# Thermal conductivity is dependent upon the value of the level set function
# at each timestep.
# Results:
# The temperature at the left boundary (x=1) exhibits the largest difference
# between the FEM/Moose solution and XFEM results. We present the XFEM
# results at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 480.0008131
# 0.6 520 520.0038333
# 0.8 560 560.0088286
# 1.0 600 600.0131612
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 1
xmin = 1.0
xmax = 2.0
ymin = 0.0
ymax = 0.5
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-200*x+400) + (1/x)*(310*t - (10/1.02)*x*t - (1/1.02)*t^2)'
[../]
[./neumann_func]
type = ParsedFunction
expression = '((0.05/2.04)*(2.04-x-0.2*t) + 1.5)*200*t'
[../]
[./k_func]
type = ParsedFunction
expression = '(0.05/2.04)*(2.04-x-0.2*t) + 1.5'
[../]
[./ls_func]
type = ParsedFunction
expression = '2.04 - x -0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericFunctionMaterial
prop_names = 'diffusion_coefficient'
prop_values = 'k_func'
[../]
[]
[BCs]
[./left_u]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 'right'
value = 400
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/examples/phase_field-mechanics/kks_mechanics_VTS.i)
# KKS phase-field model coupled with elasticity using the Voigt-Taylor scheme as
# described in L.K. Aagesen et al., Computational Materials Science, 140, 10-21 (2017)
# Original run #170329e
[Mesh]
type = GeneratedMesh
dim = 3
nx = 640
ny = 1
nz = 1
xmin = -10
xmax = 10
ymin = 0
ymax = 0.03125
zmin = 0
zmax = 0.03125
elem_type = HEX8
[]
[Variables]
# order parameter
[./eta]
order = FIRST
family = LAGRANGE
[../]
# solute concentration
[./c]
order = FIRST
family = LAGRANGE
[../]
# chemical potential
[./w]
order = FIRST
family = LAGRANGE
[../]
# solute phase concentration (matrix)
[./cm]
order = FIRST
family = LAGRANGE
[../]
# solute phase concentration (precipitate)
[./cp]
order = FIRST
family = LAGRANGE
[../]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./eta_ic]
variable = eta
type = FunctionIC
function = ic_func_eta
block = 0
[../]
[./c_ic]
variable = c
type = FunctionIC
function = ic_func_c
block = 0
[../]
[./w_ic]
variable = w
type = ConstantIC
value = 0.00991
block = 0
[../]
[./cm_ic]
variable = cm
type = ConstantIC
value = 0.131
block = 0
[../]
[./cp_ic]
variable = cp
type = ConstantIC
value = 0.236
block = 0
[../]
[]
[Functions]
[./ic_func_eta]
type = ParsedFunction
expression = '0.5*(1.0+tanh((x)/delta_eta/sqrt(2.0)))'
symbol_names = 'delta_eta'
symbol_values = '0.8034'
[../]
[./ic_func_c]
type = ParsedFunction
expression = '0.2388*(0.5*(1.0+tanh(x/delta/sqrt(2.0))))^3*(6*(0.5*(1.0+tanh(x/delta/sqrt(2.0))))^2-15*(0.5*(1.0+tanh(x/delta/sqrt(2.0))))+10)+0.1338*(1-(0.5*(1.0+tanh(x/delta/sqrt(2.0))))^3*(6*(0.5*(1.0+tanh(x/delta/sqrt(2.0))))^2-15*(0.5*(1.0+tanh(x/delta/sqrt(2.0))))+10))'
symbol_names = 'delta'
symbol_values = '0.8034'
[../]
[./psi_eq_int]
type = ParsedFunction
expression = 'volume*psi_alpha'
symbol_names = 'volume psi_alpha'
symbol_values = 'volume psi_alpha'
[../]
[./gamma]
type = ParsedFunction
expression = '(psi_int - psi_eq_int) / dy / dz'
symbol_names = 'psi_int psi_eq_int dy dz'
symbol_values = 'psi_int psi_eq_int 0.03125 0.03125'
[../]
[]
[AuxVariables]
[./sigma11]
order = CONSTANT
family = MONOMIAL
[../]
[./sigma22]
order = CONSTANT
family = MONOMIAL
[../]
[./sigma33]
order = CONSTANT
family = MONOMIAL
[../]
[./e11]
order = CONSTANT
family = MONOMIAL
[../]
[./e12]
order = CONSTANT
family = MONOMIAL
[../]
[./e22]
order = CONSTANT
family = MONOMIAL
[../]
[./e33]
order = CONSTANT
family = MONOMIAL
[../]
[./e_el11]
order = CONSTANT
family = MONOMIAL
[../]
[./e_el12]
order = CONSTANT
family = MONOMIAL
[../]
[./e_el22]
order = CONSTANT
family = MONOMIAL
[../]
[./f_el]
order = CONSTANT
family = MONOMIAL
[../]
[./eigen_strain00]
order = CONSTANT
family = MONOMIAL
[../]
[./Fglobal]
order = CONSTANT
family = MONOMIAL
[../]
[./psi]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_sigma11]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = sigma11
[../]
[./matl_sigma22]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = sigma22
[../]
[./matl_sigma33]
type = RankTwoAux
rank_two_tensor = stress
index_i = 2
index_j = 2
variable = sigma33
[../]
[./matl_e11]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 0
index_j = 0
variable = e11
[../]
[./matl_e12]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 0
index_j = 1
variable = e12
[../]
[./matl_e22]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 1
index_j = 1
variable = e22
[../]
[./matl_e33]
type = RankTwoAux
rank_two_tensor = total_strain
index_i = 2
index_j = 2
variable = e33
[../]
[./f_el]
type = MaterialRealAux
variable = f_el
property = f_el_mat
execute_on = timestep_end
[../]
[./GlobalFreeEnergy]
variable = Fglobal
type = KKSGlobalFreeEnergy
fa_name = fm
fb_name = fp
w = 0.0264
kappa_names = kappa
interfacial_vars = eta
[../]
[./psi_potential]
variable = psi
type = ParsedAux
coupled_variables = 'Fglobal w c f_el sigma11 e11'
expression = 'Fglobal - w*c + f_el - sigma11*e11'
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value = 0
[../]
[./front_y]
type = DirichletBC
variable = disp_y
boundary = front
value = 0
[../]
[./back_y]
type = DirichletBC
variable = disp_y
boundary = back
value = 0
[../]
[./top_z]
type = DirichletBC
variable = disp_z
boundary = top
value = 0
[../]
[./bottom_z]
type = DirichletBC
variable = disp_z
boundary = bottom
value = 0
[../]
[]
[Materials]
# Chemical free energy of the matrix
[./fm]
type = DerivativeParsedMaterial
property_name = fm
coupled_variables = 'cm'
expression = '6.55*(cm-0.13)^2'
[../]
# Elastic energy of the matrix
[./elastic_free_energy_m]
type = ElasticEnergyMaterial
base_name = matrix
f_name = fe_m
args = ' '
outputs = exodus
[../]
# Total free energy of the matrix
[./Total_energy_matrix]
type = DerivativeSumMaterial
property_name = f_total_matrix
sum_materials = 'fm fe_m'
coupled_variables = 'cm'
[../]
# Free energy of the precipitate phase
[./fp]
type = DerivativeParsedMaterial
property_name = fp
coupled_variables = 'cp'
expression = '6.55*(cp-0.235)^2'
[../]
# Elastic energy of the precipitate
[./elastic_free_energy_p]
type = ElasticEnergyMaterial
base_name = ppt
f_name = fe_p
args = ' '
outputs = exodus
[../]
# Total free energy of the precipitate
[./Total_energy_ppt]
type = DerivativeSumMaterial
property_name = f_total_ppt
sum_materials = 'fp fe_p'
coupled_variables = 'cp'
[../]
# Total elastic energy
[./Total_elastic_energy]
type = DerivativeTwoPhaseMaterial
eta = eta
f_name = f_el_mat
fa_name = fe_m
fb_name = fe_p
outputs = exodus
W = 0
[../]
# h(eta)
[./h_eta]
type = SwitchingFunctionMaterial
h_order = HIGH
eta = eta
[../]
# g(eta)
[./g_eta]
type = BarrierFunctionMaterial
g_order = SIMPLE
eta = eta
[../]
# constant properties
[./constants]
type = GenericConstantMaterial
prop_names = 'M L kappa misfit'
prop_values = '0.7 0.7 0.01704 0.00377'
[../]
#Mechanical properties
[./Stiffness_matrix]
type = ComputeElasticityTensor
C_ijkl = '103.3 74.25 74.25 103.3 74.25 103.3 46.75 46.75 46.75'
base_name = matrix
fill_method = symmetric9
[../]
[./Stiffness_ppt]
type = ComputeElasticityTensor
C_ijkl = '100.7 71.45 71.45 100.7 71.45 100.7 50.10 50.10 50.10'
base_name = ppt
fill_method = symmetric9
[../]
[./stress_matrix]
type = ComputeLinearElasticStress
base_name = matrix
[../]
[./stress_ppt]
type = ComputeLinearElasticStress
base_name = ppt
[../]
[./strain_matrix]
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
base_name = matrix
[../]
[./strain_ppt]
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
base_name = ppt
eigenstrain_names = 'eigenstrain_ppt'
[../]
[./eigen_strain]
type = ComputeEigenstrain
base_name = ppt
eigen_base = '1 1 1 0 0 0'
prefactor = misfit
eigenstrain_name = 'eigenstrain_ppt'
[../]
[./global_stress]
type = TwoPhaseStressMaterial
base_A = matrix
base_B = ppt
[../]
[./global_strain]
type = ComputeSmallStrain
displacements = 'disp_x disp_y disp_z'
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y disp_z'
[../]
# enforce c = (1-h(eta))*cm + h(eta)*cp
[./PhaseConc]
type = KKSPhaseConcentration
ca = cm
variable = cp
c = c
eta = eta
[../]
# enforce pointwise equality of chemical potentials
[./ChemPotVacancies]
type = KKSPhaseChemicalPotential
variable = cm
cb = cp
fa_name = f_total_matrix
fb_name = f_total_ppt
[../]
#
# Cahn-Hilliard Equation
#
[./CHBulk]
type = KKSSplitCHCRes
variable = c
ca = cm
fa_name = f_total_matrix
w = w
[../]
[./dcdt]
type = CoupledTimeDerivative
variable = w
v = c
[../]
[./ckernel]
type = SplitCHWRes
mob_name = M
variable = w
[../]
#
# Allen-Cahn Equation
#
[./ACBulkF]
type = KKSACBulkF
variable = eta
fa_name = f_total_matrix
fb_name = f_total_ppt
w = 0.0264
args = 'cp cm'
[../]
[./ACBulkC]
type = KKSACBulkC
variable = eta
ca = cm
cb = cp
fa_name = f_total_matrix
[../]
[./ACInterface]
type = ACInterface
variable = eta
kappa_name = kappa
[../]
[./detadt]
type = TimeDerivative
variable = eta
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'asm ilu nonzero'
l_max_its = 30
nl_max_its = 10
l_tol = 1.0e-4
nl_rel_tol = 1.0e-8
nl_abs_tol = 1.0e-11
num_steps = 200
[./TimeStepper]
type = SolutionTimeAdaptiveDT
dt = 0.5
[../]
[]
[VectorPostprocessors]
#[./eta]
# type = LineValueSampler
# start_point = '-10 0 0'
# end_point = '10 0 0'
# variable = eta
# num_points = 321
# sort_by = id
#[../]
#[./eta_position]
# type = FindValueOnLineSample
# vectorpostprocessor = eta
# variable_name = eta
# search_value = 0.5
#[../]
# [./f_el]
# type = LineMaterialRealSampler
# start = '-20 0 0'
# end = '20 0 0'
# sort_by = id
# property = f_el
# [../]
# [./f_el_a]
# type = LineMaterialRealSampler
# start = '-20 0 0'
# end = '20 0 0'
# sort_by = id
# property = fe_m
# [../]
# [./f_el_b]
# type = LineMaterialRealSampler
# start = '-20 0 0'
# end = '20 0 0'
# sort_by = id
# property = fe_p
# [../]
# [./h_out]
# type = LineMaterialRealSampler
# start = '-20 0 0'
# end = '20 0 0'
# sort_by = id
# property = h
# [../]
# [./fm_out]
# type = LineMaterialRealSampler
# start = '-20 0 0'
# end = '20 0 0'
# sort_by = id
# property = fm
# [../]
[]
[Postprocessors]
[./f_el_int]
type = ElementIntegralMaterialProperty
mat_prop = f_el_mat
[../]
[./c_alpha]
type = SideAverageValue
boundary = left
variable = c
[../]
[./c_beta]
type = SideAverageValue
boundary = right
variable = c
[../]
[./e11_alpha]
type = SideAverageValue
boundary = left
variable = e11
[../]
[./e11_beta]
type = SideAverageValue
boundary = right
variable = e11
[../]
[./s11_alpha]
type = SideAverageValue
boundary = left
variable = sigma11
[../]
[./s22_alpha]
type = SideAverageValue
boundary = left
variable = sigma22
[../]
[./s33_alpha]
type = SideAverageValue
boundary = left
variable = sigma33
[../]
[./s11_beta]
type = SideAverageValue
boundary = right
variable = sigma11
[../]
[./s22_beta]
type = SideAverageValue
boundary = right
variable = sigma22
[../]
[./s33_beta]
type = SideAverageValue
boundary = right
variable = sigma33
[../]
[./f_el_alpha]
type = SideAverageValue
boundary = left
variable = f_el
[../]
[./f_el_beta]
type = SideAverageValue
boundary = right
variable = f_el
[../]
[./f_c_alpha]
type = SideAverageValue
boundary = left
variable = Fglobal
[../]
[./f_c_beta]
type = SideAverageValue
boundary = right
variable = Fglobal
[../]
[./chem_pot_alpha]
type = SideAverageValue
boundary = left
variable = w
[../]
[./chem_pot_beta]
type = SideAverageValue
boundary = right
variable = w
[../]
[./psi_alpha]
type = SideAverageValue
boundary = left
variable = psi
[../]
[./psi_beta]
type = SideAverageValue
boundary = right
variable = psi
[../]
[./total_energy]
type = ElementIntegralVariablePostprocessor
variable = Fglobal
[../]
# Get simulation cell size from postprocessor
[./volume]
type = ElementIntegralMaterialProperty
mat_prop = 1
[../]
[./psi_eq_int]
type = FunctionValuePostprocessor
function = psi_eq_int
[../]
[./psi_int]
type = ElementIntegralVariablePostprocessor
variable = psi
[../]
[./gamma]
type = FunctionValuePostprocessor
function = gamma
[../]
[]
#
# Precondition using handcoded off-diagonal terms
#
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Outputs]
[./exodus]
type = Exodus
time_step_interval = 20
[../]
[./csv]
type = CSV
execute_on = 'final'
[../]
#[./console]
# type = Console
# output_file = true
# [../]
[]
(modules/solid_mechanics/test/tests/material_limit_time_step/creep/nafems_test5a_lim.i)
[GlobalParams]
temperature = temp
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane1_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
group_variables = 'disp_x disp_y'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./temp]
initial_condition = 1500.0
[../]
[./creep]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./invariant3]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[SolidMechanics]
use_displaced_mesh = true
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./creep_aux]
type = MaterialRealAux
property = effective_creep_strain
variable = creep
[../]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
[../]
[./invariant3]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = invariant3
scalar_type = ThirdInvariant
[../]
[./creep_strain_xx]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
[../]
[./creep_strain_yy]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
[../]
[./creep_strain_zz]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_zz
index_i = 2
index_j = 2
[../]
[./creep_strain_xy]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xy
index_i = 0
index_j = 1
[../]
[./elastic_str_xx_aux]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
[../]
[./elastic_str_yy_aux]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
[../]
[./elastic_str_zz_aux]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 3
factor = -100.0
[../]
[./side_press]
type = Pressure
variable = disp_x
boundary = 4
factor = -200.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 200e3
poissons_ratio = 0.3
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
block = 1
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
block = 1
coefficient = 3.125e-14
n_exponent = 5.0
m_exponent = 0.0
activation_energy = 0.0
max_inelastic_increment = 0.01
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = ' lu superlu_dist'
line_search = 'none'
l_max_its = 50
nl_max_its = 100
end_time = 1000.0
num_steps = 10000
l_tol = 1e-3
[./TimeStepper]
type = IterationAdaptiveDT
dt = 1e-6
time_t = '1e-6 2e-6 3e-6 5e-6 9e-6 1.7e-5 3.3e-5 6.5e-5 1.29e-4 2.57e-4 5.13e-4 1.025e-3 2.049e-3 4.097e-3 8.193e-3 1.638e-2 3.276e-2 5.734e-2 0.106 0.180 0.291 0.457 0.706 1.08 1.64 2.48 3.74 5.63 8.46 12.7 19.1 28.7 43.0 64.5 108.0 194.0 366.0 710.0 1000.0'
time_dt = '1e-6 1e-6 2e-6 4e-6 8e-6 1.6e-5 3.2e-5 6.4e-5 1.28e-4 2.56e-4 5.12e-4 1.024e-3 2.048e-3 4.096e-3 8.192e-3 1.6384e-2 2.458e-2 4.915e-2 7.40e-2 0.111 0.166 0.249 0.374 0.560 0.840 1.26 1.89 2.83 4.25 6.40 9.6 14.3 21.5 43.0 86.1 172.0 344.0 290.0 290.0'
optimal_iterations = 30
iteration_window = 9
growth_factor = 2.0
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
[../]
[]
[Postprocessors]
[./matl_ts_min]
type = MaterialTimeStepPostprocessor
[../]
[./sigma_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./invariant3]
type = ElementAverageValue
variable = invariant3
[../]
[./eps_crp_xx]
type = ElementAverageValue
variable = creep_strain_xx
[../]
[./eps_crp_yy]
type = ElementAverageValue
variable = creep_strain_yy
[../]
[./eps_crp_zz]
type = ElementAverageValue
variable = creep_strain_zz
[../]
[./eps_crp_mag]
type = ElementAverageValue
variable = creep
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x3]
type = NodalVariableValue
nodeid = 2
variable = disp_x
[../]
[./disp_y3]
type = NodalVariableValue
nodeid = 2
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./elas_str_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./elas_str_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./elas_str_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
csv = true
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 25
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_4/brick4_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick4_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x59]
type = NodalVariableValue
nodeid = 58
variable = disp_x
[../]
[./disp_x64]
type = NodalVariableValue
nodeid = 63
variable = disp_x
[../]
[./disp_y59]
type = NodalVariableValue
nodeid = 58
variable = disp_y
[../]
[./disp_y64]
type = NodalVariableValue
nodeid = 63
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x59 disp_y59 disp_x64 disp_y64 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(test/tests/userobjects/toggle_mesh_adaptivity/toggle_mesh_adaptivity_gaussian_ic_stop_time.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./gaussian_ic]
type = FunctionIC
variable = u
function = gaussian_2d
[../]
[]
[Functions]
[./gaussian_2d]
type = ParsedFunction
expression = exp(-((x-x0)*(x-x0)+(y-y0)*(y-y0))/2.0/sigma/sigma)
symbol_names = 'sigma x0 y0'
symbol_values = '0.05 0.35 0.25'
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.02
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Transient
num_steps = 4
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
initial_steps = 1
initial_marker = marker
cycles_per_step = 1
marker = marker
max_h_level = 2
stop_time = 0.0
[./Markers]
[./marker]
type = CircleMarker
point = '0.35 0.25 0'
radius = 0.2
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(test/tests/userobjects/toggle_mesh_adaptivity/toggle_mesh_adaptivity.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Transient
num_steps = 4
dt = 0.1
[]
[Adaptivity]
cycles_per_step = 1
marker = marker
max_h_level = 2
[./Markers]
[./marker]
type = BoxMarker
bottom_left = '0.35 0.25 0'
top_right = '0.5 0.5 0'
inside = refine
outside = coarsen
[../]
[../]
[]
[UserObjects]
[./mesh_adaptivity_off]
type = ToggleMeshAdaptivity
mesh_adaptivity = 'off'
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_4/brick4_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick4_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[./tang_force_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x59]
type = NodalVariableValue
nodeid = 58
variable = disp_x
[../]
[./disp_x64]
type = NodalVariableValue
nodeid = 63
variable = disp_x
[../]
[./disp_y59]
type = NodalVariableValue
nodeid = 58
variable = disp_y
[../]
[./disp_y64]
type = NodalVariableValue
nodeid = 63
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
file_base = brick4_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = brick4_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x59 disp_y59 disp_x64 disp_y64 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+6
[../]
[]
(modules/xfem/test/tests/side_integral/side_integral_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 3
nz = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_cut_uo]
type = RectangleCutUserObject
cut_data = ' -1.0 -0.1 -1.0
2.0 1.1 -1.0
2.0 1.1 1.0
-1.0 -0.1 1.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./front]
type = DirichletBC
variable = u
boundary = front
value = 3
[../]
[./back]
type = DirichletBC
variable = u
boundary = back
value = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Postprocessors]
[./front]
type = SideIntegralVariablePostprocessor
variable = u
boundary = front
[../]
[./back]
type = SideIntegralVariablePostprocessor
variable = u
boundary = back
[../]
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/navier_stokes/test/tests/finite_element/pins/channel-flow/pm_heat_source.i)
# This test case tests the porous-medium flow with volumetric heat source
#
# At the steady state, the energy balance is given by
# rho * u * (h_out - h_in) = q''' * L
#
# with rho * u = 100; cp = 100; q''' = 1e6, L = 1, it is easy to obtain:
# T_out - T_in = 1e6 / (100 * 100) = 100
#
# This can be verified by check the T_out - T_in
[GlobalParams]
gravity = '0 0 0'
order = FIRST
family = LAGRANGE
u = vel_x
v = vel_y
pressure = p
temperature = T
porosity = porosity
eos = eos
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
nx = 10
ny = 4
elem_type = QUAD4
[]
[FluidProperties]
[./eos]
type = SimpleFluidProperties
density0 = 100 # kg/m^3
thermal_expansion = 0 # K^{-1}
cp = 100
viscosity = 0.1 # Pa-s, Re=rho*u*L/mu = 100*1*0.1/0.1 = 100
thermal_conductivity = 0.1
[../]
[]
[Functions]
[v_in]
type = PiecewiseLinear
x = '0 1e5'
y = '1 1'
[]
[T_in]
type = PiecewiseLinear
x = '0 1e5'
y = '630 630'
[]
[]
[Variables]
# velocity
[vel_x]
initial_condition = 1
[]
[vel_y]
initial_condition = 0
[]
[p]
initial_condition = 1e5
[]
[T]
scaling = 1e-3
initial_condition = 630
[]
[]
[AuxVariables]
[rho]
initial_condition = 100
[]
[porosity]
initial_condition = 0.4
[]
[vol_heat]
initial_condition = 1e6
[]
[]
[Materials]
[mat]
type = PINSFEMaterial
alpha = 1000
beta = 100
[]
[]
[Kernels]
[mass_time]
type = PINSFEFluidPressureTimeDerivative
variable = p
[]
[mass_space]
type = INSFEFluidMassKernel
variable = p
[]
[x_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_x
[]
[x_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_x
component = 0
[]
[y_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_y
[]
[y_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_y
component = 1
[]
[temperature_time]
type = PINSFEFluidTemperatureTimeDerivative
variable = T
[../]
[temperature_space]
type = INSFEFluidEnergyKernel
variable = T
power_density = vol_heat
[]
[]
[AuxKernels]
[rho_aux]
type = FluidDensityAux
variable = rho
p = p
T = T
fp = eos
[]
[]
[BCs]
# BCs for mass equation
# Inlet
[mass_inlet]
type = INSFEFluidMassBC
variable = p
boundary = 'left'
v_fn = v_in
[]
# Outlet
[./pressure_out]
type = DirichletBC
variable = p
boundary = 'right'
value = 1e5
[../]
# BCs for x-momentum equation
# Inlet
[vx_in]
type = FunctionDirichletBC
variable = vel_x
boundary = 'left'
function = v_in
[]
# Outlet (no BC is needed)
# BCs for y-momentum equation
# Both Inlet and Outlet, and Top and Bottom
[vy]
type = DirichletBC
variable = vel_y
boundary = 'left right bottom top'
value = 0
[]
# BCs for energy equation
[T_in]
type = FunctionDirichletBC
variable = T
boundary = 'left'
function = T_in
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
solve_type = 'PJFNK'
[]
[]
[Postprocessors]
[p_in]
type = SideAverageValue
variable = p
boundary = left
[]
[p_out]
type = SideAverageValue
variable = p
boundary = right
[]
[T_in]
type = SideAverageValue
variable = T
boundary = left
[]
[T_out]
type = SideAverageValue
variable = T
boundary = right
[]
[]
[Executioner]
type = Transient
dt = 1
dtmin = 1.e-3
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
nl_max_its = 20
l_tol = 1e-5
l_max_its = 100
start_time = 0.0
end_time = 10
num_steps = 10
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
time_step_interval = 1
execute_on = 'initial timestep_end'
[console]
type = Console
output_linear = false
[]
[out]
type = Exodus
use_displaced = false
[]
[]
(modules/xfem/test/tests/single_var_constraint_2d/stationary_jump_func.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = jump_func
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[Functions]
[./jump_func]
type = ParsedFunction
expression = '0.5'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/sliding_block/sliding/frictional_02_aug.i)
# This is a benchmark test that checks constraint based frictional
# contact using the augmented lagrangian method. In this test a constant
# displacement is applied in the horizontal direction to simulate
# a small block come sliding down a larger block.
#
# A friction coefficient of 0.2 is used. The gold file is run on one processor
# and the benchmark case is run on a minimum of 4 processors to ensure no
# parallel variability in the contact pressure and penetration results.
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[AuxVariables]
[./contact_traction]
[../]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 20
nl_max_its = 200
dt = 0.1
end_time = 15
num_steps = 200
l_tol = 1e-6
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
time_step_interval = 10
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Problem]
type = AugmentedLagrangianContactProblem
solution_variables = 'disp_x disp_y'
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 100
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = coulomb
penalty = 1e+7
friction_coefficient = 0.2
formulation = augmented_lagrange
normalize_penalty = true
al_penetration_tolerance = 1e-6
al_incremental_slip_tolerance = 1.0e-2
al_frictional_force_tolerance = 1e-3
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
(modules/solid_mechanics/test/tests/crystal_plasticity/hcp_single_crystal/hcp_volumetric_eigenstrain.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
elem_type = HEX8
[]
[AuxVariables]
[temperature]
order = FIRST
family = LAGRANGE
[]
[e_xtalpl_xx]
order = CONSTANT
family = MONOMIAL
[]
[e_xtalpl_yy]
order = CONSTANT
family = MONOMIAL
[]
[ev_zz]
order = CONSTANT
family = MONOMIAL
[]
[e_xtalpl_zz]
order = CONSTANT
family = MONOMIAL
[]
[fv_xx]
order = CONSTANT
family = MONOMIAL
[]
[fv_yy]
order = CONSTANT
family = MONOMIAL
[]
[fv_zz]
order = CONSTANT
family = MONOMIAL
[]
[fp_xx]
order = CONSTANT
family = MONOMIAL
[]
[fp_yy]
order = CONSTANT
family = MONOMIAL
[]
[fp_zz]
order = CONSTANT
family = MONOMIAL
[]
[f_xx]
order = CONSTANT
family = MONOMIAL
[]
[f_yy]
order = CONSTANT
family = MONOMIAL
[]
[f_zz]
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic/all]
strain = FINITE
incremental = true
add_variables = true
additional_generate_output = 'stress_zz stress_xx stress_yy vonmises_stress l2norm_strain'
additional_material_output_order = FIRST
[]
[Functions]
[temperature_ramp]
type = ParsedFunction
expression = 'if(t<=1500.0, 600.0 + t/6.0, 850.0)'
[]
[]
[AuxKernels]
[temperature]
type = FunctionAux
variable = temperature
function = 'temperature_ramp'
execute_on = timestep_begin
[]
[e_xtalpl_xx]
type = RankTwoAux
variable = e_xtalpl_xx
rank_two_tensor = total_lagrangian_strain
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[e_xtalpl_yy]
type = RankTwoAux
variable = e_xtalpl_yy
rank_two_tensor = total_lagrangian_strain
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[ev_zz]
type = RankTwoAux
variable = ev_zz
rank_two_tensor = void_eigenstrain
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[e_xtalpl_zz]
type = RankTwoAux
variable = e_xtalpl_zz
rank_two_tensor = total_lagrangian_strain
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[fv_xx]
type = RankTwoAux
variable = fv_xx
rank_two_tensor = volumetric_deformation_gradient
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[fv_yy]
type = RankTwoAux
variable = fv_yy
rank_two_tensor = volumetric_deformation_gradient
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[fv_zz]
type = RankTwoAux
variable = fv_zz
rank_two_tensor = volumetric_deformation_gradient
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[fp_xx]
type = RankTwoAux
variable = fp_xx
rank_two_tensor = plastic_deformation_gradient
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[fp_yy]
type = RankTwoAux
variable = fp_yy
rank_two_tensor = plastic_deformation_gradient
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[fp_zz]
type = RankTwoAux
variable = fp_zz
rank_two_tensor = plastic_deformation_gradient
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[f_xx]
type = RankTwoAux
variable = f_xx
rank_two_tensor = deformation_gradient
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[f_yy]
type = RankTwoAux
variable = f_yy
rank_two_tensor = deformation_gradient
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[f_zz]
type = RankTwoAux
variable = f_zz
rank_two_tensor = deformation_gradient
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[tdisp]
type = DirichletBC
variable = disp_z
boundary = front
value = 0
[]
[]
[Materials]
[elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '1.684e5 1.214e5 1.214e5 1.684e5 1.214e5 1.684e5 0.754e5 0.754e5 0.754e5'
fill_method = symmetric9
[]
[stress]
type = ComputeMultipleCrystalPlasticityStress
crystal_plasticity_models = 'trial_xtalpl'
eigenstrain_names = void_eigenstrain
tan_mod_type = exact
line_search_method = CUT_HALF
use_line_search = true
maximum_substep_iteration = 10
[]
[trial_xtalpl]
type = CrystalPlasticityHCPDislocationSlipBeyerleinUpdate
number_slip_systems = 15
slip_sys_file_name = hcp_aprismatic_capyramidal_slip_sys.txt
unit_cell_dimension = '2.934e-7 2.934e-7 4.657e-7' #Ti, in mm, https://materialsproject.org/materials/mp-46/
temperature = temperature
initial_forest_dislocation_density = 15.0e3
initial_substructure_density = 1.0e3
slip_system_modes = 2
number_slip_systems_per_mode = '3 12'
lattice_friction_per_mode = '9 22' #Knezevic et al MSEA 654 (2013)
effective_shear_modulus_per_mode = '4.7e2 4.7e2' #Ti, in MPa, https://materialsproject.org/materials/mp-46/
burgers_vector_per_mode = '2.934e-7 6.586e-7' #Ti, in mm, https://materialsproject.org/materials/mp-46/
slip_generation_coefficient_per_mode = '1.25e5 2.25e7' #from Beyerlein and Tome 2008 IJP
normalized_slip_activiation_energy_per_mode = '3.73e-3 3.2e-2' #from Beyerlein and Tome 2008 IJP
slip_energy_proportionality_factor_per_mode = '330 100' #from Beyerlein and Tome 2008 IJP
substructure_rate_coefficient_per_mode = '355 0.4' #from Capolungo et al MSEA (2009)
applied_strain_rate = 0.001
gamma_o = 1.0e-3
Hall_Petch_like_constant_per_mode = '0.2 0.2' #Estimated to match graph in Capolungo et al MSEA (2009), Figure 2
grain_size = 20.0e-3 #20 microns, Beyerlein and Tome IJP (2008)
[]
[void_eigenstrain]
type = ComputeCrystalPlasticityVolumetricEigenstrain
eigenstrain_name = void_eigenstrain
deformation_gradient_name = volumetric_deformation_gradient
mean_spherical_void_radius = void_radius
spherical_void_number_density = void_density
[]
[void_density]
type = ParsedMaterial
property_name = void_density
coupled_variables = temperature
expression = 'if(temperature<611.0, 0.0,
if(temperature<=835.0, 2.387e13 *(temperature - 611.0) / 1344.0, 0.0))' #1/mm^3, gives an eigenstrain of 1.0e-5 with radius=1.0e-6mm
# outputs = exodus
[]
[void_radius]
type = GenericConstantMaterial
prop_names = void_radius
prop_values = '1.0e-6' ##1 nm avg particle radius
[]
[]
[Postprocessors]
[stress_zz]
type = ElementAverageValue
variable = stress_zz
[]
[e_xtalpl_xx]
type = ElementAverageValue
variable = e_xtalpl_xx
[]
[e_xtalpl_yy]
type = ElementAverageValue
variable = e_xtalpl_yy
[]
[ev_zz]
type = ElementAverageValue
variable = ev_zz
[]
[e_xtalpl_zz]
type = ElementAverageValue
variable = e_xtalpl_zz
[]
[fv_xx]
type = ElementAverageValue
variable = fv_xx
[]
[fv_yy]
type = ElementAverageValue
variable = fv_yy
[]
[fv_zz]
type = ElementAverageValue
variable = fv_zz
[]
[temperature]
type = ElementAverageValue
variable = temperature
[]
[fp_xx]
type = ElementAverageValue
variable = fp_xx
[]
[fp_yy]
type = ElementAverageValue
variable = fp_yy
[]
[fp_zz]
type = ElementAverageValue
variable = fp_zz
[]
[f_xx]
type = ElementAverageValue
variable = f_xx
[]
[f_yy]
type = ElementAverageValue
variable = f_yy
[]
[f_zz]
type = ElementAverageValue
variable = f_zz
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Debug]
show_var_residual_norms = true
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-10
nl_abs_step_tol = 1e-10
dt = 10.0
dtmin = 1e-4
# end_time = 10
num_steps = 10
[]
[Outputs]
csv = true
[console]
type = Console
# max_rows = 5
[]
[]
(test/tests/adaptivity/recompute_markers_during_cycles/recompute_markers_during_cycles.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Transient
num_steps = 2
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
cycles_per_step = 4
marker = circle_marker
max_h_level = 2
recompute_markers_during_cycles = true
[./Markers]
[./circle_marker]
type = CircleMarker
point = '0.5 0.5 0'
radius = 0.1
inside = refine
outside = do_nothing
[../]
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(modules/thermal_hydraulics/test/tests/components/heat_structure_cylindrical/part_base.i)
[Functions]
[power_profile_fn]
type = ParsedFunction
expression = '1.570796326794897 * sin(x / 3.6576 * pi)'
[]
[]
[Components]
[reactor]
type = TotalPower
power = 296153.84615384615385
[]
[hs]
type = HeatStructureCylindrical
position = '0 0 1'
orientation = '1 0 0'
length = 3.6576
n_elems = 20
names = 'FUEL GAP CLAD'
widths = '0.0046955 0.0000955 0.000673'
n_part_elems = '3 1 1'
initial_T = 564.15
[]
[hg]
type = HeatSourceFromTotalPower
hs = hs
regions = 'FUEL'
power_fraction = 3.33672612e-1
power = reactor
power_shape_function = power_profile_fn
[]
[temp_outside]
type = HSBoundarySpecifiedTemperature
hs = hs
boundary = hs:outer
T = 600
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
start_time = 0
dt = 2
num_steps = 10
abort_on_solve_fail = true
solve_type = 'NEWTON'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 30
l_tol = 1e-4
l_max_its = 300
[]
[Outputs]
file_base = transient
exodus = true
[console]
type = Console
execute_scalars_on = none
[]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_balance/large_gap_heat_transfer_test_sphere.i)
sphere_outer_htc = 10 # W/m^2/K
sphere_outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
[file]
type = FileMeshGenerator
file = cyl2D.e
[]
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[]
[AuxVariables]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[power_density]
block = 'fuel'
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
[]
[heat_source]
type = CoupledForce
variable = temp
block = 'fuel'
v = power_density
[]
[]
[AuxKernels]
[gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0.8
emissivity_secondary = 0.8
gap_conductivity = 0.1
quadrature = true
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = '4' # outer RPV
coefficient = ${sphere_outer_htc}
T_infinity = ${sphere_outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[Quadrature]
order = fifth
side_order = seventh
[]
[]
[Outputs]
exodus = false
csv = true
[Console]
type = Console
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 'fuel'
[]
[sphere_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = '4' # outer RVP
T_fluid = ${sphere_outer_Tinf}
htc = ${sphere_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(sphere_convective_out - ptot) / ptot'
pp_names = 'sphere_convective_out ptot'
[]
[]
(test/tests/postprocessors/pps_interval/pps_out_interval.i)
[Mesh]
file = square-2x2-nodeids.e
# This test can only be run with renumering disabled, so the
# NodalVariableValue postprocessor's node id is well-defined.
allow_renumbering = false
[]
[Variables]
active = 'u v'
[./u]
order = SECOND
family = LAGRANGE
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Functions]
active = 'force_fn exact_fn left_bc'
[./force_fn]
type = ParsedFunction
expression = '1-x*x+2*t'
[../]
[./exact_fn]
type = ParsedFunction
expression = '(1-x*x)*t'
[../]
[./left_bc]
type = ParsedFunction
expression = t
[../]
[]
[Kernels]
active = '
time_u diff_u ffn_u
time_v diff_v'
[./time_u]
type = TimeDerivative
variable = u
[../]
[./diff_u]
type = Diffusion
variable = u
[../]
[./ffn_u]
type = BodyForce
variable = u
function = force_fn
[../]
[./time_v]
type = TimeDerivative
variable = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'all_u left_v right_v'
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = exact_fn
[../]
[./left_v]
type = FunctionDirichletBC
variable = v
boundary = '3'
function = left_bc
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = '2'
value = 0
[../]
[]
[Postprocessors]
active = 'l2 node1 node4'
[./l2]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[./node1]
type = NodalVariableValue
variable = u
nodeid = 15
[../]
[./node4]
type = NodalVariableValue
variable = v
nodeid = 10
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
dt = 0.1
start_time = 0
end_time = 1
[]
[Outputs]
file_base = pps_out_interval
time_step_interval = 2
exodus = true
[./console]
type = Console
time_step_interval = 1
[../]
[]
(test/tests/multiapps/multilevel/dt_from_parent_parent.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 1
dt = 0.25
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./out]
type = Console
output_file = true
[../]
[]
[MultiApps]
[./sub]
type = TransientMultiApp
app_type = MooseTestApp
positions = '0 0 0 0.5 0.5 0'
input_files = dt_from_parent_sub.i
[../]
[]
(modules/thermal_hydraulics/test/tests/components/heat_structure_cylindrical/steady.i)
# Tests that cylindrical heat structure geometry can be used with a steady executioner.
[Functions]
[power_profile_fn]
type = ParsedFunction
expression = '1.570796326794897 * sin(x / 3.6576 * pi)'
[]
[]
[SolidProperties]
[fuel_sp]
type = ThermalFunctionSolidProperties
rho = 1.0412e2
cp = 288.734
k = 3.65
[]
[gap_sp]
type = ThermalFunctionSolidProperties
rho = 1.0
cp = 1.0
k = 1.084498
[]
[clad_sp]
type = ThermalFunctionSolidProperties
rho = 6.6e1
cp = 321.384
k = 16.48672
[]
[]
[Components]
[reactor]
type = TotalPower
power = 296153.84615384615385
[]
[hs]
type = HeatStructureCylindrical
position = '0 0 1'
orientation = '1 0 0'
length = 3.6576
n_elems = 20
names = 'FUEL GAP CLAD'
widths = '0.0046955 0.0000955 0.000673'
n_part_elems = '3 1 1'
solid_properties = 'fuel_sp gap_sp clad_sp'
solid_properties_T_ref = '300 300 300'
initial_T = 564.15
[]
[hg]
type = HeatSourceFromTotalPower
hs = hs
regions = 'FUEL'
power_fraction = 3.33672612e-1
power = reactor
power_shape_function = power_profile_fn
[]
[temp_outside]
type = HSBoundarySpecifiedTemperature
hs = hs
boundary = hs:outer
T = 600
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 30
l_tol = 1e-4
l_max_its = 300
[]
[Outputs]
[out]
type = Exodus
[]
[console]
type = Console
execute_scalars_on = none
[]
[]
(modules/contact/test/tests/frictional/sliding_elastic_blocks_2d/sliding_elastic_blocks_2d_tp.i)
[Mesh]
file = sliding_elastic_blocks_2d.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
diag_save_in = 'diag_saved_x diag_saved_y'
[../]
[]
[AuxKernels]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip]
type = PenetrationAux
variable = accum_slip
execute_on = timestep_end
quantity = accumulated_slip
boundary = 3
paired_boundary = 2
[../]
[./tangential_force_x]
type = PenetrationAux
variable = tang_force_x
execute_on = timestep_end
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tangential_force_y]
type = PenetrationAux
variable = tang_force_y
execute_on = timestep_end
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.005
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e7
poissons_ratio = 0.3
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.05
num_steps = 1000
nl_rel_tol = 1e-16
nl_abs_tol = 1e-09
dtmin = 0.01
l_tol = 1e-3
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = coulomb
formulation = tangential_penalty
friction_coefficient = '0.25'
penalty = 1e6
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
secondary = 3
primary = 2
[../]
[]
(modules/combined/examples/xfem/xfem_thermomechanics_stress_growth.i)
# This is a demonstration of a simple thermomechanics simulation using
# XFEM in which a single crack propagates based on a principal stress
# criterion.
#
# The top and bottom of the plate are fixed in the y direction, and the
# top of the plate is cooled down over time. The thermal contraction
# causes tensile stresses, which lead to crack propagation. The crack
# propagates in a curved path because of the changinging nature of
# the thermal gradient as a result of the crack. There is no heat
# conduction across the crack as soon as it forms.
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[Variables]
# Solve for the temperature and the displacements
# Displacements are not specified because the TensorMechanics/Master Action sets them up
[./temp]
initial_condition = 300
[../]
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.8 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./xfem_marker_uo]
type = XFEMRankTwoTensorMarkerUserObject
execute_on = timestep_end
tensor = stress
scalar_type = MaxPrincipal
threshold = 5e+1
average = true
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
eigenstrain_names = eigenstrain
[../]
[]
[Kernels]
[./htcond]
type = HeatConduction
variable = temp
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = DirichletBC
boundary = top
variable = disp_y
value = 0.0
[../]
[./topt]
type = FunctionDirichletBC
boundary = top
variable = temp
function = 273-t*27.3
[../]
[./bott]
type = FunctionDirichletBC
boundary = bottom
variable = temp
function = 273
# value = 273.0
[../]
[]
[Materials]
[./thcond]
type = GenericConstantMaterial
prop_names = 'thermal_conductivity'
prop_values = '5e-6'
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_strain]
type= ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 10e-6
temperature = temp
stress_free_temperature = 273
eigenstrain_name = eigenstrain
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 10.0
max_xfem_update = 5
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/pressure_bc/2d_pressure_displaced_mesh.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.5 1.0 0.5'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
planar_formulation = PLANE_STRAIN
generate_output = 'stress_xx stress_yy'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1.0'
y = '500 500'
[../]
[./bc_func_tx]
type = ParsedFunction
expression = '0.5-(0.5-x)*cos(pi*t/2.0)-x'
[../]
[./bc_func_ty]
type = ParsedFunction
expression = '(0.5-x)*sin(pi*t/2.0)+0.5'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
boundary = 0
preset = false
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
preset = false
variable = disp_x
value = 0.0
[../]
[./top_right_y]
type = FunctionDirichletBC
boundary = 2
preset = false
variable = disp_y
function = bc_func_ty
[../]
[./top_right_x]
type = FunctionDirichletBC
boundary = 2
preset = false
variable = disp_x
function = bc_func_tx
[../]
[]
[DiracKernels]
[./pressure_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
use_displaced_mesh = true
[../]
[./pressure_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
use_displaced_mesh = true
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-14
# time control
start_time = 0.0
dt = 0.1
end_time = 1.0
[]
[Outputs]
file_base = 2d_pressure_displaced_mesh_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_2/brick2_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick2_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_x26]
type = NodalVariableValue
nodeid = 25
variable = disp_x
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_y26]
type = NodalVariableValue
nodeid = 25
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x7 disp_y7 disp_x26 disp_y26 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/stationary_jump_fluxjump.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0.5
jump_flux = 1
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/sliding_block/in_and_out/frictional_04_penalty.i)
# This is a benchmark test that checks constraint based frictional
# contact using the penalty method. In this test a sinusoidal
# displacement is applied in the horizontal direction to simulate
# a small block come in and out of contact as it slides down a larger block.
#
# The sinusoid is of the form 0.4sin(4t)+0.2 and a friction coefficient
# of 0.4 is used. The gold file is run on one processor and the benchmark
# case is run on a minimum of 4 processors to ensure no parallel variability
# in the contact pressure and penetration results. Further documentation can
# found in moose/modules/contact/doc/sliding_block/
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[penetration]
[]
[inc_slip_x]
[]
[inc_slip_y]
[]
[accum_slip_x]
[]
[accum_slip_y]
[]
[]
[Functions]
[vertical_movement]
type = ParsedFunction
expression = -t
[]
[horizontal_movement]
type = ParsedFunction
expression = -0.04*sin(4*t)+0.02
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
[]
[]
[AuxKernels]
[zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[]
[accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[]
[penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[]
[]
[Postprocessors]
[nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[]
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[]
[]
[BCs]
[left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[]
[left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[]
[right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[]
[]
[Materials]
[left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[]
[left_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 20 101'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-3
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Outputs]
# csv = true
time_step_interval = 10
[out]
type = Exodus
elemental_as_nodal = true
[]
[console]
type = Console
max_rows = 5
[]
[]
[Contact]
[leftright]
secondary = 3
primary = 2
model = coulomb
penalty = 2e+6
friction_coefficient = 0.4
formulation = penalty
normal_smoothing_distance = 0.1
[]
[]
(test/tests/problems/eigen_problem/eigensolvers/gipm_ibc.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 100
ymin = 0
ymax = 100
elem_type = QUAD4
nx = 64
ny = 64
displacements = 'x_disp y_disp'
[]
[Variables]
[./u]
order = first
family = LAGRANGE
[../]
[]
[AuxVariables]
[./x_disp]
[../]
[./y_disp]
[../]
[]
[AuxKernels]
[./x_disp]
type = FunctionAux
variable = x_disp
function = x_disp_func
[../]
[./y_disp]
type = FunctionAux
variable = y_disp
function = y_disp_func
[../]
[]
[Functions]
[./x_disp_func]
type = ParsedFunction
expression = 0
[../]
[./y_disp_func]
type = ParsedFunction
expression = 0
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
use_displaced_mesh = true
[../]
[./rea]
type = CoefReaction
variable = u
coefficient = 2.0
use_displaced_mesh = true
[../]
[./rhs]
type = CoefReaction
variable = u
use_displaced_mesh = true
coefficient = -1.0
extra_vector_tags = 'eigen'
[../]
[]
[BCs]
[./nbc_homogeneous]
type = DirichletBC
variable = u
boundary = '0'
value = 0
use_displaced_mesh = true
[../]
[./nbc_eigen]
type = EigenDirichletBC
variable = u
boundary = '0'
use_displaced_mesh = true
[../]
[./ibc]
type = VacuumBC
variable = u
boundary = '1 2 3'
extra_vector_tags = 'eigen'
use_displaced_mesh = true
[]
[]
[Executioner]
type = Eigenvalue
eigen_problem_type = gen_non_hermitian
which_eigen_pairs = SMALLEST_MAGNITUDE
n_eigen_pairs = 1
n_basis_vectors = 18
solve_type = jacobi_davidson
petsc_options = '-eps_view'
[]
[VectorPostprocessors]
[./eigenvalues]
type = Eigenvalues
execute_on = 'timestep_end'
[../]
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[./console]
type = Console
outlier_variable_norms = false
[../]
[]
(modules/xfem/test/tests/single_var_constraint_3d/stationary_fluxjump_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.25
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.5 -0.001 -0.001
0.5 1.001 -0.001
0.5 1.001 1.001
0.5 -0.001 1.001'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 1
geometric_cut_userobject = 'square_planar_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/solid_mechanics/examples/coal_mining/cosserat_mc_only.i)
# Strata deformation and fracturing around a coal mine
#
# A 2D geometry is used that simulates a transverse section of
# the coal mine. The model is actually 3D, but the "x"
# dimension is only 10m long, meshed with 1 element, and
# there is no "x" displacement. The mine is 300m deep
# and just the roof is studied (0<=z<=300). The model sits
# between 0<=y<=450. The excavation sits in 0<=y<=150. This
# is a "half model": the boundary conditions are such that
# the model simulates an excavation sitting in -150<=y<=150
# inside a model of the region -450<=y<=450. The
# excavation height is 3m (ie, the excavation lies within
# 0<=z<=3). Mining is simulated by moving the excavation's
# roof down, until disp_z=-3 at t=1.
# Time is meaningless in this example
# as quasi-static solutions are sought at each timestep, but
# the number of timesteps controls the resolution of the
# process.
#
# The boundary conditions are:
# - disp_x = 0 everywhere
# - disp_y = 0 at y=0 and y=450
# - disp_z = 0 for y>150
# - disp_z = -3 at maximum, for 0<=y<=150. See excav function.
# That is, rollers on the sides, free at top, and prescribed at bottom.
#
# The small strain formulation is used.
#
# All stresses are measured in MPa. The initial stress is consistent with
# the weight force from density 2500 kg/m^3, ie, stress_zz = -0.025*(300-z) MPa
# where gravity = 10 m.s^-2 = 1E-5 MPa m^2/kg. The maximum and minimum
# principal horizontal stresses are assumed to be equal to 0.8*stress_zz.
#
# Below you will see weak-plane parameters and AuxVariables, etc.
# These are not actally used in this example.
#
# Material properties:
# Young's modulus = 8 GPa
# Poisson's ratio = 0.25
# Cosserat layer thickness = 1 m
# Cosserat-joint normal stiffness = large
# Cosserat-joint shear stiffness = 1 GPa
# MC cohesion = 3 MPa
# MC friction angle = 37 deg
# MC dilation angle = 8 deg
# MC tensile strength = 1 MPa
# MC compressive strength = 100 MPa, varying down to 1 MPa when tensile strain = 1
#
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
xmin = -5
xmax = 5
nz = 40
zmin = 0
zmax = 400.0
bias_z = 1.1
ny = 30 # make this a multiple of 3, so y=150 is at a node
ymin = 0
ymax = 450
[]
[left]
type = SideSetsAroundSubdomainGenerator
new_boundary = 11
normal = '0 -1 0'
input = generated_mesh
[]
[right]
type = SideSetsAroundSubdomainGenerator
new_boundary = 12
normal = '0 1 0'
input = left
[]
[front]
type = SideSetsAroundSubdomainGenerator
new_boundary = 13
normal = '-1 0 0'
input = right
[]
[back]
type = SideSetsAroundSubdomainGenerator
new_boundary = 14
normal = '1 0 0'
input = front
[]
[top]
type = SideSetsAroundSubdomainGenerator
new_boundary = 15
normal = '0 0 1'
input = back
[]
[bottom]
type = SideSetsAroundSubdomainGenerator
new_boundary = 16
normal = '0 0 -1'
input = top
[]
[excav]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-5 0 0'
top_right = '5 150 3'
input = bottom
[]
[roof]
type = SideSetsBetweenSubdomainsGenerator
new_boundary = 21
primary_block = 0
paired_block = 1
input = excav
[]
[hole]
type = BlockDeletionGenerator
block = 1
input = roof
[]
[]
[GlobalParams]
block = 0
perform_finite_strain_rotations = false
displacements = 'disp_x disp_y disp_z'
Cosserat_rotations = 'wc_x wc_y wc_z'
[]
[Variables]
[./disp_y]
[../]
[./disp_z]
[../]
[./wc_x]
[../]
[]
[Kernels]
[./cy_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_y
component = 1
[../]
[./cz_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_z
component = 2
[../]
[./x_couple]
type = StressDivergenceTensors
use_displaced_mesh = false
variable = wc_x
displacements = 'wc_x wc_y wc_z'
component = 0
base_name = couple
[../]
[./x_moment]
type = MomentBalancing
use_displaced_mesh = false
variable = wc_x
component = 0
[../]
[./gravity]
type = Gravity
use_displaced_mesh = false
variable = disp_z
value = -10E-6
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./wc_y]
[../]
[./wc_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./mc_shear]
type = MaterialStdVectorAux
index = 0
property = mc_plastic_internal_parameter
variable = mc_shear
[../]
[./mc_tensile]
type = MaterialStdVectorAux
index = 1
property = mc_plastic_internal_parameter
variable = mc_tensile
[../]
[./wp_shear]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_internal_parameter
variable = wp_shear
[../]
[./wp_tensile]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_internal_parameter
variable = wp_tensile
[../]
[./mc_shear_f]
type = MaterialStdVectorAux
index = 6
property = mc_plastic_yield_function
variable = mc_shear_f
[../]
[./mc_tensile_f]
type = MaterialStdVectorAux
index = 0
property = mc_plastic_yield_function
variable = mc_tensile_f
[../]
[./wp_shear_f]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_yield_function
variable = wp_shear_f
[../]
[./wp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_yield_function
variable = wp_tensile_f
[../]
[]
[BCs]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '11 12 16 21' # note addition of 16 and 21
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '16'
value = 0.0
[../]
[./no_wc_x]
type = DirichletBC
variable = wc_x
boundary = '11 12'
value = 0.0
[../]
[./roof]
type = FunctionDirichletBC
variable = disp_z
boundary = 21
function = excav_sideways
[../]
[]
[Functions]
[./ini_xx]
type = ParsedFunction
expression = '-0.8*2500*10E-6*(400-z)'
[../]
[./ini_zz]
type = ParsedFunction
expression = '-2500*10E-6*(400-z)'
[../]
[./excav_sideways]
type = ParsedFunction
symbol_names = 'end_t ymin ymax e_h closure_dist'
symbol_values = '1.0 0 150.0 -3.0 15.0'
expression = 'e_h*max(min((t/end_t*(ymax-ymin)+ymin-y)/closure_dist,1),0)'
[../]
[./excav_downwards]
type = ParsedFunction
symbol_names = 'end_t ymin ymax e_h closure_dist'
symbol_values = '1.0 0 150.0 -3.0 15.0'
expression = 'e_h*t/end_t*max(min(((ymax-ymin)+ymin-y)/closure_dist,1),0)'
[../]
[]
[UserObjects]
[./mc_coh_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 2.99 # MPa
value_residual = 3.01 # MPa
rate = 1.0
[../]
[./mc_fric]
type = SolidMechanicsHardeningConstant
value = 0.65 # 37deg
[../]
[./mc_dil]
type = SolidMechanicsHardeningConstant
value = 0.15 # 8deg
[../]
[./mc_tensile_str_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 1.0 # MPa
value_residual = 1.0 # MPa
rate = 1.0
[../]
[./mc_compressive_str]
type = SolidMechanicsHardeningCubic
value_0 = 100 # Large!
value_residual = 100
internal_limit = 0.1
[../]
[./wp_coh_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_tan_fric]
type = SolidMechanicsHardeningConstant
value = 0.36 # 20deg
[../]
[./wp_tan_dil]
type = SolidMechanicsHardeningConstant
value = 0.18 # 10deg
[../]
[./wp_tensile_str_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_compressive_str_soften]
type = SolidMechanicsHardeningCubic
value_0 = 100
value_residual = 1.0
internal_limit = 1.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeLayeredCosseratElasticityTensor
young = 8E3 # MPa
poisson = 0.25
layer_thickness = 1.0
joint_normal_stiffness = 1E9 # huge
joint_shear_stiffness = 1E3
[../]
[./strain]
type = ComputeCosseratIncrementalSmallStrain
eigenstrain_names = ini_stress
[../]
[./ini_stress]
type = ComputeEigenstrainFromInitialStress
initial_stress = 'ini_xx 0 0 0 ini_xx 0 0 0 ini_zz'
eigenstrain_name = ini_stress
[../]
[./stress]
type = ComputeMultipleInelasticCosseratStress
block = 0
inelastic_models = mc
relative_tolerance = 2.0
absolute_tolerance = 1E6
max_iterations = 1
tangent_operator = nonlinear
perform_finite_strain_rotations = false
[../]
[./mc]
type = CappedMohrCoulombCosseratStressUpdate
block = 0
warn_about_precision_loss = false
host_youngs_modulus = 8E3
host_poissons_ratio = 0.25
base_name = mc
tensile_strength = mc_tensile_str_strong_harden
compressive_strength = mc_compressive_str
cohesion = mc_coh_strong_harden
friction_angle = mc_fric
dilation_angle = mc_dil
max_NR_iterations = 100000
smoothing_tol = 0.1 # MPa # Must be linked to cohesion
yield_function_tol = 1E-9 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0
[../]
[./wp]
type = CappedWeakPlaneCosseratStressUpdate
block = 0
warn_about_precision_loss = false
base_name = wp
cohesion = wp_coh_harden
tan_friction_angle = wp_tan_fric
tan_dilation_angle = wp_tan_dil
tensile_strength = wp_tensile_str_harden
compressive_strength = wp_compressive_str_soften
max_NR_iterations = 10000
tip_smoother = 0.1
smoothing_tol = 0.1 # MPa # Note, this must be tied to cohesion, otherwise get no possible return at cone apex
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0E-3
[../]
[./density]
type = GenericConstantMaterial
prop_names = density
prop_values = 2500
[../]
[]
[Postprocessors]
[./subsidence]
type = PointValue
point = '0 0 400'
variable = disp_z
use_displaced_mesh = false
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
line_search = bt
nl_abs_tol = 1e-3
nl_rel_tol = 1e-5
l_max_its = 30
nl_max_its = 1000
start_time = 0.0
dt = 0.2
end_time = 0.2
[]
[Outputs]
file_base = cosserat_mc_only
time_step_interval = 1
print_linear_residuals = false
csv = true
exodus = true
[./console]
type = Console
output_linear = false
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_3/cyl3_template2.i)
#
# This input file is a template for both the frictionless and glued test
# variations for the current problem geometry. In order to create an input
# file to run outside the runtest framework, look at the tests file and add the
# appropriate input file lines from the cli_args line.
#
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl3_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
tangential_tolerance = 1e-3
penalty = 1e+11
al_penetration_tolerance = 1e-8
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_3/ring3_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring3_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = ring3_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = ring3_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(test/tests/utils/perf_graph_live_print/perf_graph_live_print.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Problem]
type = SlowProblem
seconds_to_sleep = 4
print_during_section = false
nest_inside_section = false
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
active = ''
[subapp]
type = FullSolveMultiApp
input_files = 'perf_graph_live_print.i'
cli_args = "perf_graph_live_print.i"
[]
[]
[Outputs]
perf_graph_live_time_limit = 1
[console]
type = Console
fit_mode = 80
[]
[]
(modules/porous_flow/test/tests/sinks/s02.i)
# apply a sink flux with use_mobility=true and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1
[]
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = y+1
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '0.2 0 0 0 0.1 0 0 0 0.1'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[xval]
[]
[yval]
[]
[]
[ICs]
[xval]
type = FunctionIC
variable = xval
function = x
[]
[yval]
type = FunctionIC
variable = yval
function = y
[]
[]
[Functions]
[mass00]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)'
symbol_names = 'vol por dens0 pp bulk'
symbol_values = '0.25 0.1 1.1 p00 1.3'
[]
[mass01]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)'
symbol_names = 'vol por dens0 pp bulk'
symbol_values = '0.25 0.1 1.1 p01 1.3'
[]
[expected_mass_change00]
type = ParsedFunction
expression = 'fcn*perm*dens0*exp(pp/bulk)/visc*area*dt'
symbol_names = 'fcn perm dens0 pp bulk visc area dt'
symbol_values = '6 0.2 1.1 p00 1.3 1.1 0.5 1E-3'
[]
[expected_mass_change01]
type = ParsedFunction
expression = 'fcn*perm*dens0*exp(pp/bulk)/visc*area*dt'
symbol_names = 'fcn perm dens0 pp bulk visc area dt'
symbol_values = '6 0.2 1.1 p01 1.3 1.1 0.5 1E-3'
[]
[mass00_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm00_prev del_m00'
[]
[mass01_expect]
type = ParsedFunction
expression = 'mass_prev-mass_change'
symbol_names = 'mass_prev mass_change'
symbol_values = 'm01_prev del_m01'
[]
[]
[Postprocessors]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m00]
type = FunctionValuePostprocessor
function = mass00
execute_on = 'initial timestep_end'
[]
[m00_prev]
type = FunctionValuePostprocessor
function = mass00
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m00]
type = FunctionValuePostprocessor
function = expected_mass_change00
execute_on = 'timestep_end'
outputs = 'console'
[]
[m00_expect]
type = FunctionValuePostprocessor
function = mass00_expect
execute_on = 'timestep_end'
[]
[p10]
type = PointValue
point = '1 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m01]
type = FunctionValuePostprocessor
function = mass01
execute_on = 'initial timestep_end'
[]
[m01_prev]
type = FunctionValuePostprocessor
function = mass01
execute_on = 'timestep_begin'
outputs = 'console'
[]
[del_m01]
type = FunctionValuePostprocessor
function = expected_mass_change01
execute_on = 'timestep_end'
outputs = 'console'
[]
[m01_expect]
type = FunctionValuePostprocessor
function = mass01_expect
execute_on = 'timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowSink
boundary = 'left'
variable = pp
use_mobility = true
use_relperm = true
fluid_phase = 0
flux_function = 6
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-3
end_time = 0.03
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s02
[console]
type = Console
execute_on = 'nonlinear linear'
time_step_interval = 30
[]
[csv]
type = CSV
execute_on = 'timestep_end'
time_step_interval = 3
[]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_4/cyl4_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl4_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_1/cyl1_template1.i)
#
# This input file is a template for both the frictionless and glued test
# variations for the current problem geometry. In order to create an input
# file to run outside the runtest framework, look at the tests file and add the
# appropriate input file lines from the cli_args line.
#
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl1_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/xfem/test/tests/high_order_elements/diffusion_3d.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = TET10
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.35 1.01 -0.001
0.35 0.49 -0.001
0.35 0.49 0.201
0.35 1.01 0.201'
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = left
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_2/brick2_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick2_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[./tang_force_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_x26]
type = NodalVariableValue
nodeid = 25
variable = disp_x
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_y26]
type = NodalVariableValue
nodeid = 25
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
file_base = brick2_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = brick2_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x7 disp_y7 disp_x26 disp_y26 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+7
[../]
[]
(modules/solid_mechanics/test/tests/material_limit_time_step/elas_plas/nafems_nl1_lim.i)
#
# Tests material model IsotropicPlasticity with material based time stepper
# Boundary conditions from NAFEMS test NL1
#
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]#Comment
file = one_elem2.e
[] # Mesh
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[] # Variables
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_eff]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[] # AuxVariables
[Kernels]
[SolidMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
[../]
[./plastic_strain_eff]
type = MaterialRealAux
property = effective_plastic_strain
variable = plastic_strain_eff
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
[../]
[] # AuxKernels
[Functions]
[./appl_dispx]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0'
y = '0.0 0.25e-4 0.50e-4 0.50e-4 0.50e-4 0.25e-4 0.0 0.0 0.0'
[../]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0'
y = '0.0 0.0 0.0 0.25e-4 0.50e-4 0.50e-4 0.50e-4 0.25e-4 0.0 '
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[./right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 2
function = appl_dispx
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
block = 1
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 5e6
hardening_constant = 0.0
relative_tolerance = 1e-20
absolute_tolerance = 1e-8
max_inelastic_increment = 0.000001
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
[./TimeStepper]
type = IterationAdaptiveDT
dt = 0.1
time_t = '1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0'
time_dt = '0.1 0.1 0.1 0.1 0.1 0.1 0.1 0.1'
optimal_iterations = 30
iteration_window = 9
growth_factor = 2.0
cutback_factor = 0.5
timestep_limiting_postprocessor = matl_ts_min
[../]
start_time = 0.0
num_steps = 1000
end_time = 8.0
[] # Executioner
[Postprocessors]
[./matl_ts_min]
type = MaterialTimeStepPostprocessor
[../]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./plas_strain_eff]
type = ElementAverageValue
variable = plastic_strain_eff
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
output_linear = true
[../]
[] # Outputs
(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/lid_driven_md.i)
[GlobalParams]
gravity = '0 0 0'
order = FIRST
family = LAGRANGE
u = vel_x
v = vel_y
pressure = p
temperature = T
porosity = porosity
eos = eos
[]
[Mesh]
[./square]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 0.1
ymin = 0
ymax = 0.1
nx = 20
ny = 20
elem_type = QUAD4
[]
[middle_node]
type = ExtraNodesetGenerator
input = square
new_boundary = 'bottom_left_corner'
coord = '0 0'
[]
[]
[FluidProperties]
[./eos]
type = SimpleFluidProperties
density0 = 100 # kg/m^3
thermal_expansion = 0 # K^{-1}
cp = 1272.0
viscosity = 0.1 # Pa-s, Re=rho*u*L/mu = 100*1*0.1/0.1 = 100
[../]
[]
[Variables]
# velocity
[./vel_x]
scaling = 1.e-1
initial_condition = 0.0
[../]
[./vel_y]
scaling = 1.e-1
initial_condition = 0.0
[../]
# Pressure
[./p]
scaling = 1
initial_condition = 1.0e5
[../]
[]
[AuxVariables]
[rho]
# incompressible flow, rho = constant
initial_condition = 100
[]
[T]
# nothing really depends on T, but eos requires temperature
initial_condition = 800
[]
[porosity]
# nothing really depends on porosity, but PINSFEFluidPressureTimeDerivative requires it
# need make it conditional
initial_condition = 1
[]
[]
[Materials]
[flow_mat]
type = INSFEMaterial
[]
[]
[Kernels]
# mass eqn
[mass_time]
type = PINSFEFluidPressureTimeDerivative
variable = p
[]
[mass_space]
type = INSFEFluidMassKernel
variable = p
[]
# x-momentum eqn
[x_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_x
[]
[x_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_x
component = 0
[]
# y-momentum eqn
[y_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_y
[]
[y_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_y
component = 1
[]
[]
[BCs]
[x_zero]
type = DirichletBC
variable = vel_x
boundary = 'bottom left right'
value = 0
[]
[x_lid]
type = DirichletBC
variable = vel_x
boundary = 'top'
value = 1
[]
[y_zero]
type = DirichletBC
variable = vel_y
boundary = 'bottom top left right'
value = 0
[]
[p_anchor]
type = DirichletBC
variable = p
boundary = 'bottom_left_corner'
value = 1e5
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
solve_type = 'PJFNK'
[]
[]
[Executioner]
type = Transient
dt = 0.01
dtmin = 1.e-4
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
nl_max_its = 10
l_tol = 1e-6
l_max_its = 100
start_time = 0.0
end_time = 2
num_steps = 5
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
time_step_interval = 1
execute_on = 'initial timestep_end'
[./console]
type = Console
output_linear = false
[../]
[./out]
type = Exodus
hide = 'porosity'
[../]
[]
(modules/xfem/test/tests/init_solution_propagation/init_solution_propagation.i)
# The purpose of this test is to verify that the procedures for initializing
# the solution on nodes/elements affected by XFEM works correctly in both
# serial and parallel.
# The crack cuts near to domain boundaries in parallel, and the displacement
# solution will be wrong in parallel if this is not done correctly. This
# test also has multiple aux variables of various types that are only computed
# on initialization, and which will be wrong if the XFEM initializtion
# is not done correctly.
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 7
ny = 7
xmin = 0.0
xmax = 25.0
ymin = -12.5
ymax = 12.5
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_set_uo]
type = LineSegmentCutSetUserObject
cut_data ='0.0000e+000 0.0000e+000 5.5000e+000 0.0000e+000 0.0 0.0
5.5000e+000 0.0000e+000 2.5500e+001 0.0000e+000 0.05 1.05'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./const_monomial]
order = CONSTANT
family = MONOMIAL
[../]
[./first_monomial]
order = FIRST
family = MONOMIAL
[../]
[./first_linear]
order = FIRST
family = LAGRANGE
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
planar_formulation = PLANE_STRAIN
[../]
[]
[AuxKernels]
[./const_monomial]
type = FunctionAux
function = 'dummy'
variable = const_monomial
execute_on = 'initial'
[../]
[./first_monomial]
type = FunctionAux
function = 'dummy'
variable = first_monomial
execute_on = 'initial'
[../]
[./first_linear]
type = FunctionAux
function = 'dummy'
variable = first_linear
execute_on = 'initial'
[../]
[]
[Functions]
[./dummy]
type = ParsedFunction
expression = 'x*x+y*y'
[../]
[./disp_top_y]
type = PiecewiseLinear
x = '0 1'
y = '0 0.1'
[../]
[]
[BCs]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = disp_top_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./right_x]
type = DirichletBC
boundary = 1
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
petsc_options = '-snes_ksp_ew'
l_max_its = 100
nl_max_its = 25
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
start_time = 0.0
dt = 0.1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/edge_crack_3d_propagation.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX8
[]
[UserObjects]
[./cut_mesh]
type = CrackMeshCut3DUserObject
mesh_file = mesh_edge_crack.xda
growth_dir_method = FUNCTION
size_control = 0.1
n_step_growth = 1
growth_direction_x = growth_func_x
growth_direction_y = growth_func_y
growth_direction_z = growth_func_z
growth_rate = growth_func_v
[../]
[]
[Functions]
[./growth_func_x]
type = ParsedFunction
expression = 1
[../]
[./growth_func_y]
type = ParsedFunction
expression = 0
[../]
[./growth_func_z]
type = ParsedFunction
expression = 0
[../]
[./growth_func_v]
type = ParsedFunction
expression = 0.15
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[Functions]
[./top_trac_y]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_y]
type = FunctionNeumannBC
boundary = top
variable = disp_y
function = top_trac_y
[../]
[./bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 3.0
max_xfem_update = 1
[]
[Outputs]
file_base = edge_crack_3d_propagation_out
execute_on = 'timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_1/plane1_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane1_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/solid_mechanics/examples/coal_mining/cosserat_wp_only.i)
# Strata deformation and fracturing around a coal mine
#
# A 2D geometry is used that simulates a transverse section of
# the coal mine. The model is actually 3D, but the "x"
# dimension is only 10m long, meshed with 1 element, and
# there is no "x" displacement. The mine is 300m deep
# and just the roof is studied (0<=z<=300). The model sits
# between 0<=y<=450. The excavation sits in 0<=y<=150. This
# is a "half model": the boundary conditions are such that
# the model simulates an excavation sitting in -150<=y<=150
# inside a model of the region -450<=y<=450. The
# excavation height is 3m (ie, the excavation lies within
# 0<=z<=3). Mining is simulated by moving the excavation's
# roof down, until disp_z=-3 at t=1.
# Time is meaningless in this example
# as quasi-static solutions are sought at each timestep, but
# the number of timesteps controls the resolution of the
# process.
#
# The boundary conditions are:
# - disp_x = 0 everywhere
# - disp_y = 0 at y=0 and y=450
# - disp_z = 0 for y>150
# - disp_z = -3 at maximum, for 0<=y<=150. See excav function.
# That is, rollers on the sides, free at top, and prescribed at bottom.
#
# The small strain formulation is used.
#
# All stresses are measured in MPa. The initial stress is consistent with
# the weight force from density 2500 kg/m^3, ie, stress_zz = -0.025*(300-z) MPa
# where gravity = 10 m.s^-2 = 1E-5 MPa m^2/kg. The maximum and minimum
# principal horizontal stresses are assumed to be equal to 0.8*stress_zz.
#
# Below you will see Drucker-Prager parameters and AuxVariables, etc.
# These are not actally used in this example.
#
# Material properties:
# Young's modulus = 8 GPa
# Poisson's ratio = 0.25
# Cosserat layer thickness = 1 m
# Cosserat-joint normal stiffness = large
# Cosserat-joint shear stiffness = 1 GPa
# Weak-plane cohesion = 0.1 MPa
# Weak-plane friction angle = 20 deg
# Weak-plane dilation angle = 10 deg
# Weak-plane tensile strength = 0.1 MPa
# Weak-plane compressive strength = 100 MPa, varying down to 1 MPa when tensile strain = 1
#
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
xmin = -5
xmax = 5
nz = 40
zmin = 0
zmax = 400
bias_z = 1.1
ny = 30 # make this a multiple of 3, so y=150 is at a node
ymin = 0
ymax = 450
[]
[left]
type = SideSetsAroundSubdomainGenerator
new_boundary = 11
normal = '0 -1 0'
input = generated_mesh
[]
[right]
type = SideSetsAroundSubdomainGenerator
new_boundary = 12
normal = '0 1 0'
input = left
[]
[front]
type = SideSetsAroundSubdomainGenerator
new_boundary = 13
normal = '-1 0 0'
input = right
[]
[back]
type = SideSetsAroundSubdomainGenerator
new_boundary = 14
normal = '1 0 0'
input = front
[]
[top]
type = SideSetsAroundSubdomainGenerator
new_boundary = 15
normal = '0 0 1'
input = back
[]
[bottom]
type = SideSetsAroundSubdomainGenerator
new_boundary = 16
normal = '0 0 -1'
input = top
[]
[excav]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-5 0 0'
top_right = '5 150 3'
input = bottom
[]
[roof]
type = SideSetsBetweenSubdomainsGenerator
new_boundary = 21
primary_block = 0
paired_block = 1
input = excav
[]
[hole]
type = BlockDeletionGenerator
block = 1
input = roof
[]
[]
[GlobalParams]
block = 0
perform_finite_strain_rotations = false
displacements = 'disp_x disp_y disp_z'
Cosserat_rotations = 'wc_x wc_y wc_z'
[]
[Variables]
[./disp_y]
[../]
[./disp_z]
[../]
[./wc_x]
[../]
[]
[Kernels]
[./cy_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_y
component = 1
[../]
[./cz_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_z
component = 2
[../]
[./x_couple]
type = StressDivergenceTensors
use_displaced_mesh = false
variable = wc_x
displacements = 'wc_x wc_y wc_z'
component = 0
base_name = couple
[../]
[./x_moment]
type = MomentBalancing
use_displaced_mesh = false
variable = wc_x
component = 0
[../]
[./gravity]
type = Gravity
use_displaced_mesh = false
variable = disp_z
value = -10E-6
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./wc_y]
[../]
[./wc_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./dp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./dp_shear]
type = MaterialStdVectorAux
index = 0
property = dp_plastic_internal_parameter
variable = dp_shear
[../]
[./dp_tensile]
type = MaterialStdVectorAux
index = 1
property = dp_plastic_internal_parameter
variable = dp_tensile
[../]
[./wp_shear]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_internal_parameter
variable = wp_shear
[../]
[./wp_tensile]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_internal_parameter
variable = wp_tensile
[../]
[./dp_shear_f]
type = MaterialStdVectorAux
index = 0
property = dp_plastic_yield_function
variable = dp_shear_f
[../]
[./dp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = dp_plastic_yield_function
variable = dp_tensile_f
[../]
[./wp_shear_f]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_yield_function
variable = wp_shear_f
[../]
[./wp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_yield_function
variable = wp_tensile_f
[../]
[]
[BCs]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '11 12 16 21' # note addition of 16 and 21
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '16'
value = 0.0
[../]
[./no_wc_x]
type = DirichletBC
variable = wc_x
boundary = '11 12'
value = 0.0
[../]
[./roof]
type = FunctionDirichletBC
variable = disp_z
boundary = 21
function = excav_sideways
[../]
[]
[Functions]
[./ini_xx]
type = ParsedFunction
expression = '-0.8*2500*10E-6*(400-z)'
[../]
[./ini_zz]
type = ParsedFunction
expression = '-2500*10E-6*(400-z)'
[../]
[./excav_sideways]
type = ParsedFunction
symbol_names = 'end_t ymin ymax e_h closure_dist'
symbol_values = '1.0 0 150.0 -3.0 15.0'
expression = 'e_h*max(min((t/end_t*(ymax-ymin)+ymin-y)/closure_dist,1),0)'
[../]
[./excav_downwards]
type = ParsedFunction
symbol_names = 'end_t ymin ymax e_h closure_dist'
symbol_values = '1.0 0 150.0 -3.0 15.0'
expression = 'e_h*t/end_t*max(min(((ymax-ymin)+ymin-y)/closure_dist,1),0)'
[../]
[]
[UserObjects]
[./dp_coh_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 2.9 # MPa
value_residual = 3.1 # MPa
rate = 1.0
[../]
[./dp_fric]
type = SolidMechanicsHardeningConstant
value = 0.65 # 37deg
[../]
[./dp_dil]
type = SolidMechanicsHardeningConstant
value = 0.65
[../]
[./dp_tensile_str_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 1.0 # MPa
value_residual = 1.4 # MPa
rate = 1.0
[../]
[./dp_compressive_str]
type = SolidMechanicsHardeningConstant
value = 1.0E3 # Large!
[../]
[./drucker_prager_model]
type = SolidMechanicsPlasticDruckerPrager
mc_cohesion = dp_coh_strong_harden
mc_friction_angle = dp_fric
mc_dilation_angle = dp_dil
internal_constraint_tolerance = 1 # irrelevant here
yield_function_tolerance = 1 # irrelevant here
[../]
[./wp_coh_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_tan_fric]
type = SolidMechanicsHardeningConstant
value = 0.36 # 20deg
[../]
[./wp_tan_dil]
type = SolidMechanicsHardeningConstant
value = 0.18 # 10deg
[../]
[./wp_tensile_str_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_compressive_str_soften]
type = SolidMechanicsHardeningCubic
value_0 = 100
value_residual = 1.0
internal_limit = 1.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeLayeredCosseratElasticityTensor
young = 8E3 # MPa
poisson = 0.25
layer_thickness = 1.0
joint_normal_stiffness = 1E9 # huge
joint_shear_stiffness = 1E3
[../]
[./strain]
type = ComputeCosseratIncrementalSmallStrain
eigenstrain_names = ini_stress
[../]
[./ini_stress]
type = ComputeEigenstrainFromInitialStress
initial_stress = 'ini_xx 0 0 0 ini_xx 0 0 0 ini_zz'
eigenstrain_name = ini_stress
[../]
[./stress]
type = ComputeMultipleInelasticCosseratStress
block = 0
inelastic_models = 'wp'
relative_tolerance = 2.0
absolute_tolerance = 1E6
max_iterations = 1
tangent_operator = nonlinear
perform_finite_strain_rotations = false
[../]
[./dp]
type = CappedDruckerPragerCosseratStressUpdate
block = 0
warn_about_precision_loss = false
host_youngs_modulus = 8E3
host_poissons_ratio = 0.25
base_name = dp
DP_model = drucker_prager_model
tensile_strength = dp_tensile_str_strong_harden
compressive_strength = dp_compressive_str
max_NR_iterations = 100000
tip_smoother = 0.1E1
smoothing_tol = 0.1E1 # MPa # Must be linked to cohesion
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0
[../]
[./wp]
type = CappedWeakPlaneCosseratStressUpdate
block = 0
warn_about_precision_loss = false
base_name = wp
cohesion = wp_coh_harden
tan_friction_angle = wp_tan_fric
tan_dilation_angle = wp_tan_dil
tensile_strength = wp_tensile_str_harden
compressive_strength = wp_compressive_str_soften
max_NR_iterations = 10000
tip_smoother = 0.1
smoothing_tol = 0.1 # MPa # Note, this must be tied to cohesion, otherwise get no possible return at cone apex
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0E-3
[../]
[./density]
type = GenericConstantMaterial
prop_names = density
prop_values = 2500
[../]
[]
[Postprocessors]
[./subsidence]
type = PointValue
point = '0 0 400'
variable = disp_z
use_displaced_mesh = false
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
line_search = bt
nl_abs_tol = 1e-3
nl_rel_tol = 1e-5
l_max_its = 30
nl_max_its = 1000
start_time = 0.0
dt = 0.2
end_time = 0.2
[]
[Outputs]
file_base = cosserat_wp_only
time_step_interval = 1
print_linear_residuals = false
csv = true
exodus = true
[./console]
type = Console
output_linear = false
[../]
[]
(test/tests/multiapps/multilevel/time_dt_from_parent_parent.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 100
[]
[Functions]
[./dts]
type = PiecewiseLinear
x = '0 1'
y = '0.25 1'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 4
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
dt = 0.25
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
exodus = true
[./out]
type = Console
output_file = true
[../]
[]
[MultiApps]
[./sub]
type = TransientMultiApp
app_type = MooseTestApp
positions = '0 0 0 0.5 0.5 0'
input_files = time_dt_from_parent_sub.i
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_4/plane4_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane4_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 200
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(test/tests/postprocessors/pps_interval/pps_interval_mismatch.i)
[Mesh]
file = square-2x2-nodeids.e
# This test can only be run with renumering disabled, so the
# NodalVariableValue postprocessor's node id is well-defined.
allow_renumbering = false
[]
[Variables]
active = 'u v'
[./u]
order = SECOND
family = LAGRANGE
[../]
[./v]
order = SECOND
family = LAGRANGE
[../]
[]
[Functions]
active = 'force_fn exact_fn left_bc'
[./force_fn]
type = ParsedFunction
expression = '1-x*x+2*t'
[../]
[./exact_fn]
type = ParsedFunction
expression = '(1-x*x)*t'
[../]
[./left_bc]
type = ParsedFunction
expression = t
[../]
[]
[Kernels]
active = '
time_u diff_u ffn_u
time_v diff_v'
[./time_u]
type = TimeDerivative
variable = u
[../]
[./diff_u]
type = Diffusion
variable = u
[../]
[./ffn_u]
type = BodyForce
variable = u
function = force_fn
[../]
[./time_v]
type = TimeDerivative
variable = v
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[BCs]
active = 'all_u left_v right_v'
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = '1'
function = exact_fn
[../]
[./left_v]
type = FunctionDirichletBC
variable = v
boundary = '3'
function = left_bc
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = '2'
value = 0
[../]
[]
[Postprocessors]
active = 'l2 node1 node4'
[./l2]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[./node1]
type = NodalVariableValue
variable = u
nodeid = 15
[../]
[./node4]
type = NodalVariableValue
variable = v
nodeid = 10
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
dt = 0.1
start_time = 0
end_time = 1
[]
[Outputs]
time_step_interval = 4
exodus = true
[./console]
type = Console
time_step_interval = 3
[../]
[]
(test/tests/userobjects/toggle_mesh_adaptivity/toggle_mesh_adaptivity_wait.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Problem]
solve = false
[]
[Executioner]
type = Transient
num_steps = 4
dt = 0.1
[]
[Adaptivity]
cycles_per_step = 1
marker = marker
max_h_level = 4
[./Markers]
[./marker]
type = BoxMarker
bottom_left = '0.35 0.25 0'
top_right = '0.5 0.5 0'
inside = refine
outside = coarsen
[../]
[../]
[]
[UserObjects]
[./mesh_adaptivity_off]
type = ToggleMeshAdaptivity
mesh_adaptivity = 'off'
apply_after_timestep = 1
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/2D_xy_homog1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: 2D
# Coordinate System: xy
# Material Numbers/Types: homogeneous 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# Transient 2D heat transfer problem in Cartesian coordinates designed with
# the Method of Manufactured Solutions. This problem was developed to verify
# XFEM performance on linear elements in the presence of a moving interface
# sweeping across the x-y coordinates of a system with homogeneous material
# properties. This problem can be exactly evaluated by FEM/Moose without the
# moving interface. Both the temperature and level set function are designed
# to be linear to attempt to minimize error between the Moose/exact solution
# and XFEM results.
# Results:
# The temperature at the bottom left boundary (x=0, y=0) exhibits the largest
# difference between the FEM/Moose solution and XFEM results. We present the
# XFEM results at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 479.9998791
# 0.6 520 519.9995307
# 0.8 560 559.9989724
# 1.0 600 599.9984541
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraints]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-100*x-100*y+200)'
[../]
[./neumann_func]
type = ParsedFunction
expression = '1.5*100*t'
[../]
[./dirichlet_right_func]
type = ParsedFunction
expression = '(-100*y+100)*t+400'
[../]
[./dirichlet_top_func]
type = ParsedFunction
expression = '(-100*x+100)*t+400'
[../]
[./ls_func]
type = ParsedFunction
expression = '-0.5*(x+y) + 1.04 - 0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericConstantMaterial
prop_names = 'diffusion_coefficient'
prop_values = 1.5
[../]
[]
[BCs]
[./left_du]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = FunctionDirichletBC
variable = u
boundary = 'right'
function = dirichlet_right_func
[../]
[./bottom_du]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = neumann_func
[../]
[./top_u]
type = FunctionDirichletBC
variable = u
boundary = 'top'
function = dirichlet_top_func
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/inelastic_strain/creep/creep_nl1.i)
#
# Test for effective strain calculation.
# Boundary conditions from NAFEMS test NL1
#
# This is not a verification test. This is the creep analog of the same test
# in the elas_plas directory. Instead of using the IsotropicPlasticity
# material model this test uses the PowerLawCreep material model.
#
[GlobalParams]
temperature = temp
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = one_elem2.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./temp]
initial_condition = 600.0
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./creep_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./eff_creep_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
decomposition_method = EigenSolution
[../]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
execute_on = timestep_end
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain_zz]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./creep_strain_xx]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./creep_strain_yy]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./creep_strain_zz]
type = RankTwoAux
rank_two_tensor = creep_strain
variable = creep_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./tot_strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_xx
index_i = 0
index_j = 0
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
[../]
[./tot_strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_zz
index_i = 2
index_j = 2
[../]
[./eff_creep_strain]
type = MaterialRealAux
property = effective_creep_strain
variable = eff_creep_strain
[../]
[]
[Functions]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0'
y = '0.0 0.25e-4 0.50e-4'
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[./temp_fix]
type = DirichletBC
variable = temp
boundary = '1 2'
value = 600.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./radial_return_stress]
type = ComputeMultipleInelasticStress
block = 1
inelastic_models = 'powerlawcrp'
[../]
[./powerlawcrp]
type = PowerLawCreepStressUpdate
block = 1
coefficient = 3.125e-14
n_exponent = 5.0
m_exponent = 0.0
activation_energy = 0.0
[../]
[./thermal]
type = HeatConductionMaterial
block = 1
specific_heat = 1.0
thermal_conductivity = 100.
[../]
[./density]
type = Density
block = 1
density = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-6
l_max_its = 100
nl_max_its = 20
dt = 1.0
start_time = 0.0
num_steps = 100
end_time = 2.0
[]
[Postprocessors]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./stress_xy]
type = ElementAverageValue
variable = stress_xy
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./el_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./el_strain_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[./crp_strain_xx]
type = ElementAverageValue
variable = creep_strain_xx
[../]
[./crp_strain_yy]
type = ElementAverageValue
variable = creep_strain_yy
[../]
[./crp_strain_zz]
type = ElementAverageValue
variable = creep_strain_zz
[../]
[./eff_creep_strain]
type = ElementAverageValue
variable = eff_creep_strain
[../]
[./tot_strain_xx]
type = ElementAverageValue
variable = tot_strain_xx
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./tot_strain_zz]
type = ElementAverageValue
variable = tot_strain_zz
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_4/cyl4_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl4_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_2/cyl2_template2.i)
#
# This input file is a template for both the frictionless and glued test
# variations for the current problem geometry. In order to create an input
# file to run outside the runtest framework, look at the tests file and add the
# appropriate input file lines from the cli_args line.
#
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl2_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/xfem/test/tests/high_order_elements/square_branch_2d.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = TRI6
[]
[UserObjects]
[./line_seg_cut_set_uo]
type = LineSegmentCutSetUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10 0.0 1.0
3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01 1.0 2.0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 10'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/functions/piecewise_linear_from_vectorpostprocessor/vector_postprocessor_function.i)
# This function linearly interpolates the data generated by a vector post
# processor. The purpose is to have a function take points and a field variable
# (aux or primary) as arguments.
# It also uses a ConstantVectorPostprocessor to test that parallel syncing is
# working for VectorPostprocessorFunction.
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 4
xmin = 0.0
xmax = 0.004
ymin = 0.0
ymax = 0.008
[]
[Variables]
[u]
initial_condition = 0
[]
[]
[AuxVariables]
[v]
initial_condition = 1
[]
[test_parallel]
[]
[]
[Functions]
[ramp_u]
type = ParsedFunction
expression = 't'
[]
[point_value_function_u]
type = VectorPostprocessorFunction
component = y
argument_column = y
value_column = u
vectorpostprocessor_name = point_value_vector_postprocessor_u
[]
[line_value_function_v]
type = VectorPostprocessorFunction
component = y
argument_column = y
value_column = v
vectorpostprocessor_name = line_value_vector_postprocessor_v
[]
[test_parallel_func]
type = VectorPostprocessorFunction
component = x
argument_column = xx
value_column = qq
vectorpostprocessor_name = test_parallel_vpp
[]
[function_v]
type = PiecewiseLinear
x = '0 0.008'
y = '1 2'
axis = y
[]
[]
[Kernels]
[diffusion_u]
type = Diffusion
variable = u
[]
[]
[AuxKernels]
[aux_v]
type = FunctionAux
variable = v
function = function_v
execute_on = 'TIMESTEP_BEGIN'
[]
[test_parallel]
type = FunctionAux
variable = test_parallel
function = test_parallel_func
execute_on = 'TIMESTEP_END'
[]
[]
[BCs]
[top_u]
type = FunctionDirichletBC
boundary = top
variable = u
function = ramp_u
[]
[bottom_u]
type = DirichletBC
boundary = bottom
variable = u
value = 0
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package -ksp_gmres_restart'
petsc_options_value = ' lu superlu_dist 51'
line_search = 'none'
l_max_its = 50
l_tol = 1e-3
nl_max_its = 20
nl_rel_tol = 1e-4
nl_abs_tol = 1e-6
start_time = 0
num_steps = 1
dt = 1
[]
[Postprocessors]
[point_value_postprocessor_u]
type = FunctionValuePostprocessor
function = point_value_function_u
point = '0.002 0.004 0'
[]
[line_value_postprocessor_v]
type = FunctionValuePostprocessor
function = line_value_function_v
point = '0.002 0.004 0'
[]
[postprocessor_average_u]
type = ElementAverageValue
variable = u
[]
[postprocessor_average_v]
type = ElementAverageValue
variable = v
[]
[]
[VectorPostprocessors]
[point_value_vector_postprocessor_u]
type = PointValueSampler
variable = u
points = '0 0.001 0 0 0.004 0 0 0.008 0'
#points = '0.001 0 0 0.002 0 0'
sort_by = y
execute_on = linear
[]
[line_value_vector_postprocessor_v]
type = LineValueSampler
variable = v
start_point = '0 0.001 0'
end_point = '0 0.008 0'
num_points = 5
sort_by = y
execute_on = linear
[]
[test_parallel_vpp]
type = ConstantVectorPostprocessor
vector_names = 'xx qq'
value = '0 1;
1000 1000'
execute_on = 'initial timestep_begin'
[]
[]
[Outputs]
time_step_interval = 1
csv = false
exodus = true
file_base = out
[console]
type = Console
output_linear = true
max_rows = 10
[]
[]
(modules/contact/test/tests/verification/patch_tests/brick_4/brick4_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick4_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x59]
type = NodalVariableValue
nodeid = 58
variable = disp_x
[../]
[./disp_x64]
type = NodalVariableValue
nodeid = 63
variable = disp_x
[../]
[./disp_y59]
type = NodalVariableValue
nodeid = 58
variable = disp_y
[../]
[./disp_y64]
type = NodalVariableValue
nodeid = 63
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x59 disp_y59 disp_x64 disp_y64 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_1/cyl1_template2.i)
#
# This input file is a template for both the frictionless and glued test
# variations for the current problem geometry. In order to create an input
# file to run outside the runtest framework, look at the tests file and add the
# appropriate input file lines from the cli_args line.
#
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl1_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/optimization/test/tests/executioners/transient_and_adjoint/nonuniform_tstep.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[]
[Problem]
nl_sys_names = 'nl0 adjoint'
[]
[Variables]
[u]
[]
[u_adjoint]
solver_sys = adjoint
[]
[]
[Kernels]
[time]
type = TimeDerivative
variable = u
[]
[diff]
type = Diffusion
variable = u
[]
[src]
type = BodyForce
variable = u
value = 10
[]
[src_adjoint]
type = BodyForce
variable = u_adjoint
value = 100
[]
[]
[BCs]
[dirichlet]
type = DirichletBC
variable = u
boundary = 'top right'
value = 0
[]
[]
[Executioner]
type = TransientAndAdjoint
forward_system = nl0
adjoint_system = adjoint
[TimeStepper]
type = TimeSequenceStepper
time_sequence = '0 0.1 0.2 0.4 0.7 1.1 1.4 1.6 1.7'
[]
end_time = 1.7
nl_rel_tol = 1e-12
l_tol = 1e-12
[]
[Postprocessors]
[u_avg]
type = ElementAverageValue
variable = u
execute_on = 'TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[u_adjoint_avg]
type = ElementAverageValue
variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[inner_product]
type = VariableInnerProduct
variable = u
second_variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[]
[Outputs]
[forward]
type = CSV
[]
[adjoint]
type = CSV
execute_on = 'INITIAL ADJOINT_TIMESTEP_END'
[]
[console]
type = Console
execute_postprocessors_on = 'INITIAL TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[]
(modules/xfem/test/tests/moment_fitting/diffusion_moment_fitting_six_points.i)
# Test for a diffusion problem which uses six points moment_fitting approach.
# To use six points rule, add Quadrature block with order = FOURTH and type = MONOMIAL.
# See this paper (https://doi.org/10.1007/s00466-018-1544-2) for more details about moment_fitting approach.
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
[./Quadrature]
order = FOURTH
type = MONOMIAL
[../]
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/high_order_elements/diffusion_quad9_levelsetcut.i)
# A simple diffusion problem with quad9 elements
# The mesh is cut using levle set based cutter
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD9
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[./ls_func]
type = ParsedFunction
expression = 'x-0.53'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/axisymmetric_2d3d_solution_function/3dy.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 3dy.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./temp]
[../]
[./hoop_stress]
order = CONSTANT
family = MONOMIAL
[../]
[]
[UserObjects]
[./soln]
type = SolutionUserObject
mesh = 2d_out.e
system_variables = 'disp_x disp_y temp'
[../]
[]
[Functions]
[./soln_func_temp]
type = Axisymmetric2D3DSolutionFunction
solution = soln
from_variables = 'temp'
[../]
[./soln_func_disp_x]
type = Axisymmetric2D3DSolutionFunction
solution = soln
from_variables = 'disp_x disp_y'
component = 0
[../]
[./soln_func_disp_y]
type = Axisymmetric2D3DSolutionFunction
solution = soln
from_variables = 'disp_x disp_y'
component = 1
[../]
[./soln_func_disp_z]
type = Axisymmetric2D3DSolutionFunction
solution = soln
from_variables = 'disp_x disp_y'
component = 2
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
volumetric_locking_correction = true
add_variables = true
incremental = true
strain = FINITE
eigenstrain_names = thermal_expansion
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress hydrostatic_stress'
[../]
[]
[AuxKernels]
[./t_soln_aux]
type = FunctionAux
variable = temp
block = '1 2'
function = soln_func_temp
[../]
[./hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[../]
[]
[BCs]
[./x_soln_bc]
type = FunctionDirichletBC
variable = disp_x
preset = false
boundary = '1 2'
function = soln_func_disp_x
[../]
[./y_soln_bc]
type = FunctionDirichletBC
variable = disp_y
preset = false
boundary = '1 2'
function = soln_func_disp_y
[../]
[./z_soln_bc]
type = FunctionDirichletBC
variable = disp_z
preset = false
boundary = '1 2'
function = soln_func_disp_z
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 193.05e9
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
block = '1 2'
thermal_expansion_coeff = 13e-6
stress_free_temperature = 295.00
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
block = '1'
density = 8000.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-ksp_snes_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 25
nl_max_its = 20
nl_rel_tol = 1e-10
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
dtmin = 1
[]
[Outputs]
file_base = 3dy_out
exodus = true
[./console]
type = Console
max_rows = 25
[../]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/01_flow_channel.i)
T_in = 300. # K
m_dot_in = 1e-2 # kg/s
press = 10e5 # Pa
[GlobalParams]
initial_p = ${press}
initial_vel = 0.0001
initial_T = ${T_in}
gravity_vector = '0 0 0'
rdg_slope_reconstruction = minmod
scaling_factor_1phase = '1 1e-2 1e-4'
closures = thm_closures
fp = he
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[]
[Closures]
[thm_closures]
type = Closures1PhaseTHM
[]
[]
[Components]
[inlet]
type = InletMassFlowRateTemperature1Phase
input = 'core_chan:in'
m_dot = ${m_dot_in}
T = ${T_in}
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 1
n_elems = 25
A = 7.2548e-3
D_h = 7.0636e-2
[]
[outlet]
type = Outlet1Phase
input = 'core_chan:out'
p = ${press}
[]
[]
[Postprocessors]
[core_p_in]
type = SideAverageValue
boundary = core_chan:in
variable = p
[]
[core_p_out]
type = SideAverageValue
boundary = core_chan:out
variable = p
[]
[core_delta_p]
type = ParsedPostprocessor
pp_names = 'core_p_in core_p_out'
expression = 'core_p_in - core_p_out'
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
line_search = basic
start_time = 0
end_time = 1000
dt = 10
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 25
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/test/tests/problems/brayton_cycle/open_brayton_cycle.i)
# This input file is used to demonstrate a simple open-air Brayton cycle using
# a compressor, turbine, shaft, motor, and generator.
# The flow length is divided into 5 segments as illustrated below, where
# - "(I)" denotes the inlet
# - "(C)" denotes the compressor
# - "(T)" denotes the turbine
# - "(O)" denotes the outlet
# - "*" denotes a fictitious junction
#
# Heated section
# (I)-----(C)-----*--------------*-----(T)-----(O)
# 1 2 3 4 5
#
# Initially the fluid is at rest at ambient conditions, the shaft speed is zero,
# and no heat transfer occurs with the system.
# The transient is controlled as follows:
# * 0 - 100 s: motor ramps up torque linearly from zero
# * 100 - 200 s: motor ramps down torque linearly to zero, HTC ramps up linearly from zero.
# * 200 - 300 s: (no changes; should approach steady condition)
I_motor = 1.0
motor_torque_max = 400.0
I_generator = 1.0
generator_torque_per_shaft_speed = -0.00025
motor_ramp_up_duration = 100.0
motor_ramp_down_duration = 100.0
post_motor_time = 100.0
t1 = ${motor_ramp_up_duration}
t2 = ${fparse t1 + motor_ramp_down_duration}
t3 = ${fparse t2 + post_motor_time}
D1 = 0.15
D2 = ${D1}
D3 = ${D1}
D4 = ${D1}
D5 = ${D1}
A1 = ${fparse 0.25 * pi * D1^2}
A2 = ${fparse 0.25 * pi * D2^2}
A3 = ${fparse 0.25 * pi * D3^2}
A4 = ${fparse 0.25 * pi * D4^2}
A5 = ${fparse 0.25 * pi * D5^2}
L1 = 10.0
L2 = ${L1}
L3 = ${L1}
L4 = ${L1}
L5 = ${L1}
x1 = 0.0
x2 = ${fparse x1 + L1}
x3 = ${fparse x2 + L2}
x4 = ${fparse x3 + L3}
x5 = ${fparse x4 + L4}
x2_minus = ${fparse x2 - 0.001}
x2_plus = ${fparse x2 + 0.001}
x5_minus = ${fparse x5 - 0.001}
x5_plus = ${fparse x5 + 0.001}
n_elems1 = 10
n_elems2 = ${n_elems1}
n_elems3 = ${n_elems1}
n_elems4 = ${n_elems1}
n_elems5 = ${n_elems1}
A_ref_comp = ${fparse 0.5 * (A1 + A2)}
V_comp = ${fparse A_ref_comp * 1.0}
I_comp = 1.0
A_ref_turb = ${fparse 0.5 * (A4 + A5)}
V_turb = ${fparse A_ref_turb * 1.0}
I_turb = 1.0
c0_rated_comp = 351.6925137
rho0_rated_comp = 1.146881112
rated_mfr = 0.25
speed_rated_rpm = 96000
speed_rated = ${fparse speed_rated_rpm * 2 * pi / 60.0}
speed_initial = 0
eff_comp = 0.79
eff_turb = 0.843
T_hot = 1000
T_ambient = 300
p_ambient = 1e5
[GlobalParams]
orientation = '1 0 0'
gravity_vector = '0 0 0'
initial_p = ${p_ambient}
initial_T = ${T_ambient}
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
fp = fp_air
closures = closures
f = 0
scaling_factor_1phase = '1 1 1e-5'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1
scaling_factor_rhovV = 1
scaling_factor_rhowV = 1
scaling_factor_rhoEV = 1e-5
rdg_slope_reconstruction = none
[]
[Functions]
[motor_torque_fn]
type = PiecewiseLinear
x = '0 ${t1} ${t2}'
y = '0 ${motor_torque_max} 0'
[]
[motor_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'motor_torque shaft:omega'
[]
[generator_torque_fn]
type = ParsedFunction
expression = 'slope * t'
symbol_names = 'slope'
symbol_values = '${generator_torque_per_shaft_speed}'
[]
[generator_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'generator_torque shaft:omega'
[]
[htc_wall_fn]
type = PiecewiseLinear
x = '0 ${t1} ${t2}'
y = '0 0 1e3'
[]
[]
[FluidProperties]
[fp_air]
type = IdealGasFluidProperties
emit_on_nan = none
[]
[]
[Closures]
[closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[shaft]
type = Shaft
connected_components = 'motor compressor turbine generator'
initial_speed = ${speed_initial}
[]
[motor]
type = ShaftConnectedMotor
inertia = ${I_motor}
torque = 0 # controlled
[]
[generator]
type = ShaftConnectedMotor
inertia = ${I_generator}
torque = generator_torque_fn
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = ${p_ambient}
T0 = ${T_ambient}
[]
[pipe1]
type = FlowChannel1Phase
position = '${x1} 0 0'
length = ${L1}
n_elems = ${n_elems1}
A = ${A1}
[]
[compressor]
type = ShaftConnectedCompressor1Phase
position = '${x2} 0 0'
inlet = 'pipe1:out'
outlet = 'pipe2:in'
A_ref = ${A_ref_comp}
volume = ${V_comp}
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
speeds = '0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_comp1 rp_comp2 rp_comp3 rp_comp4 rp_comp5'
eff_functions = 'eff_comp1 eff_comp2 eff_comp3 eff_comp4 eff_comp5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_comp}
inertia_coeff = '${I_comp} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
[pipe2]
type = FlowChannel1Phase
position = '${x2} 0 0'
length = ${L2}
n_elems = ${n_elems2}
A = ${A2}
[]
[junction2_3]
type = JunctionOneToOne1Phase
connections = 'pipe2:out pipe3:in'
[]
[pipe3]
type = FlowChannel1Phase
position = '${x3} 0 0'
length = ${L3}
n_elems = ${n_elems3}
A = ${A3}
[]
[junction3_4]
type = JunctionOneToOne1Phase
connections = 'pipe3:out pipe4:in'
[]
[pipe4]
type = FlowChannel1Phase
position = '${x4} 0 0'
length = ${L4}
n_elems = ${n_elems4}
A = ${A4}
[]
[turbine]
type = ShaftConnectedCompressor1Phase
position = '${x5} 0 0'
inlet = 'pipe4:out'
outlet = 'pipe5:in'
A_ref = ${A_ref_turb}
volume = ${V_turb}
treat_as_turbine = true
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
speeds = '0 0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_turb0 rp_turb1 rp_turb2 rp_turb3 rp_turb4 rp_turb5'
eff_functions = 'eff_turb1 eff_turb1 eff_turb2 eff_turb3 eff_turb4 eff_turb5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_turb}
inertia_coeff = '${I_turb} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
[pipe5]
type = FlowChannel1Phase
position = '${x5} 0 0'
length = ${L5}
n_elems = ${n_elems5}
A = ${A5}
[]
[outlet]
type = Outlet1Phase
input = 'pipe5:out'
p = ${p_ambient}
[]
[heating]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = pipe3
T_wall = ${T_hot}
Hw = htc_wall_fn
[]
[]
[ControlLogic]
[motor_ctrl]
type = TimeFunctionComponentControl
component = motor
parameter = torque
function = motor_torque_fn
[]
[]
[Postprocessors]
[heating_rate]
type = ADHeatRateConvection1Phase
block = 'pipe3'
T = T
T_wall = T_wall
Hw = Hw
P_hf = P_hf
execute_on = 'INITIAL TIMESTEP_END'
[]
[motor_torque]
type = RealComponentParameterValuePostprocessor
component = motor
parameter = torque
execute_on = 'INITIAL TIMESTEP_END'
[]
[motor_power]
type = FunctionValuePostprocessor
function = motor_power_fn
execute_on = 'INITIAL TIMESTEP_END'
indirect_dependencies = 'motor_torque shaft:omega'
[]
[generator_torque]
type = ShaftConnectedComponentPostprocessor
quantity = torque
shaft_connected_component_uo = generator:shaftconnected_uo
execute_on = 'INITIAL TIMESTEP_END'
[]
[generator_power]
type = FunctionValuePostprocessor
function = generator_power_fn
execute_on = 'INITIAL TIMESTEP_END'
indirect_dependencies = 'generator_torque shaft:omega'
[]
[shaft_speed]
type = ScalarVariable
variable = 'shaft:omega'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_in_comp]
type = PointValue
variable = p
point = '${x2_minus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_comp]
type = PointValue
variable = p
point = '${x2_plus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_comp]
type = ParsedPostprocessor
pp_names = 'p_in_comp p_out_comp'
expression = 'p_out_comp / p_in_comp'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_in_turb]
type = PointValue
variable = p
point = '${x5_minus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_turb]
type = PointValue
variable = p
point = '${x5_plus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_turb]
type = ParsedPostprocessor
pp_names = 'p_in_turb p_out_turb'
expression = 'p_in_turb / p_out_turb'
execute_on = 'INITIAL TIMESTEP_END'
[]
[mfr_comp]
type = ADFlowJunctionFlux1Phase
boundary = pipe1:out
connection_index = 0
equation = mass
junction = compressor
[]
[mfr_turb]
type = ADFlowJunctionFlux1Phase
boundary = pipe4:out
connection_index = 0
equation = mass
junction = turbine
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
end_time = ${t3}
dt = 0.1
abort_on_solve_fail = true
solve_type = NEWTON
nl_rel_tol = 1e-50
nl_abs_tol = 1e-11
nl_max_its = 15
l_tol = 1e-4
l_max_its = 10
[]
[Outputs]
[csv]
type = CSV
file_base = 'open_brayton_cycle'
execute_vector_postprocessors_on = 'INITIAL'
[]
[console]
type = Console
show = 'shaft_speed p_ratio_comp p_ratio_turb compressor:pressure_ratio turbine:pressure_ratio'
[]
[]
[Functions]
# compressor pressure ratio
[rp_comp1]
type = PiecewiseLinear
data_file = 'rp_comp1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp2]
type = PiecewiseLinear
data_file = 'rp_comp2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp3]
type = PiecewiseLinear
data_file = 'rp_comp3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp4]
type = PiecewiseLinear
data_file = 'rp_comp4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp5]
type = PiecewiseLinear
data_file = 'rp_comp5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# compressor efficiency
[eff_comp1]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp2]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp3]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp4]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp5]
type = ConstantFunction
value = ${eff_comp}
[]
# turbine pressure ratio
[rp_turb0]
type = ConstantFunction
value = 1
[]
[rp_turb1]
type = PiecewiseLinear
data_file = 'rp_turb1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb2]
type = PiecewiseLinear
data_file = 'rp_turb2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb3]
type = PiecewiseLinear
data_file = 'rp_turb3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb4]
type = PiecewiseLinear
data_file = 'rp_turb4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb5]
type = PiecewiseLinear
data_file = 'rp_turb5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# turbine efficiency
[eff_turb1]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb2]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb3]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb4]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb5]
type = ConstantFunction
value = ${eff_turb}
[]
[]
(modules/xfem/test/tests/single_var_constraint_3d/stationary_equal_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.25
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.5 -0.001 -0.001
0.5 1.001 -0.001
0.5 1.001 1.001
0.5 -0.001 1.001'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 0
geometric_cut_userobject = 'square_planar_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/time_integrators/explicit-euler/ee-2d-linear.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = (x+y)
[../]
[./exact_fn]
type = ParsedFunction
expression = t*(x+y)
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
lumping = true
implicit = true
[../]
[./diff]
type = Diffusion
variable = u
implicit = false
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
implicit = false
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1 2 3'
function = exact_fn
implicit = true
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
scheme = 'explicit-euler'
solve_type = 'LINEAR'
start_time = 0.0
num_steps = 20
dt = 0.00005
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/stationary_equal.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_1/brick1_template2.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick1_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x8]
type = NodalVariableValue
nodeid = 7
variable = disp_x
[../]
[./disp_x13]
type = NodalVariableValue
nodeid = 12
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y8]
type = NodalVariableValue
nodeid = 7
variable = disp_y
[../]
[./disp_y13]
type = NodalVariableValue
nodeid = 12
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_x8 disp_x13 disp_x16 disp_y5 disp_y8 disp_y13 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 5e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_4/ring4_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring4_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = ring4_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = ring4_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(test/tests/multiapps/picard_multilevel/2level_picard/sub_level1.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[v]
[]
[]
[AuxVariables]
[u]
[]
[w]
[]
[]
[Kernels]
[time_derivative]
type = TimeDerivative
variable = v
[]
[diffusion]
type = Diffusion
variable = v
[]
[source]
type = CoupledForce
variable = v
v = u
[]
[]
[BCs]
[dirichlet0]
type = DirichletBC
variable = v
boundary = '0'
value = 0
[]
[dirichlet]
type = DirichletBC
variable = v
boundary = '2'
value = 100
[]
[]
[Postprocessors]
[avg_u]
type = ElementAverageValue
variable = u
execute_on = 'initial timestep_begin timestep_end'
[]
[avg_v]
type = ElementAverageValue
variable = v
execute_on = 'initial timestep_begin timestep_end'
[]
[avg_w]
type = ElementAverageValue
variable = w
execute_on = 'initial timestep_begin timestep_end'
[]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
end_time = 0.1
dt = 0.02
[]
[MultiApps]
[level2-]
type = TransientMultiApp
app_type = MooseTestApp
positions = '0 0 0'
input_files = sub_level2.i
execute_on = 'timestep_end'
[]
[]
[Transfers]
[v_to_sub]
type = MultiAppGeneralFieldShapeEvaluationTransfer
source_variable = v
variable = v
to_multi_app = level2-
execute_on = 'timestep_end'
[]
[w_from_sub]
type = MultiAppGeneralFieldShapeEvaluationTransfer
source_variable = w
variable = w
from_multi_app = level2-
execute_on = 'timestep_end'
[]
[]
[Outputs]
exodus = true
perf_graph = true
[screen]
type = Console
execute_postprocessors_on = "timestep_end timestep_begin"
[]
[]
(modules/combined/test/tests/heat_conduction_xfem/heat.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./temp]
initial_condition = 300.0 # set initial temp to ambient
[../]
[]
[Functions]
[./temp_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./heat] # gradient term in heat conduction equation
type = HeatConduction
variable = temp
[../]
[]
[BCs]
# Define boundary conditions
[./left_temp]
type = FunctionDirichletBC
variable = temp
boundary = 3
function = temp_left
[../]
[./right_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 0
[../]
[]
[Materials]
[./fuel_thermal]
type = HeatConductionMaterial
block = 0
temp = temp
thermal_conductivity = 5.0
specific_heat = 1.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
l_max_its = 100
l_tol = 8e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 2
[]
[Outputs]
# Define output file(s)
file_base = heat_out
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/phase_field/examples/measure_interface_energy/1Dinterface_energy.i)
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmax = 100
xmin = 0
elem_type = EDGE
[]
[AuxVariables]
[./local_energy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./local_free_energy]
type = TotalFreeEnergy
variable = local_energy
kappa_names = kappa_c
interfacial_vars = c
[../]
[]
[Variables]
[./c]
order = FIRST
family = LAGRANGE
scaling = 1e1
[./InitialCondition]
type = RampIC
variable = c
value_left = 0
value_right = 1
[../]
[../]
[./w]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./c_res]
type = SplitCHParsed
variable = c
f_name = F
kappa_name = kappa_c
w = w
[../]
[./w_res]
type = SplitCHWRes
variable = w
mob_name = M
[../]
[./time]
type = CoupledTimeDerivative
variable = w
v = c
[../]
[]
[Functions]
[./Int_energy]
type = ParsedFunction
symbol_values = 'total_solute Cleft Cright Fleft Fright volume'
expression = '((total_solute-Cleft*volume)/(Cright-Cleft))*Fright+(volume-(total_solute-Cleft*volume)/(Cright-Cleft))*Fleft'
symbol_names = 'total_solute Cleft Cright Fleft Fright volume'
[../]
[./Diff]
type = ParsedFunction
symbol_values = 'total_free_energy total_no_int'
symbol_names = 'total_free_energy total_no_int'
expression = total_free_energy-total_no_int
[../]
[]
[Materials]
[./consts]
type = GenericConstantMaterial
prop_names = 'kappa_c M'
prop_values = '25 150'
[../]
[./Free_energy]
type = DerivativeParsedMaterial
property_name = F
expression = 'c^2*(c-1)^2'
coupled_variables = c
derivative_order = 2
[../]
[]
[Postprocessors]
# The total free energy of the simulation cell to observe the energy reduction.
[./total_free_energy]
type = ElementIntegralVariablePostprocessor
variable = local_energy
[../]
# for testing we also monitor the total solute amount, which should be conserved,
# gives Cavg in % for this problem.
[./total_solute]
type = ElementIntegralVariablePostprocessor
variable = c
[../]
# Get simulation cell size (1D volume) from postprocessor
[./volume]
type = ElementIntegralMaterialProperty
mat_prop = 1
[../]
# Find concentration in each phase using SideAverageValue
[./Cleft]
type = SideAverageValue
boundary = left
variable = c
[../]
[./Cright]
type = SideAverageValue
boundary = right
variable = c
[../]
# Find local energy in each phase by checking boundaries
[./Fleft]
type = SideAverageValue
boundary = left
variable = local_energy
[../]
[./Fright]
type = SideAverageValue
boundary = right
variable = local_energy
[../]
# Use concentrations and energies to find total free energy without any interface,
# only applies once equilibrium is reached!!
# Difference between energy with and without interface
# gives interface energy per unit area.
[./total_no_int]
type = FunctionValuePostprocessor
function = Int_energy
[../]
[./Energy_of_Interface]
type = FunctionValuePostprocessor
function = Diff
[../]
[]
[Preconditioning]
# This preconditioner makes sure the Jacobian Matrix is fully populated. Our
# kernels compute all Jacobian matrix entries.
# This allows us to use the Newton solver below.
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
# Automatic differentiation provides a _full_ Jacobian in this example
# so we can safely use NEWTON for a fast solve
solve_type = 'NEWTON'
l_max_its = 15
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-4
start_time = 0.0
# make sure that the result obtained for the interfacial free energy is fully converged
end_time = 40
[./TimeStepper]
type = SolutionTimeAdaptiveDT
dt = 0.5
[../]
[]
[Outputs]
gnuplot = true
csv = true
[./exodus]
type = Exodus
show = 'c local_energy'
execute_on = 'failed initial nonlinear timestep_end final'
[../]
[./console]
type = Console
execute_on = 'FAILED INITIAL NONLINEAR TIMESTEP_END final'
[../]
perf_graph = true
[]
(modules/xfem/test/tests/diffusion_xfem/diffusion.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/side_integral/side_integral.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.55 1.0 0.55 0.0'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./top]
type = DirichletBC
variable = u
boundary = 2
value = 3
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 0
value = 2
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Postprocessors]
[./top_surface]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 2
[../]
[./bottom_surface]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 0
[../]
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/1D_xy_lsdep1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: quasi-1D
# Coordinate System: xy
# Material Numbers/Types: level set dep 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# A simple transient heat transfer problem in Cartesian coordinates designed
# with the Method of Manufactured Solutions. This problem was developed to
# verify XFEM performance in the presence of a moving interface for linear
# element models that can be exactly evaluated by FEM/Moose. Both the
# temperature solution and level set function are designed to be linear to
# attempt to minimize error between the Moose/exact solution and XFEM results.
# Thermal conductivity is dependent upon the value of the level set function
# at each timestep.
# Results:
# The temperature at the left boundary (x=0) exhibits the largest difference
# between the FEM/Moose solution and XFEM results. We present the XFEM
# results at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 479.9999722
# 0.6 520 519.9998726
# 0.8 560 559.9997314
# 1.0 600 599.9996885
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 0.5
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = 'rhoCp*(-200*x+200)-(0.05*200*t/1.04)'
symbol_names = 'rhoCp'
symbol_values = 10
[../]
[./neumann_func]
type = ParsedFunction
expression = '((0.05/1.04)*(1-(x-0.04)-0.2*t) + 1.5)*200*t'
[../]
[./k_func]
type = ParsedFunction
expression = '(0.05/1.04)*(1-(x-0.04)-0.2*t) + 1.5'
[../]
[./ls_func]
type = ParsedFunction
expression = '1.04 - x - 0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericFunctionMaterial
prop_names = 'diffusion_coefficient'
prop_values = 'k_func'
[../]
[]
[BCs]
[./left_u]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 'right'
value = 400
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_2/cyl2_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl2_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = cyl2_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = cyl2_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/sliding_block/in_and_out/frictionless_penalty.i)
# This is a benchmark test that checks constraint based frictionless
# contact using the penalty method. In this test a sinusoidal
# displacement is applied in the horizontal direction to simulate
# a small block come in and out of contact as it slides down a larger block.
#
# The sinusoid is of the form 0.4sin(4t)+0.2. The gold file is run
# on one processor and the benchmark
# case is run on a minimum of 4 processors to ensure no parallel variability
# in the contact pressure and penetration results. Further documentation can
# found in moose/modules/contact/doc/sliding_block/
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[./horizontal_movement]
type = ParsedFunction
expression = -0.04*sin(4*t)+0.02
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
time_step_interval = 10
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = frictionless
penalty = 1e+7
formulation = penalty
normal_smoothing_distance = 0.1
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/2D_rz_homog1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: 2D
# Coordinate System: rz
# Material Numbers/Types: homogeneous 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# Transient 2D heat transfer problem in cylindrical coordinates designed with
# the Method of Manufactured Solutions. This problem was developed to verify
# XFEM performance on linear elements in the presence of a moving interface
# sweeping across the x-y coordinates of a system with homogeneous material
# properties. This problem can be exactly evaluated by FEM/Moose without the
# moving interface. Both the temperature and level set function are designed
# to be linear to attempt to minimize error between the Moose/exact solution
# and XFEM results.
# Results:
# The temperature at the bottom left boundary (x=1, y=1) exhibits the largest
# difference between the FEM/Moose solution and XFEM results. We present the
# XFEM results at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 479.9998745
# 0.6 520 519.9995067
# 0.8 560 559.9989409
# 1.0 600 599.9987054
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmin = 1.0
xmax = 2.0
ymin = 1.0
ymax = 2.0
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraints]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-100*x-100*y+400) + 100*1.5*t/x'
[../]
[./neumann_func]
type = ParsedFunction
expression = '1.5*100*t'
[../]
[./dirichlet_right_func]
type = ParsedFunction
expression = '(-100*y+200)*t+400'
[../]
[./dirichlet_top_func]
type = ParsedFunction
expression = '(-100*x+200)*t+400'
[../]
[./ls_func]
type = ParsedFunction
expression = '-0.5*(x+y) + 2.04 - 0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericConstantMaterial
prop_names = 'diffusion_coefficient'
prop_values = 1.5
[../]
[]
[BCs]
[./left_du]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = FunctionDirichletBC
variable = u
boundary = 'right'
function = dirichlet_right_func
[../]
[./bottom_du]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = neumann_func
[../]
[./top_u]
type = FunctionDirichletBC
variable = u
boundary = 'top'
function = dirichlet_top_func
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/diffusion_xfem/diffusion_flux_bc.i)
# The Neumann BC is applied on the cutted boundary.
# The solution is not correct because so far integration along the cutted element faces is not right.
# To correct this, we need to re-calcuate the weights based on area/volume fraction. This will be implemented soon.
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 6
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./top_u]
type = NeumannBC
variable = u
boundary = 2
value = -1.0
[../]
[./bottom]
type = DirichletBC
variable = u
boundary = 0
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/materials/piecewise_by_block_material/discontinuous.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 10
xmax = 2
[]
[subdomain1]
input = gen
type = SubdomainBoundingBoxGenerator
bottom_left = '1.0 0 0'
block_id = 1
top_right = '2.0 1.0 0'
[]
[middle]
input = subdomain1
type = SideSetsBetweenSubdomainsGenerator
new_boundary = middle
paired_block = 1
primary_block = 0
[]
[]
[Variables]
[dummy]
type = MooseVariableFVReal
[]
[]
# This is added to have sufficient ghosting layers, see #19534
[FVKernels]
[diff]
type = FVDiffusion
variable = 'dummy'
coeff = 1
[]
[]
[AuxVariables]
[u]
type = MooseVariableFVReal
[]
[v]
type = MooseVariableFVReal
[FVInitialCondition]
type = FVFunctionIC
function = '4 * (x - 7) * (x - 8)'
[]
[]
[]
[AuxKernels]
# to trigger off-boundary element computations
[to_var]
type = ADMaterialRealAux
variable = 'u'
property = coeff
[]
[]
[Materials]
[coeff_mat]
type = ADPiecewiseConstantByBlockMaterial
prop_name = 'coeff'
subdomain_to_prop_value = '0 4
1 2'
[]
[]
[Postprocessors]
# to trigger on boundary element computations
[flux]
type = ADNonFunctorSideDiffusiveFluxIntegral
boundary = left
variable = v
diffusivity = 'coeff'
[]
# to trigger ghost evaluations
[flux_mid]
type = ADInterfaceDiffusiveFluxIntegral
boundary = middle
variable = v
diffusivity = 'coeff'
coeff_interp_method = average
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
# To get level of ghosting
[console]
type = Console
system_info = 'framework mesh aux nonlinear execution relationship'
[]
[]
(modules/xfem/test/tests/solid_mechanics_basic/crack_propagation_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
use_crack_growth_increment = true
crack_growth_increment = 0.2
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.7 0.5'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./xfem_marker_uo]
type = XFEMRankTwoTensorMarkerUserObject
execute_on = timestep_end
tensor = stress
scalar_type = MaxPrincipal
threshold = 5e+1
average = true
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50 100'
y='0 0.02 0.1'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
block = 0
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
num_steps = 5000
max_xfem_update = 1
[]
[Outputs]
file_base = crack_propagation_2d_out
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/optimization/test/tests/executioners/transient_and_adjoint/multi_variable.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[]
[Problem]
nl_sys_names = 'nl0 adjoint'
[]
[Variables]
[u]
[]
[v]
[]
[u_adjoint]
solver_sys = adjoint
[]
[v_adjoint]
solver_sys = adjoint
[]
[]
[Kernels]
[time_u]
type = TimeDerivative
variable = u
[]
[time_v]
type = TimeDerivative
variable = v
[]
[diff_u]
type = Diffusion
variable = u
[]
[diff_v]
type = Diffusion
variable = v
[]
[uv]
type = CoupledForce
variable = u
v = v
coef = 10
[]
[vu]
type = CoupledForce
variable = v
v = u
coef = 1
[]
[src_u]
type = BodyForce
variable = u
value = 1
[]
[src_u_adjoint]
type = BodyForce
variable = u_adjoint
value = 0
[]
[src_v_adjoint]
type = BodyForce
variable = v_adjoint
value = 1
[]
[]
[BCs]
[dirichlet_u]
type = DirichletBC
variable = u
boundary = 'top right'
value = 0
[]
[dirichlet_v]
type = DirichletBC
variable = v
boundary = 'top right'
value = 0
[]
[]
[Executioner]
type = TransientAndAdjoint
forward_system = nl0
adjoint_system = adjoint
dt = 0.2
num_steps = 5
nl_rel_tol = 1e-12
l_tol = 1e-12
[]
[Postprocessors]
[u_avg]
type = ElementAverageValue
variable = u
execute_on = 'TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[u_adjoint_avg]
type = ElementAverageValue
variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[v_avg]
type = ElementAverageValue
variable = v
execute_on = 'TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[v_adjoint_avg]
type = ElementAverageValue
variable = v_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[u_inner_product]
type = VariableInnerProduct
variable = u
second_variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[v_inner_product]
type = VariableInnerProduct
variable = v
second_variable = v_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[]
[Outputs]
[forward]
type = CSV
[]
[adjoint]
type = CSV
execute_on = 'INITIAL ADJOINT_TIMESTEP_END'
[]
[console]
type = Console
execute_postprocessors_on = 'INITIAL TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[]
(modules/contact/test/tests/frictional/single_point_2d/single_point_2d.i)
[Mesh]
file = single_point_2d.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./horizontal_movement]
type = ParsedFunction
expression = t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
diag_save_in = 'diag_saved_x diag_saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./botx2]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./boty2]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.005
[../]
[]
[Materials]
[./bottom]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e9
poissons_ratio = 0.3
[../]
[./top]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
petsc_options = '-mat_superlu_dist_iterrefine -mat_superlu_dist_replacetinypivot'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.01
num_steps = 1000
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = '0.25'
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/stationary_fluxjump.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 1
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/nucleation_uo/nucleate_edge_crack_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh2'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 20
ny = 10
xmin = 0
xmax = 2
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[top_left]
type = BoundingBoxNodeSetGenerator
new_boundary = pull_top_left
bottom_left = '-0.01 0.99 0'
top_right = '0.11 1.01 0'
input = gen
[]
[top_right]
type = BoundingBoxNodeSetGenerator
new_boundary = pull_top_right
bottom_left = '1.89 0.99 0'
top_right = '2.01 1.01 0'
input = top_left
[]
[top_middle_ss]
type = SideSetsFromBoundingBoxGenerator
input = top_right
bottom_left = '0.79 0.89 0'
top_right = '1.21 1.01 0'
block_id = '0'
boundary_new = top_middle_ss
boundaries_old = top
[]
[nucleate]
type = ParsedSubdomainMeshGenerator
input = top_middle_ss
combinatorial_geometry = 'y > 0.39 & y < 0.51'
block_id = 10
[]
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI InteractionIntegralKII'
displacements = 'disp_x disp_y'
crack_front_points_provider = cut_mesh2
2d=true
number_points_from_provider = 0
crack_direction_method = CurvedCrackFront
radius_inner = '0.15'
radius_outer = '0.45'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
incremental = true
used_by_xfem_to_grow_crack = true
[]
[UserObjects]
[nucleate]
type = MeshCut2DRankTwoTensorNucleation
tensor = stress
scalar_type = MaxPrincipal
nucleation_threshold = nucleation_threshold
initiate_on_boundary = 'left right'
nucleation_length = .2
[]
[cut_mesh2]
type = MeshCut2DFractureUserObject
mesh_file = make_edge_crack_in.e
k_critical=230
growth_increment = 0.11
nucleate_uo = nucleate
[]
[]
[AuxVariables]
[nucleation_threshold]
order = CONSTANT
family = MONOMIAL
[]
[]
[ICs]
[nucleation_bulk]
type = ConstantIC
value = 10000
variable = nucleation_threshold
block = 0
[]
[nucleation_weak]
type = FunctionIC
function = nucleation_x
variable = nucleation_threshold
block = 10
[]
[]
[Functions]
[nucleation_x]
type = ParsedFunction
expression = '300+x*50'
[]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
generate_output = 'stress_xx stress_yy vonmises_stress max_principal_stress'
[../]
[]
[Functions]
[bc_pull_top]
type = ParsedFunction
expression = 0.0005*t
[]
[]
[BCs]
[top_edges]
type = FunctionDirichletBC
boundary = 'pull_top_left pull_top_right'
variable = disp_y
function = bc_pull_top
[]
[top_middle]
type = NeumannBC
boundary = top_middle_ss
variable = disp_y
value = -2000
[]
[bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[]
[bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 5
max_xfem_update = 100
[]
[Outputs]
csv=true
execute_on = TIMESTEP_END
# [xfemcutter]
# type=XFEMCutMeshOutput
# xfem_cutter_uo=cut_mesh2
# []
# console = false
[./console]
type = Console
output_linear = false
output_nonlinear = false
[../]
[]
(modules/navier_stokes/test/tests/postprocessors/flow_rates/conservation_INSFE.i)
[Mesh]
second_order = true
inactive = 'mesh internal_boundary_bot internal_boundary_top'
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '1'
dy = '1 1 1'
ix = '5'
iy = '5 5 5'
subdomain_id = '1
2
3'
[]
[internal_boundary_bot]
type = SideSetsBetweenSubdomainsGenerator
input = mesh
new_boundary = 'internal_bot'
primary_block = 1
paired_block = 2
[]
[internal_boundary_top]
type = SideSetsBetweenSubdomainsGenerator
input = internal_boundary_bot
new_boundary = 'internal_top'
primary_block = 2
paired_block = 3
[]
[diverging_mesh]
type = FileMeshGenerator
file = 'expansion_quad.e'
[]
[]
[Modules]
[IncompressibleNavierStokes]
equation_type = steady-state
# no slip BCs
velocity_boundary = 'bottom right left'
velocity_function = '0 1 0 0 0 0'
pressure_boundary = 'top'
pressure_function = '1'
density_name = rho
dynamic_viscosity_name = mu
integrate_p_by_parts = false
order = SECOND
[]
[]
[Materials]
[const]
type = GenericConstantMaterial
block = '1 2 3'
prop_names = 'rho mu'
prop_values = '1 1'
[]
[]
[FunctorMaterials]
[ADconst]
type = ADGenericFunctorMaterial
block = '1 2 3'
prop_names = 'rho_ad'
prop_values = '1'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
petsc_options_value = '300 bjacobi ilu 4'
line_search = none
nl_rel_tol = 1e-12
nl_max_its = 6
l_tol = 1e-6
l_max_its = 300
[]
[Postprocessors]
[inlet_mass_constant]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_variable = 1
[]
[inlet_mass_matprop]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_mat_prop = 'rho_ad'
[]
[mid1_mass]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
[]
[other_mid1_mass]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
advected_mat_prop = 'rho_ad'
[]
[mid2_mass]
type = VolumetricFlowRate
boundary = internal_top
vel_x = vel_x
vel_y = vel_y
[]
[outlet_mass]
type = VolumetricFlowRate
boundary = top
vel_x = vel_x
vel_y = vel_y
[]
[inlet_momentum_x]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[mid1_momentum_x]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[mid2_momentum_x]
type = VolumetricFlowRate
boundary = internal_top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[outlet_momentum_x]
type = VolumetricFlowRate
boundary = top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_x
[]
[inlet_momentum_y]
type = VolumetricFlowRate
boundary = bottom
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[mid1_momentum_y]
type = VolumetricFlowRate
boundary = internal_bot
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[mid2_momentum_y]
type = VolumetricFlowRate
boundary = internal_top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[outlet_momentum_y]
type = VolumetricFlowRate
boundary = top
vel_x = vel_x
vel_y = vel_y
advected_variable = vel_y
[]
[]
[Outputs]
exodus = false
csv = true
inactive = 'console_mass console_momentum_x console_momentum_y'
[console_mass]
type = Console
start_step = 1
show = 'inlet_mass_variable inlet_mass_constant inlet_mass_matprop mid1_mass mid2_mass outlet_mass'
[]
[console_momentum_x]
type = Console
start_step = 1
show = 'inlet_momentum_x mid1_momentum_x mid2_momentum_x outlet_momentum_x'
[]
[console_momentum_y]
type = Console
start_step = 1
show = 'inlet_momentum_y mid1_momentum_y mid2_momentum_y outlet_momentum_y'
[]
[]
(modules/phase_field/test/tests/GBType/GB_Type_Phase1.i)
# MOOSE input file
# Written by Pierre-Clement Simon - Idaho National Laboratory
#
# Project:
# TRISO fuel fission gas transport: Silver diffusion in silicon carbide
#
# Published with:
# ---
#
# Phase Field Model: Isotropic diffusion equation
# type: Transient
# Grain structure: Single grain
# BCs: Fixed value on the right, flux on the left
#
#
# Info:
# - Input file used to generate polycrystals for SiC
#
# Updates from previous file:
# -
#
# Units
# length: --
# time: --
# energy: --
# quantity: --
# This simulation predicts GB migration of a 2D copper polycrystal with 15 grains
# Mesh adaptivity (new system) and time step adaptivity are used
# An AuxVariable is used to calculate the grain boundary locations
# Postprocessors are used to record time step and the number of grains
# We are not using the GrainTracker in this example so the number
# of order paramaters must match the number of grains.
[Mesh]
[ebsd_mesh]
type = EBSDMeshGenerator
# Two Parallel Grains
filename = 'EBSD_ThreeGrains.txt'
[]
[]
[GlobalParams]
# Parameters used by several kernels that are defined globally to simplify input file
op_num = 6 # Number of grains
var_name_base = gr # Base name of grains
[]
[UserObjects]
[ebsd_reader]
type = EBSDReader
[]
[ebsd]
type = PolycrystalEBSD
coloring_algorithm = bt
ebsd_reader = ebsd_reader
enable_var_coloring = true
# output_adjacency_matrix = true
[]
[grain_tracker]
type = GrainTracker
threshold = 0.001
connecting_threshold = 0.008
compute_var_to_feature_map = true
compute_halo_maps = true # For displaying HALO fields
remap_grains = true
polycrystal_ic_uo = ebsd
[]
[]
[ICs]
[PolycrystalICs]
[PolycrystalColoringIC]
polycrystal_ic_uo = ebsd
[]
[]
[]
[Variables]
# Variable block, where all variables in the simulation are declared
[./PolycrystalVariables]
# Custom action that created all of the grain variables and sets their initial condition
[../]
[]
[AuxVariables]
# Dependent variables
[./bnds]
# Variable used to visualize the grain boundaries in the simulation
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./aphi1]
order = CONSTANT
family = MONOMIAL
[../]
[./bPhi]
order = CONSTANT
family = MONOMIAL
[../]
[./cphi2]
order = CONSTANT
family = MONOMIAL
[../]
[./ebsd_numbers]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
# Kernel block, where the kernels defining the residual equations are set up.
[./PolycrystalKernel]
# Custom action creating all necessary kernels for grain growth. All input parameters are up in GlobalParams
[../]
[]
[AuxKernels]
# AuxKernel block, defining the equations used to calculate the auxvars
[./bnds_aux]
# AuxKernel that calculates the GB term
type = BndsCalcAux
variable = bnds
execute_on = 'initial timestep_end'
[../]
# generate the unique ID from grain_tracker
[./unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
field_display = UNIQUE_REGION
[../]
# The phi will output the Euler angle from EBSD data, and the data structure
# will change with the guide from grain_tracker
[./aphi1]
type = OutputEulerAngles
variable = aphi1
euler_angle_provider = ebsd_reader
grain_tracker = grain_tracker
output_euler_angle = 'phi1'
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./bPhi]
type = OutputEulerAngles
variable = bPhi
euler_angle_provider = ebsd_reader
grain_tracker = grain_tracker
output_euler_angle = 'Phi'
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./cphi2]
type = OutputEulerAngles
variable = cphi2
euler_angle_provider = ebsd_reader
grain_tracker = grain_tracker
output_euler_angle = 'phi2'
execute_on = 'INITIAL TIMESTEP_END'
[../]
# Import the unique grain ID from ebsd data, and the data structure
# will change with the guide from grain_tracker
[ebsd_numbers]
type = EBSDReaderAvgDataAux
data_name = feature_id
ebsd_reader = ebsd_reader
grain_tracker = grain_tracker
variable = ebsd_numbers
execute_on = 'initial timestep_end'
[../]
[]
[BCs]
# Boundary Condition block
[./Periodic]
[./top_bottom]
auto_direction = 'x y' # Makes problem periodic in the x and y directions
[../]
[../]
[]
[Materials]
[./CuGrGr]
# Material properties
type = GBEvolution # Quantitative material properties for copper grain growth. Dimensions are nm and ns
GBmob0 = 2.5e-6 # Mobility prefactor for Cu from schonfelder1997molecular bibtex entry
GBenergy = 0.708 # GB energy for Cu from schonfelder1997molecular bibtex entry
Q = 0.23 # Activation energy for grain growth from Schonfelder 1997
T = 450 # Constant temperature of the simulation (for mobility calculation)
wGB = 6 # Width of the diffuse GB
[../]
[./GB_type]
# The new developed Miso Bnds Aux Kernel
type = ComputeGBMisorientationType
ebsd_reader = ebsd_reader
grain_tracker = grain_tracker
output_properties = 'gb_type'
outputs = exodus
[../]
[]
[Postprocessors]
# Scalar postprocessors
[./dt]
# Outputs the current time step
type = TimestepSize
[../]
[n_elements]
type = NumElems
execute_on = 'initial timestep_end'
[]
[n_nodes]
type = NumNodes
execute_on = 'initial timestep_end'
[]
[DOFs]
type = NumDOFs
[]
[]
[Adaptivity]
initial_steps = 1
max_h_level = 1
marker = combined
[./Indicators]
[./error]
type = GradientJumpIndicator
variable = bnds
[../]
[../]
[./Markers]
[./bound_adapt]
type = ValueThresholdMarker
third_state = DO_NOTHING
coarsen = 0.999 #1.0
refine = 0.95 #0.95
variable = bnds
invert = true
[../]
[./errorfrac]
type = ErrorFractionMarker
coarsen = 0.1
indicator = error
refine = 0.7
[../]
[./combined]
type = ComboMarker
markers = 'bound_adapt errorfrac'
[../]
[../]
[]
[Executioner]
type = Transient # Type of executioner, here it is transient with an adaptive time step
scheme = bdf2 # Type of time integration (2nd order backward euler), defaults to 1st order backward euler
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = ' hypre boomeramg 0.7'
l_max_its = 30 # Max number of linear iterations
l_tol = 1e-4 # Relative tolerance for linear solves
nl_max_its = 40 # Max number of nonlinear iterations
nl_abs_tol = 1e-11 # Relative tolerance for nonlienar solves
nl_rel_tol = 1e-10 # Absolute tolerance for nonlienar solves
[TimeStepper]
type = IterationAdaptiveDT
cutback_factor = 0.9
dt = 1
growth_factor = 1.1
optimal_iterations = 7
[]
start_time = 0.0
num_steps = 2
[]
[Outputs]
perf_graph = true
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/contact/test/tests/pdass_problems/ironing_penalty_action.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = iron.e
[]
patch_update_strategy = auto
patch_size = 20
allow_renumbering = false
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[penalty_normal_pressure]
order = FIRST
family = LAGRANGE
[]
[penalty_frictional_pressure]
order = FIRST
family = LAGRANGE
[]
[accumulated_slip_one]
order = FIRST
family = LAGRANGE
[]
[tangential_vel_one]
order = FIRST
family = LAGRANGE
[]
[real_weighted_gap]
order = FIRST
family = LAGRANGE
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[von_mises]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 2. 8.'
y = '0. -1.0 -1.0'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 8.'
y = '0. 8.'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
block = '1 2'
strain = FINITE
[]
[]
[AuxKernels]
[penalty_normal_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_normal_pressure
user_object = penalty_friction_object_contact_block
contact_quantity = normal_pressure
[]
[penalty_frictional_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_frictional_pressure
user_object = penalty_friction_object_contact_block
contact_quantity = tangential_pressure_one
[]
[penalty_accumulated_slip_auxk]
type = PenaltyMortarUserObjectAux
variable = accumulated_slip_one
user_object = penalty_friction_object_contact_block
contact_quantity = accumulated_slip_one
[]
[penalty_tangential_vel_auxk]
type = PenaltyMortarUserObjectAux
variable = tangential_vel_one
user_object = penalty_friction_object_contact_block
contact_quantity = tangential_velocity_one
[]
[real_weighted_gap_auxk]
type = PenaltyMortarUserObjectAux
variable = real_weighted_gap
user_object = penalty_friction_object_contact_block
contact_quantity = normal_gap
[]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[von_mises_kernel]
#Calculates the von mises stress and assigns it to von_mises
type = RankTwoScalarAux
variable = von_mises
rank_two_tensor = stress
execute_on = timestep_end
scalar_type = VonMisesStress
block = '1 2'
[]
[]
[Contact]
[contact_block]
primary = 20
secondary = 10
friction_coefficient = 0.1
model = coulomb
formulation = mortar_penalty
penalty = 1e5
penalty_friction = 1e4
use_dual = false
[]
[]
[VectorPostprocessors]
[penalty_normal_pressure]
type = NodalValueSampler
variable = penalty_normal_pressure
boundary = 10
sort_by = id
[]
[]
[Postprocessors]
[top_react_x]
type = NodalSum
variable = saved_x
boundary = 30
[]
[top_react_y]
type = NodalSum
variable = saved_y
boundary = 30
[]
[]
[BCs]
[bot_x_disp]
type = DirichletBC
variable = disp_x
boundary = '40'
value = 0.0
preset = false
[]
[bot_y_disp]
type = DirichletBC
variable = disp_y
boundary = '40'
value = 0.0
preset = false
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = '30'
function = disp_ramp_vert
preset = false
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = '30'
function = disp_ramp_horz
preset = false
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 6896
poissons_ratio = 0.32
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '2'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 689.6
poissons_ratio = 0.32
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
l_tol = 1e-6
l_max_its = 50
nl_max_its = 30
start_time = 0.0
end_time = 6.5 # 6.5
dt = 0.0125
dtmin = 1e-5
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = true
hide = 'nodal_area penetration contact_pressure'
[chkfile]
type = CSV
start_time = 0.0
execute_vector_postprocessors_on = FINAL
[]
[console]
type = Console
max_rows = 5
[]
[]
[Debug]
show_var_residual_norms = true
[]
(modules/contact/test/tests/mortar_cartesian_lms/cylinder_friction_cartesian_vcp.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '3'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '2'
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
converge_on = 'disp_x disp_y'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[lm_x]
block = 'secondary_lower'
use_dual = true
scaling = 1.0e-5
[]
[lm_y]
block = 'secondary_lower'
use_dual = true
scaling = 1.0e-5
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Modules/TensorMechanics/Master]
[all]
incremental = false
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
strain = SMALL
add_variables = false
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[]
[_dt]
type = TimestepSize
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff1_stress]
type = ComputeLinearElasticStress
block = '1'
[]
[stuff2_stress]
type = ComputeLinearElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'NONZERO 1e-12'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 5
nl_rel_tol = 1e-09
start_time = -0.1
end_time = 0.3 # 3.5
l_tol = 1e-8
dt = 0.1
dtmin = 0.001
[]
[Preconditioning]
[vcp]
type = VCP
full = true
lm_variable = 'lm_x lm_y'
primary_variable = 'disp_x disp_y'
preconditioner = 'LU'
is_lm_coupling_diagonal = false
adaptive_condensation = true
[]
[]
[VectorPostprocessors]
[x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[]
[y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[]
[lm_x]
type = NodalValueSampler
variable = lm_x
boundary = '3'
sort_by = id
[]
[lm_y]
type = NodalValueSampler
variable = lm_y
boundary = '3'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = false
[console]
type = Console
max_rows = 5
[]
[chkfile]
type = CSV
show = 'x_disp y_disp lm_x lm_y'
file_base = cylinder_friction_check
create_final_symlink = true
execute_on = 'FINAL'
[]
[]
[Constraints]
[weighted_gap_lm]
type = ComputeFrictionalForceCartesianLMMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
lm_x = lm_x
lm_y = lm_y
variable = lm_x
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
correct_edge_dropping = false
mu = 0.4
c_t = 1.0e6
c = 1.0e6
[]
[x]
type = CartesianMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = lm_x
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
correct_edge_dropping = false
[]
[y]
type = CartesianMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = lm_y
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
correct_edge_dropping = false
[]
[]
(modules/xfem/test/tests/diffusion_xfem/levelsetcut2d.i)
# 2D: Mesh is cut by level set based cutter
# The level set is a MOOSE variable
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[./ls]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./diff_ls]
type = Diffusion
variable = ls
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./left_ls]
type = DirichletBC
variable = ls
boundary = 3
value = 3
[../]
[./right_ls]
type = DirichletBC
variable = ls
boundary = 1
value = -3
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_3/cyl3_template1.i)
#
# This input file is a template for both the frictionless and glued test
# variations for the current problem geometry. In order to create an input
# file to run outside the runtest framework, look at the tests file and add the
# appropriate input file lines from the cli_args line.
#
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl3_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_1/plane1_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane1_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = plane1_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = plane1_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_4/plane4_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane4_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = plane4_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = plane4_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(test/tests/userobjects/pre_aux_based_on_exec_flag/pre_post_aux_test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
nx = 2
ymin = 0
ymax = 1
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
initial_condition = 1
[../]
[]
[AuxVariables]
[w1]
order = FIRST
family = LAGRANGE
initial_condition = 2
[]
[w2]
order = FIRST
family = LAGRANGE
[]
[w3]
order = FIRST
family = LAGRANGE
[]
[w4]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[./time]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
# The purpose of this auxkernel is to provide the variable w1
# and the scalepostprocessors included below will either get
# an updated w1 or the previous w1 value depending on whether
# they are forced in preaux or postaux
[NormalizationAuxW1]
type = NormalizationAux
variable = w1
source_variable = u
shift = -100.0
normalization = 1.0
execute_on = 'INITIAL FINAL'
[]
# This establishes a dependency for scale_initial on exec INITIAL
[NormalizationAuxINITIAL]
type = NormalizationAux
variable = w2
source_variable = u
normalization = scale_initial
execute_on = 'INITIAL'
[]
# This establishes a dependency for scale_initial on exec TIMESTEP_END
[NormalizationAuxTIMESTEP_END]
type = NormalizationAux
variable = w3
source_variable = u
normalization = scale_td_end
execute_on = 'TIMESTEP_END'
[]
# This establishes a dependency for scale_initial on exec FINAL
[NormalizationAuxFINAL]
type = NormalizationAux
variable = w4
source_variable = u
normalization = scale_final
execute_on = 'FINAL'
[]
[]
[Postprocessors]
#
# scalePostAux always gets run post_aux
#
[./total_u1]
type = ElementIntegralVariablePostprocessor
variable = w1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
[./scalePostAux]
type = ScalePostprocessor
value = total_u1
scaling_factor = 1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
#
# shoule only run pre_aux on initial
#
[./total_u2]
type = ElementIntegralVariablePostprocessor
variable = w1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
[./scale_initial]
type = ScalePostprocessor
value = total_u2
scaling_factor = 1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
#
# shoule be forced into preaux on timestep_end
#
[./total_u3]
type = ElementIntegralVariablePostprocessor
variable = w1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
[./scale_td_end]
type = ScalePostprocessor
value = total_u3
scaling_factor = 1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
#
# shoule be forced into preaux on final
#
[./total_u4]
type = ElementIntegralVariablePostprocessor
variable = w1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
[./scale_final]
type = ScalePostprocessor
value = total_u4
scaling_factor = 1
execute_on = 'INITIAL TIMESTEP_BEGIN TIMESTEP_END FINAL'
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
dt = 1.0
end_time = 2.0
[]
[Outputs]
[console]
type = Console
execute_on = 'INITIAL FINAL'
[]
[out]
type = CSV
execute_on = 'INITIAL FINAL'
[]
[]
(test/tests/outputs/console/additional_execute_on.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 20
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
[./console]
type = Console
additional_execute_on = initial
[../]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/BFS_ERCOFTAC.i)
##########################################################
# ERCOFTAC test case foe BFS
# Case Number: 031
# Author: Dr. Mauricio Tano
# Last Update: Novomber, 2023
# Turbulent model using:
# k-epsilon model
# Equilibrium + Newton wall treatement
# SIMPLE solve
##########################################################
Re = 5100
rho = 1.0
bulk_u = 1.0
H = 1.0
mu = '${fparse rho * bulk_u * H/ Re}'
advected_interp_method = 'upwind'
pressure_tag = "pressure_grad"
### k-epslilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / H}'
### Modeling parameters ###
non_equilibrium_treatment = true
bulk_wall_treatment = false
walls = 'bottom wall-side top'
max_mixing_length = 1e10
linearized_yplus_mu_t = false
wall_treatment = 'eq_incremental' # Options: eq_newton, eq_incremental, eq_linearized, neq
[Mesh]
[gen]
type = CartesianMeshGenerator
dim = 2
dx = '${fparse 10.0*H} ${fparse 20.0*H}'
dy = '${H} ${fparse 5*H}'
ix = '8 16'
iy = '2 8'
subdomain_id = '
2 1
1 1
'
[]
[corner_walls]
type = SideSetsBetweenSubdomainsGenerator
input = gen
primary_block = '1'
paired_block = '2'
new_boundary = 'wall-side'
[]
[delete_bottom]
type = BlockDeletionGenerator
input = corner_walls
block = '2'
[]
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = ${bulk_u}
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
initial_condition = 1e-8
solver_sys = pressure_system
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
non_equilibrium_treatment = ${non_equilibrium_treatment}
max_mixing_length = ${max_mixing_length}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
k = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
non_equilibrium_treatment = ${non_equilibrium_treatment}
max_mixing_length = ${max_mixing_length}
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${bulk_u}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = 0
[]
[inlet_TKE]
type = INSFVInletIntensityTKEBC
boundary = 'left'
variable = TKE
u = vel_x
v = vel_y
intensity = ${intensity}
[]
[inlet_TKED]
type = INSFVMixingLengthTKEDBC
boundary = 'left'
variable = TKED
k = TKE
characteristic_length = '${fparse 2*H}'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
functor = 0
[]
[walls-u]
type = FVDirichletBC
boundary = ${walls}
variable = vel_x
value = 0
[]
[walls-v]
type = FVDirichletBC
boundary = ${walls}
variable = vel_y
value = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = ${walls}
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
k = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
k = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
linearized_yplus = ${linearized_yplus_mu_t}
non_equilibrium_treatment = ${non_equilibrium_treatment}
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
turbulence_equation_relaxation = '0.3 0.3'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
[]
[Outputs]
exodus = true
[console]
type = Console
outlier_variable_norms = false
[]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/02_core.i)
T_in = 300. # K
m_dot_in = 1e-2 # kg/s
press = 10e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 25
core_dia = '${units 2. cm -> m}'
core_pitch = '${units 8.7 cm -> m}'
A_core = '${fparse core_pitch^2 - 0.25 *pi * core_dia^2}'
P_wet_core = '${fparse 4*core_pitch + pi * core_dia}'
Dh_core = '${fparse 4 * A_core / P_wet_core}'
tot_power = 2000 # W
[GlobalParams]
initial_p = ${press}
initial_vel = 0.0001
initial_T = ${T_in}
gravity_vector = '0 0 0'
rdg_slope_reconstruction = minmod
scaling_factor_1phase = '1 1e-2 1e-4'
closures = thm_closures
fp = he
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[]
[Closures]
[thm_closures]
type = Closures1PhaseTHM
[]
[]
[SolidProperties]
[steel]
type = ThermalFunctionSolidProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[inlet]
type = InletMassFlowRateTemperature1Phase
input = 'core_chan:in'
m_dot = ${m_dot_in}
T = ${T_in}
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
roughness = .0001
A = '${A_core}'
D_h = ${Dh_core}
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
solid_properties = 'steel'
solid_properties_T_ref = '300'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = '${fparse pi * core_dia}'
[]
[outlet]
type = Outlet1Phase
input = 'core_chan:out'
p = ${press}
[]
[]
[Postprocessors]
[power_to_coolant]
type = ADHeatRateConvection1Phase
block = core_chan
P_hf = '${fparse pi *core_dia}'
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[core_p_in]
type = SideAverageValue
boundary = core_chan:in
variable = p
[]
[core_p_out]
type = SideAverageValue
boundary = core_chan:out
variable = p
[]
[core_delta_p]
type = ParsedPostprocessor
pp_names = 'core_p_in core_p_out'
expression = 'core_p_in - core_p_out'
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = IterationAdaptiveDT
dt = 10
[]
end_time = 5000
line_search = basic
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 25
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/xfem/test/tests/single_var_constraint_2d/propagating_2field_2constraint.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[Constraints]
[./xfem_constraint_u]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[./xfem_constraint_v]
type = XFEMSingleVariableConstraint
variable = v
jump = 0
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/phase_field/examples/grain_growth/grain_growth_2D_voronoi_newadapt.i)
# This simulation predicts GB migration of a 2D copper polycrystal with 15 grains
# Mesh adaptivity (new system) and time step adaptivity are used
# An AuxVariable is used to calculate the grain boundary locations
# Postprocessors are used to record time step and the number of grains
# We are not using the GrainTracker in this example so the number
# of order paramaters must match the number of grains.
[Mesh]
# Mesh block. Meshes can be read in or automatically generated
type = GeneratedMesh
dim = 2 # Problem dimension
nx = 12 # Number of elements in the x-direction
ny = 12 # Number of elements in the y-direction
nz = 0 # Number of elements in the z-direction
xmin = 0 # minimum x-coordinate of the mesh
xmax = 1000 # maximum x-coordinate of the mesh
ymin = 0 # minimum y-coordinate of the mesh
ymax = 1000 # maximum y-coordinate of the mesh
zmin = 0
zmax = 0
elem_type = QUAD4 # Type of elements used in the mesh
uniform_refine = 3 # Initial uniform refinement of the mesh
parallel_type = replicated # Periodic BCs
[]
[GlobalParams]
# Parameters used by several kernels that are defined globally to simplify input file
op_num = 15 # Number of grains
var_name_base = gr # Base name of grains
[]
[UserObjects]
[./voronoi]
type = PolycrystalVoronoi
grain_num = 15
rand_seed = 42
coloring_algorithm = bt # We must use bt to force the UserObject to assign one grain to each op
[../]
[]
[ICs]
[./PolycrystalICs]
[./PolycrystalColoringIC]
polycrystal_ic_uo = voronoi
[../]
[../]
[]
[Variables]
# Variable block, where all variables in the simulation are declared
[./PolycrystalVariables]
# Custom action that created all of the grain variables and sets their initial condition
[../]
[]
[AuxVariables]
# Dependent variables
[./bnds]
# Variable used to visualize the grain boundaries in the simulation
[../]
[]
[Kernels]
# Kernel block, where the kernels defining the residual equations are set up.
[./PolycrystalKernel]
# Custom action creating all necessary kernels for grain growth. All input parameters are up in GlobalParams
[../]
[]
[AuxKernels]
# AuxKernel block, defining the equations used to calculate the auxvars
[./bnds_aux]
# AuxKernel that calculates the GB term
type = BndsCalcAux
variable = bnds
execute_on = timestep_end
[../]
[]
[BCs]
# Boundary Condition block
[./Periodic]
[./top_bottom]
auto_direction = 'x y' # Makes problem periodic in the x and y directions
[../]
[../]
[]
[Materials]
[./CuGrGr]
# Material properties
type = GBEvolution # Quantitative material properties for copper grain growth. Dimensions are nm and ns
GBmob0 = 2.5e-6 # Mobility prefactor for Cu from schonfelder1997molecular bibtex entry
GBenergy = 0.708 # GB energy for Cu from schonfelder1997molecular bibtex entry
Q = 0.23 # Activation energy for grain growth from Schonfelder 1997
T = 450 # Constant temperature of the simulation (for mobility calculation)
wGB = 14 # Width of the diffuse GB
[../]
[]
[Postprocessors]
# Scalar postprocessors
[./dt]
# Outputs the current time step
type = TimestepSize
[../]
[]
[Executioner]
type = Transient # Type of executioner, here it is transient with an adaptive time step
scheme = bdf2 # Type of time integration (2nd order backward euler), defaults to 1st order backward euler
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -mat_mffd_type'
petsc_options_value = 'hypre boomeramg 101 ds'
l_max_its = 30 # Max number of linear iterations
l_tol = 1e-4 # Relative tolerance for linear solves
nl_max_its = 40 # Max number of nonlinear iterations
nl_abs_tol = 1e-11 # Relative tolerance for nonlienar solves
nl_rel_tol = 1e-10 # Absolute tolerance for nonlienar solves
[./TimeStepper]
type = SolutionTimeAdaptiveDT
dt = 25 # Initial time step. In this simulation it changes.
[../]
start_time = 0.0
end_time = 4000
num_steps = 3
[]
[Adaptivity]
marker = errorfrac
max_h_level = 4
[./Indicators]
[./error]
type = GradientJumpIndicator
variable = bnds
[../]
[../]
[./Markers]
[./bound_adapt]
type = ValueThresholdMarker
third_state = DO_NOTHING
coarsen = 1.0
refine = 0.99
variable = bnds
invert = true
[../]
[./errorfrac]
type = ErrorFractionMarker
coarsen = 0.1
indicator = error
refine = 0.7
[../]
[../]
[]
[Outputs]
exodus = true
csv = true
[./console]
type = Console
max_rows = 20
[../]
[]
(test/tests/markers/two_circle_marker/two_circle_marker.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.02
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Transient
num_steps = 6
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
initial_steps = 1
initial_marker = two_circle_marker
cycles_per_step = 1
marker = two_circle_marker
max_h_level = 1
[./Markers]
[./two_circle_marker]
type = TwoCircleMarker
point1 = '0.5 0.5 0'
radius1 = 0.3
point2 = '0.35 0.25 0'
radius2 = 0.3
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(modules/phase_field/tutorials/spinodal_decomposition/s3_decomp.i)
#
# Simulation of iron-chromium alloy decomposition using simplified conditions.
#
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
nx = 25
ny = 25
nz = 0
xmin = 0
xmax = 25
ymin = 0
ymax = 25
zmin = 0
zmax = 0
uniform_refine = 2
[]
[Variables]
[./c] # Mole fraction of Cr (unitless)
order = FIRST
family = LAGRANGE
[../]
[./w] # Chemical potential (eV/mol)
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./concentrationIC] # 46.774 mol% Cr with variations
type = RandomIC
min = 0.44774
max = 0.48774
seed = 210
variable = c
[../]
[]
[BCs]
[./Periodic]
[./c_bcs]
auto_direction = 'x y'
[../]
[../]
[]
[Kernels]
[./w_dot]
variable = w
v = c
type = CoupledTimeDerivative
[../]
[./coupled_res]
variable = w
type = SplitCHWRes
mob_name = M
[../]
[./coupled_parsed]
variable = c
type = SplitCHParsed
f_name = f_loc
kappa_name = kappa_c
w = w
[../]
[]
[Materials]
# d is a scaling factor that makes it easier for the solution to converge
# without changing the results. It is defined in each of the materials and
# must have the same value in each one.
[./constants]
# Define constant values kappa_c and M. Eventually M will be replaced with
# an equation rather than a constant.
type = GenericFunctionMaterial
prop_names = 'kappa_c M'
prop_values = '8.125e-16*6.24150934e+18*1e+09^2*1e-27
2.2841e-26*1e+09^2/6.24150934e+18/1e-27'
# kappa_c*eV_J*nm_m^2*d
# M*nm_m^2/eV_J/d
[../]
[./local_energy]
# Defines the function for the local free energy density as given in the
# problem, then converts units and adds scaling factor.
type = DerivativeParsedMaterial
property_name = f_loc
coupled_variables = c
constant_names = 'A B C D E F G eV_J d'
constant_expressions = '-2.446831e+04 -2.827533e+04 4.167994e+03 7.052907e+03
1.208993e+04 2.568625e+03 -2.354293e+03
6.24150934e+18 1e-27'
expression = 'eV_J*d*(A*c+B*(1-c)+C*c*log(c)+D*(1-c)*log(1-c)+
E*c*(1-c)+F*c*(1-c)*(2*c-1)+G*c*(1-c)*(2*c-1)^2)'
derivative_order = 2
[../]
[]
[Postprocessors]
[./step_size] # Size of the time step
type = TimestepSize
[../]
[./iterations] # Number of iterations needed to converge timestep
type = NumNonlinearIterations
[../]
[./nodes] # Number of nodes in mesh
type = NumNodes
[../]
[./evaluations] # Cumulative residual calculations for simulation
type = NumResidualEvaluations
[../]
[./active_time] # Time computer spent on simulation
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[]
[Preconditioning]
[./coupled]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 30
l_tol = 1e-6
nl_max_its = 50
nl_abs_tol = 1e-9
end_time = 604800 # 7 days
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type
-sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly
ilu 1'
[./TimeStepper]
type = IterationAdaptiveDT
dt = 10
cutback_factor = 0.8
growth_factor = 1.5
optimal_iterations = 7
[../]
[./Adaptivity]
coarsen_fraction = 0.1
refine_fraction = 0.7
max_h_level = 2
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
exodus = true
console = true
csv = true
[./console]
type = Console
max_rows = 10
[../]
[]
(test/tests/time_integrators/actually_explicit_euler_verification/ee-2d-linear.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = (x+y)
[../]
[./exact_fn]
type = ParsedFunction
expression = t*(x+y)
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
start_time = 0.0
num_steps = 20
dt = 0.00005
l_tol = 1e-12
[./TimeIntegrator]
type = ActuallyExplicitEuler
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/thermal_hydraulics/test/tests/controls/pid_control/test.i)
# This test "measures" the liquid temperature at location (10, 0, 0) on a 15 meters
# long pipe and adjusts the inlet stagnation temperature using a PID controller with
# set point at 340 K. The pipe is filled with water at T = 350 K. The purpose is to
# make sure that the channel fills with colder liquid and levels at the set point
# value. In steady state there should be a flat temperature profile at ~340 K.
[GlobalParams]
initial_p = 100.e3
initial_vel = 1.0
initial_T = 350.
scaling_factor_1phase = '1 1e-2 1e-4'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 105.e3
T0 = 300.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[ControlLogic]
[T_set_point]
type = GetFunctionValueControl
function = 340
[]
[pid_ctrl]
type = PIDControl
input = T_reading
set_point = T_set_point:value
K_i = 0.05
K_p = 0.2
K_d = 0.1
initial_value = 340
[]
[set_inlet_value]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = pid_ctrl:output
[]
[]
[Postprocessors]
[T_reading]
type = PointValue
point = '10 0 0'
variable = T
execute_on = timestep_begin
[]
[T_inlet]
type = PointValue
point = '0 0 0'
variable = T
execute_on = timestep_begin
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
dt = 5
abort_on_solve_fail = true
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 20
l_tol = 1e-3
l_max_its = 5
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
start_time = 0.0
end_time = 300.0
[]
[Outputs]
[out]
type = CSV
execute_on = 'final'
[]
[console]
type = Console
max_rows = 1
[]
[]
(modules/thermal_hydraulics/test/tests/components/heat_structure_base/phy.sub_discretization.i)
#
# Testing the ability to discretize the HeatStructure by dividing it into
# axial subsections
#
[GlobalParams]
[]
[SolidProperties]
[fuel-mat]
type = ThermalFunctionSolidProperties
k = 3.65
cp = 288.734
rho = 1.0412e2
[]
[gap-mat]
type = ThermalFunctionSolidProperties
k = 1.084498
cp = 1.0
rho = 1.0
[]
[clad-mat]
type = ThermalFunctionSolidProperties
k = 16.48672
cp = 321.384
rho = 6.6e1
[]
[]
[Components]
[hs]
type = HeatStructureCylindrical
position = '0 0 1'
orientation = '1 0 0'
axial_region_names = 'reg1 reg2'
length = '2.0 1.6576'
n_elems = '7 4'
names = 'FUEL GAP CLAD'
widths = '0.0046955 0.0000955 0.000673'
n_part_elems = '10 3 3'
solid_properties = 'fuel-mat gap-mat clad-mat'
solid_properties_T_ref = '300 300 300'
initial_T = 300
[]
[temp_outside]
type = HSBoundarySpecifiedTemperature
hs = hs
boundary = hs:outer
T = 300
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
start_time = 0
dt = 1
num_steps = 1
abort_on_solve_fail = true
solve_type = 'PJFNK'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 30
l_tol = 1e-4
l_max_its = 300
[]
[Outputs]
[out]
type = Exodus
[]
[console]
type = Console
execute_scalars_on = none
[]
[]
(modules/xfem/test/tests/crack_tip_enrichment/penny_crack_3d.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
use_crack_tip_enrichment = true
crack_front_definition = crack_front
enrichment_displacements = 'enrich1_x enrich2_x enrich3_x enrich4_x enrich1_y enrich2_y enrich3_y enrich4_y enrich1_z enrich2_z enrich3_z enrich4_z'
cut_off_boundary = all
cut_off_radius = 0.3
[]
[UserObjects]
[circle_cut_uo]
type = CircleCutUserObject
cut_data = '0 0 0
0.5 0 0
0 0.5 0'
[]
[crack_front]
type = CrackFrontDefinition
crack_direction_method = CurvedCrackFront
crack_front_points = '0.500000000000000 0 0
0.000000000000000 0.500000000000000 0
-0.500000000000000 0.000000000000000 0
-0.000000000000000 -0.500000000000000 0'
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 3
nx = 9
ny = 9
nz = 3
xmin = -1.0
xmax = 1.0
ymin = -1.0
ymax = 1.0
zmin = -0.75
zmax = 0.75
elem_type = HEX8
[]
[all_node]
type = BoundingBoxNodeSetGenerator
input = gen
new_boundary = 'all'
top_right = '1 1 1'
bottom_left = '-1 -1 -1'
[]
[]
[Variables]
[disp_x]
order = FIRST
family = LAGRANGE
[]
[disp_y]
order = FIRST
family = LAGRANGE
[]
[disp_z]
order = FIRST
family = LAGRANGE
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_zz]
order = CONSTANT
family = MONOMIAL
[]
[SED]
order = CONSTANT
family = MONOMIAL
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = false
volumetric_locking_correction = false
[]
[]
[BCs]
[top_z]
type = Pressure
variable = disp_z
boundary = front
factor = -1
[]
[bottom_x]
type = DirichletBC
boundary = back
variable = disp_x
value = 0.0
[]
[bottom_y]
type = DirichletBC
boundary = back
variable = disp_y
value = 0.0
[]
[bottom_z]
type = DirichletBC
boundary = back
variable = disp_z
value = 0.0
[]
[]
[Materials]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[strain]
type = ComputeCrackTipEnrichmentSmallStrain
crack_front_definition = crack_front
enrichment_displacements = 'enrich1_x enrich2_x enrich3_x enrich4_x enrich1_y enrich2_y enrich3_y enrich4_y enrich1_z enrich2_z enrich3_z enrich4_z'
[]
[stress]
type = ComputeLinearElasticStress
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
[Quadrature]
type = GAUSS
order = SECOND
[]
# controls for linear iterations
l_max_its = 10
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
exodus = true
[console]
type = Console
output_linear = true
[]
[]
(modules/xfem/test/tests/solid_mechanics_basic/square_branch_quad_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo0]
type = LineSegmentCutUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10'
time_start_cut = 0.0
time_end_cut = 1.0
[../]
[./line_seg_cut_uo1]
type = LineSegmentCutUserObject
cut_data = '3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01'
time_start_cut = 1.0
time_end_cut = 2.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
planar_formulation = PLANE_STRAIN
add_variables = true
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
file_base = square_branch_quad_2d_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/time_integrators/explicit-euler/ee-2d-quadratic.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = ((x*x)+(y*y))-(4*t)
[../]
[./exact_fn]
type = ParsedFunction
expression = t*((x*x)+(y*y))
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
implicit = true
[../]
[./diff]
type = Diffusion
variable = u
implicit = false
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
implicit = false
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
implicit = true
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
scheme = 'explicit-euler'
solve_type = 'LINEAR'
l_tol = 1e-13
start_time = 0.0
num_steps = 20
dt = 0.00005
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_2/plane2_template2.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane2_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 200
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_sphere.i)
sphere_outer_htc = 10 # W/m^2/K
sphere_outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
[file]
type = FileMeshGenerator
file = cyl2D.e
[]
allow_renumbering = false
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[]
[AuxVariables]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[power_density]
block = 'fuel'
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
[]
[heat_source]
type = CoupledForce
variable = temp
block = 'fuel'
v = power_density
[]
[]
[AuxKernels]
[gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0.0
emissivity_secondary = 0.0
gap_conductivity = 5
# quadrature = true
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = '4' # outer RPV
coefficient = ${sphere_outer_htc}
T_infinity = ${sphere_outer_Tinf}
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '2 3'
variable = temp
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[Quadrature]
order = fifth
side_order = seventh
[]
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 'fuel'
[]
[sphere_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = '4' # outer RVP
T_fluid = ${sphere_outer_Tinf}
htc = ${sphere_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(sphere_convective_out - ptot) / ptot'
pp_names = 'sphere_convective_out ptot'
[]
[]
(modules/xfem/test/tests/diffusion_xfem/levelsetcut2d_aux.i)
# 2D: Mesh is cut by level set based cutter
# The level set is a MOOSE auxvariable
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 3
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '3 5'
[../]
[./ls_func]
type = ParsedFunction
expression = 'x-0.5'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 3
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/thermal_hydraulics/test/tests/components/heat_transfer_from_specified_temperature_1phase/phy.energy_walltemperature_ss_1phase.i)
# This test tests conservation of energy at steady state for 1-phase flow when
# wall temperature is specified. Conservation is checked by comparing the
# integral of the heat flux against the difference of the boundary fluxes.
[GlobalParams]
initial_p = 7.0e6
initial_vel = 0
initial_T = 513
gravity_vector = '0.0 0.0 0.0'
closures = simple_closures
[]
[FluidProperties]
[eos]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 3.66
n_elems = 10
A = 1.907720E-04
D_h = 1.698566E-02
f = 0.0
fp = eos
[]
[ht_pipe]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = pipe
T_wall = 550
Hw = 1.0e3
P_hf = 4.4925e-2
[]
[inlet]
type = SolidWall1Phase
input = 'pipe:in'
[]
[outlet]
type = SolidWall1Phase
input = 'pipe:out'
[]
[]
[Postprocessors]
[hf_pipe]
type = ADHeatRateConvection1Phase
block = pipe
T_wall = T_wall
T = T
Hw = Hw
P_hf = P_hf
execute_on = 'initial timestep_end'
[]
[heat_added]
type = TimeIntegratedPostprocessor
value = hf_pipe
execute_on = 'initial timestep_end'
[]
[E]
type = ElementIntegralVariablePostprocessor
variable = rhoEA
execute_on = 'initial timestep_end'
[]
[E_change]
type = ChangeOverTimePostprocessor
postprocessor = E
change_with_respect_to_initial = true
execute_on = 'initial timestep_end'
[]
[E_conservation]
type = DifferencePostprocessor
value1 = heat_added
value2 = E_change
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = crank-nicolson
abort_on_solve_fail = true
dt = 1e-1
solve_type = 'NEWTON'
line_search = 'basic'
petsc_options_iname = '-pc_type'
petsc_options_value = ' lu'
nl_rel_tol = 1e-9
nl_abs_tol = 1e-8
nl_max_its = 50
l_tol = 1e-3
l_max_its = 60
start_time = 0
num_steps = 10
[]
[Outputs]
[out]
type = CSV
show = 'E_conservation'
[]
[console]
type = Console
show = 'E_conservation'
[]
[]
(modules/contact/test/tests/verification/patch_tests/mindlin/cylinder_friction_node_face.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[react_x]
[]
[react_y]
[]
[penetration]
[]
[inc_slip_x]
[]
[inc_slip_y]
[]
[accum_slip_x]
[]
[accum_slip_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[]
[incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[]
[accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[]
[accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[]
[penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[]
[react_x]
type = TagVectorAux
vector_tag = 'ref'
v = 'disp_x'
variable = 'react_x'
[]
[react_y]
type = TagVectorAux
vector_tag = 'ref'
v = 'disp_y'
variable = 'react_y'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = react_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = react_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = react_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = react_y
boundary = 4
[]
[penetration]
type = NodalExtremeValue
variable = penetration
value_type = max
boundary = 3
[]
[inc_slip_x_max]
type = NodalExtremeValue
variable = inc_slip_x
value_type = max
boundary = 3
[]
[inc_slip_x_min]
type = NodalExtremeValue
variable = inc_slip_x
value_type = min
boundary = 3
[]
[inc_slip_y_max]
type = NodalExtremeValue
variable = inc_slip_y
value_type = max
boundary = 3
[]
[inc_slip_y_min]
type = NodalExtremeValue
variable = inc_slip_y
value_type = min
boundary = 3
[]
[accum_slip_x]
type = NodalExtremeValue
variable = accum_slip_x
value_type = max
boundary = 3
[]
[accum_slip_y]
type = NodalExtremeValue
variable = accum_slip_y
value_type = max
boundary = 3
[]
[_dt]
type = TimestepSize
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '2 3 4 5 6 7'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type '
'-pc_factor_shift_amount -mat_mffd_err'
petsc_options_value = 'lu superlu_dist NONZERO 1e-15 '
' 1e-5'
line_search = 'none'
nl_abs_tol = 1e-8
start_time = 0.0
end_time = 0.3
l_tol = 1e-4
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[]
[y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = true
[console]
type = Console
max_rows = 5
[]
[chkfile]
type = CSV
show = 'x_disp y_disp'
file_base = cylinder_friction_check
create_final_symlink = true
execute_on = 'FINAL'
[]
[]
[Contact]
[leftright]
primary = 2
secondary = 3
model = coulomb
formulation = penalty
penalty = 5e9
normalize_penalty = true
friction_coefficient = '0.2'
[]
[]
(modules/combined/test/tests/inelastic_strain/elas_plas/elas_plas_nl1.i)
#
# Test for effective strain calculation.
# Boundary conditions from NAFEMS test NL1
#
# This is not a verification test. The boundary conditions are applied such
# that the first step generates only elastic stresses. The second and third
# steps generate plastic deformation and the effective strain should be
# increasing throughout the run.
#
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = one_elem2.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[./pressure]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./plastic_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./tot_strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./eff_plastic_strain]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./pressure]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = pressure
scalar_type = Hydrostatic
execute_on = timestep_end
[../]
[./elastic_strain_xx]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain_yy]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain_zz]
type = RankTwoAux
rank_two_tensor = elastic_strain
variable = elastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./plastic_strain_xx]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./plastic_strain_yy]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./plastic_strain_zz]
type = RankTwoAux
rank_two_tensor = plastic_strain
variable = plastic_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./tot_strain_xx]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./tot_strain_yy]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./tot_strain_zz]
type = RankTwoAux
rank_two_tensor = total_strain
variable = tot_strain_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./eff_plastic_strain]
type = MaterialRealAux
property = effective_plastic_strain
variable = eff_plastic_strain
[../]
[]
[Functions]
[./appl_dispy]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0.0 0.208e-4 0.50e-4 1.00e-4'
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./origin_x]
type = DirichletBC
variable = disp_x
boundary = 103
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 102
value = 0.0
[../]
[./origin_y]
type = DirichletBC
variable = disp_y
boundary = 103
value = 0.0
[../]
[./top_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 1
function = appl_dispy
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
block = 1
youngs_modulus = 250e9
poissons_ratio = 0.25
[../]
[./strain]
type = ComputePlaneFiniteStrain
block = 1
[../]
[./stress]
type = ComputeMultipleInelasticStress
inelastic_models = 'isoplas'
block = 1
[../]
[./isoplas]
type = IsotropicPlasticityStressUpdate
yield_stress = 5e6
hardening_constant = 0.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
l_tol = 1e-4
l_max_its = 100
nl_max_its = 20
dt = 1.0
start_time = 0.0
num_steps = 100
end_time = 3.0
[] # Executioner
[Postprocessors]
[./stress_xx]
type = ElementAverageValue
variable = stress_xx
[../]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./stress_xy]
type = ElementAverageValue
variable = stress_xy
[../]
[./vonmises]
type = ElementAverageValue
variable = vonmises
[../]
[./pressure]
type = ElementAverageValue
variable = pressure
[../]
[./el_strain_xx]
type = ElementAverageValue
variable = elastic_strain_xx
[../]
[./el_strain_yy]
type = ElementAverageValue
variable = elastic_strain_yy
[../]
[./el_strain_zz]
type = ElementAverageValue
variable = elastic_strain_zz
[../]
[./pl_strain_xx]
type = ElementAverageValue
variable = plastic_strain_xx
[../]
[./pl_strain_yy]
type = ElementAverageValue
variable = plastic_strain_yy
[../]
[./pl_strain_zz]
type = ElementAverageValue
variable = plastic_strain_zz
[../]
[./eff_plastic_strain]
type = ElementAverageValue
variable = eff_plastic_strain
[../]
[./tot_strain_xx]
type = ElementAverageValue
variable = tot_strain_xx
[../]
[./tot_strain_yy]
type = ElementAverageValue
variable = tot_strain_yy
[../]
[./tot_strain_zz]
type = ElementAverageValue
variable = tot_strain_zz
[../]
[./disp_x1]
type = NodalVariableValue
nodeid = 0
variable = disp_x
[../]
[./disp_x4]
type = NodalVariableValue
nodeid = 3
variable = disp_x
[../]
[./disp_y1]
type = NodalVariableValue
nodeid = 0
variable = disp_y
[../]
[./disp_y4]
type = NodalVariableValue
nodeid = 3
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
output_linear = true
[../]
[] # Outputs
(modules/contact/test/tests/mechanical_constraint/frictionless_kinematic.i)
[Mesh]
file = blocks_2d.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
#Initial gap is 0.01
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e7
poissons_ratio = 0.3
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.10
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = frictionless
penalty = 1e+6
[../]
[]
(modules/combined/examples/xfem/xfem_mechanics_prescribed_growth.i)
# This is a demonstration of a simple mechanics simulation using XFEM
# to represent a single crack that is prescribed to propagate along
# a line over time.
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
geometric_cut_userobjects = 'line_seg_cut_uo'
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '1.0 0.5 0.1 0.5'
time_start_cut = 0.0
time_end_cut = 8.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
[../]
[]
[Functions]
[./pull]
type = PiecewiseLinear
x='0 50'
y='0 0.02'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = DirichletBC
boundary = top
variable = disp_x
value = 0.0
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = pull
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./_elastic_strain]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 10.0
max_xfem_update = 5
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/high_order_elements/diffusion_2d.i)
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 3
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = TRI6
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.35 1.0 0.35 0.2'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./u_left]
type = PiecewiseLinear
x = '0 2'
y = '0 0.1'
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = FunctionDirichletBC
variable = u
boundary = 3
function = u_left
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/2D_xy_lsdep1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: 2D
# Coordinate System: xy
# Material Numbers/Types: level set dep 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# Transient 2D heat transfer problem in Cartesian coordinates designed with
# the Method of Manufactured Solutions. This problem was developed to verify
# XFEM performance on linear elements in the presence of a moving interface
# sweeping across the x-y coordinates of a system with thermal conductivity
# dependent upon the transient level set function. This problem can be
# exactly evaluated by FEM/Moose without the moving interface. Both the
# temperature and level set function are designed to be linear to attempt to
# minimize the error between the Moose/exact solution and XFEM results.
# Results:
# The temperature at the bottom left boundary (x=0, y=0) exhibits the largest
# difference between the FEM/Moose solution and XFEM results. We present the
# XFEM results at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 479.9998738
# 0.6 520 519.9995114
# 0.8 560 559.9989360
# 1.0 600 599.9983833
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraints]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-100*x-100*y+200)-(5*t/1.04)'
[../]
[./neumann_func]
type = ParsedFunction
expression = '((0.01/1.04)*(-2.5*x-2.5*y-t)+1.55)*100*t'
[../]
[./dirichlet_right_func]
type = ParsedFunction
expression = '(-100*y+100)*t+400'
[../]
[./dirichlet_top_func]
type = ParsedFunction
expression = '(-100*x+100)*t+400'
[../]
[./k_func]
type = ParsedFunction
expression = '(0.01/1.04)*(-2.5*x-2.5*y-t)+1.55'
[../]
[./ls_func]
type = ParsedFunction
expression = '-0.5*(x+y) + 1.04 -0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericFunctionMaterial
prop_names = 'diffusion_coefficient'
prop_values = 'k_func'
[../]
[]
[BCs]
[./left_du]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = FunctionDirichletBC
variable = u
boundary = 'right'
function = dirichlet_right_func
[../]
[./bottom_du]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = neumann_func
[../]
[./top_u]
type = FunctionDirichletBC
variable = u
boundary = 'top'
function = dirichlet_top_func
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/sliding_block/in_and_out/frictionless_penalty_contact_line_search.i)
# This is a benchmark test that checks constraint based frictionless
# contact using the penalty method. In this test a sinusoidal
# displacement is applied in the horizontal direction to simulate
# a small block come in and out of contact as it slides down a larger block.
#
# The sinusoid is of the form 0.4sin(4t)+0.2. The gold file is run
# on one processor and the benchmark
# case is run on a minimum of 4 processors to ensure no parallel variability
# in the contact pressure and penetration results. Further documentation can
# found in moose/modules/contact/doc/sliding_block/
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[./horizontal_movement]
type = ParsedFunction
expression = -0.04*sin(4*t)+0.02
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[./tot_nonlin_it]
type = CumulativeValuePostprocessor
postprocessor = nonlinear_its
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-ksp_monitor_true_residual'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'contact'
contact_line_search_ltol = .5
contact_line_search_allowed_lambda_cuts = 0
l_max_its = 100
nl_max_its = 20
dt = 0.1
end_time = 3
# num_steps = 30
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = frictionless
penalty = 1e+7
formulation = penalty
normal_smoothing_distance = 0.1
[../]
[]
(modules/xfem/test/tests/bimaterials/glued_bimaterials_2d.i)
# This test is for two layer materials with different youngs modulus
# The global stress is determined by switching the stress based on level set values
# The material interface is marked by a level set function
# The two layer materials are glued together
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Mesh]
displacements = 'disp_x disp_y'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
[]
[./left_bottom]
type = ExtraNodesetGenerator
new_boundary = 'left_bottom'
coord = '0.0 0.0'
input = gen
[../]
[./left_top]
type = ExtraNodesetGenerator
new_boundary = 'left_top'
coord = '0.0 5.'
input = left_bottom
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'y-2.5'
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./a_strain_xx]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
boundary = top
variable = disp_x
function = 0.03*t
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ComputeSmallStrain
base_name = A
[../]
[./stress_A]
type = ComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e5
poissons_ratio = 0.3
[../]
[./strain_B]
type = ComputeSmallStrain
base_name = B
[../]
[./stress_B]
type = ComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = LevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[./combined_dstressdstrain]
type = LevelSetBiMaterialRankFour
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = Jacobian_mult
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'bt'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-7
# time control
start_time = 0.0
dt = 0.1
num_steps = 2
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/optimization/test/tests/executioners/transient_and_adjoint/self_adjoint.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[]
[Problem]
nl_sys_names = 'nl0 adjoint'
[]
[Variables]
[u]
[]
[u_adjoint]
solver_sys = adjoint
[]
[]
[Kernels]
[time]
type = TimeDerivative
variable = u
[]
[diff]
type = Diffusion
variable = u
[]
[src]
type = BodyForce
variable = u
value = 1
[]
[src_adjoint]
type = BodyForce
variable = u_adjoint
value = 10
[]
[]
[BCs]
[dirichlet]
type = DirichletBC
variable = u
boundary = 'top right'
value = 0
[]
[]
[Executioner]
type = TransientAndAdjoint
forward_system = nl0
adjoint_system = adjoint
dt = 0.2
num_steps = 5
nl_rel_tol = 1e-12
l_tol = 1e-12
[]
[Postprocessors]
[u_avg]
type = ElementAverageValue
variable = u
execute_on = 'TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[u_adjoint_avg]
type = ElementAverageValue
variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[inner_product]
type = VariableInnerProduct
variable = u
second_variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[]
[Outputs]
[forward]
type = CSV
[]
[adjoint]
type = CSV
execute_on = 'INITIAL ADJOINT_TIMESTEP_END'
[]
[console]
type = Console
execute_postprocessors_on = 'INITIAL TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[]
(modules/xfem/test/tests/pressure_bc/edge_2d_pressure.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = False
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 9
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.5 0.5 0.5'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
generate_output = 'stress_xx stress_yy'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1.0 2.0'
y = '0 500 1000'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[DiracKernels]
[./pressure_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
[../]
[./pressure_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1
end_time = 2
[]
[Outputs]
file_base = edge_2d_pressure_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_3/brick3_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick3_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x28]
type = NodalVariableValue
nodeid = 27
variable = disp_x
[../]
[./disp_x33]
type = NodalVariableValue
nodeid = 32
variable = disp_x
[../]
[./disp_y28]
type = NodalVariableValue
nodeid = 27
variable = disp_y
[../]
[./disp_y33]
type = NodalVariableValue
nodeid = 32
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x28 disp_y28 disp_x33 disp_y33 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change_restart2.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
order = FIRST
family = LAGRANGE
block = 1
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
x = '0 1e6 2e6 2.001e6 2.002e6'
y = '0 3e8 3e8 12e8 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
volumetric_locking_correction = true
incremental = true
eigenstrain_names = thermal_expansion
decomposition_method = EigenSolution
add_variables = true
generate_output = 'vonmises_stress'
temperature = temp
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
num_steps = 50000
end_time = 2.002e6
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e7
dt = 1e6
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[]
[Problem]
restart_file_base = adapt_tstep_function_change_restart1_checkpoint_cp/0065
[]
(modules/xfem/test/tests/solid_mechanics_basic/penny_crack_cfp.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 3
ny = 3
nz = 3
xmin = -1.1
xmax = 1.1
ymin = -1.1
ymax = 1.1
zmin = -1.1
zmax = 1.1
elem_type = HEX8
displacements = 'disp_x disp_y disp_z'
[]
[UserObjects]
[./circle_cut_uo]
type = CircleCutUserObject
cut_data = '0 0 0
0 -0.5 0
-0.5 0 0'
[../]
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[DomainIntegral]
integrals = 'KfromJIntegral'
crack_direction_method = CurvedCrackFront
radius_inner = '0.3'
radius_outer = '0.6'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
crack_front_points_provider = circle_cut_uo
number_points_from_provider = 10
closed_loop = true
incremental = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 0
[../]
[]
[Functions]
[./top_trac_z]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_z]
type = FunctionNeumannBC
boundary = front
variable = disp_z
function = top_trac_z
[../]
[./bottom_x]
type = DirichletBC
boundary = back
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = back
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = back
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/combined/test/tests/axisymmetric_2d3d_solution_function/2d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = 2d.e
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[temp]
initial_condition = 400
[]
[]
[AuxVariables]
[hoop_stress]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[temp_inner_func]
type = PiecewiseLinear
xy_data = '0 400
1 350'
[]
[temp_outer_func]
type = PiecewiseLinear
xy_data = '0 400
1 400'
[]
[press_func]
type = PiecewiseLinear
xy_data = '0 15
1 15'
[]
[]
[Kernels]
[heat]
type = HeatConduction
variable = temp
[]
[]
[Modules/TensorMechanics/Master]
[all]
volumetric_locking_correction = true
add_variables = true
incremental = true
strain = FINITE
eigenstrain_names = thermal_expansion
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress hydrostatic_stress'
temperature = temp
[]
[]
[AuxKernels]
[hoop_stress]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = hoop_stress
scalar_type = HoopStress
execute_on = timestep_end
[]
[]
[BCs]
[no_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0.0
[]
[Pressure]
[internal_pressure]
boundary = '4'
factor = 1.e6
function = press_func
[]
[]
[t_in]
type = FunctionDirichletBC
variable = temp
boundary = '4'
function = temp_inner_func
[]
[t_out]
type = FunctionDirichletBC
variable = temp
boundary = '2'
function = temp_outer_func
[]
[]
[Constraints]
[disp_y]
type = EqualValueBoundaryConstraint
variable = disp_y
primary = '65'
secondary = '3'
penalty = 1e18
[]
[]
[Materials]
[thermal1]
type = HeatConductionMaterial
block = '1'
thermal_conductivity = 25.0
specific_heat = 490.0
temp = temp
[]
[elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 193.05e9
poissons_ratio = 0.3
[]
[stress]
type = ComputeFiniteStrainElasticStress
[]
[thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 13e-6
stress_free_temperature = 295.00
temperature = temp
eigenstrain_name = thermal_expansion
[]
[density]
type = Density
block = '1'
density = 8000.0
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-ksp_snes_ew'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = ' 201 hypre boomeramg 4'
line_search = 'none'
l_max_its = 25
nl_max_its = 20
nl_rel_tol = 1e-9
l_tol = 1e-2
start_time = 0.0
dt = 1
end_time = 1
dtmin = 1
[]
[Outputs]
file_base = 2d_out
exodus = true
[console]
type = Console
max_rows = 25
[]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_3D.i)
outer_htc = 10 # W/m^2/K
outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
[left_block]
type = GeneratedMeshGenerator
dim = 3
nx = 3
ny = 6
nz = 6
xmin = -1
xmax = -0.5
ymin = -0.5
ymax = 0.5
zmin = -0.5
zmax = 0.5
elem_type = HEX27
[]
[left_block_sidesets]
type = RenameBoundaryGenerator
input = left_block
old_boundary = '0 1 2 3 4 5'
new_boundary = 'left_bottom left_back left_right left_front left_left left_top'
[]
[left_block_id]
type = SubdomainIDGenerator
input = left_block_sidesets
subdomain_id = 1
[]
[right_block]
type = GeneratedMeshGenerator
dim = 3
nx = 4
ny = 8
nz = 8
xmin = 0.5
xmax = 1
ymin = -0.5
ymax = 0.5
zmin = -0.5
zmax = 0.5
elem_type = HEX27
[]
[right_block_sidesets]
type = RenameBoundaryGenerator
input = right_block
old_boundary = '0 1 2 3 4 5'
# new_boundary = 'right_bottom right_back right_right right_front right_left right_top'
new_boundary = '100 101 102 103 104 105'
[]
[right_block_sidesets_rename]
type = RenameBoundaryGenerator
input = right_block_sidesets
old_boundary = '100 101 102 103 104 105'
new_boundary = 'right_bottom right_back right_right right_front right_left right_top'
[]
[right_block_id]
type = SubdomainIDGenerator
input = right_block_sidesets_rename
subdomain_id = 2
[]
[combined_mesh]
type = MeshCollectionGenerator
inputs = 'left_block_id right_block_id'
[]
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[]
[AuxVariables]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[power_density]
block = 1
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
[]
[heat_source]
type = CoupledForce
variable = temp
block = 1
v = power_density
[]
[]
[AuxKernels]
[gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 'left_right'
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 'right_left'
secondary = 'left_right'
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 5
gap_geometry_type = PLATE
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = 'right_right' # outer RPV
coefficient = ${outer_htc}
T_infinity = ${outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
[Quadrature]
order = fifth
side_order = seventh
[]
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 'left_right'
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 'right_left'
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 'left_right'
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 'right_left'
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 1
[]
[convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = 'right_right' # outer RVP
T_fluid = ${outer_Tinf}
htc = ${outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(convective_out - ptot) / ptot'
pp_names = 'convective_out ptot'
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'left_right right_left'
variable = temp
[]
[]
(modules/combined/examples/phase_field-mechanics/grain_texture.i)
# This simulation predicts GB migration of 8 grains and outputs grain texture information
# Mesh adaptivity is not used so that the VectorPostprocessor's output will be uniform
# Time step adaptivity is used
# An AuxVariable is used to calculate the grain boundary locations
# Postprocessors are used to record time step
[Mesh]
# Mesh block. Meshes can be read in or automatically generated
type = GeneratedMesh
dim = 2 # Problem dimension
nx = 100 # Number of elements in the x-direction
ny = 100 # Number of elements in the y-direction
xmin = 0 # minimum x-coordinate of the mesh
xmax = 1000 # maximum x-coordinate of the mesh
ymin = 0 # minimum y-coordinate of the mesh
ymax = 1000 # maximum y-coordinate of the mesh
elem_type = QUAD4 # Type of elements used in the mesh
[]
[GlobalParams]
# Parameters used by several kernels that are defined globally to simplify input file
op_num = 8 # Number of order parameters used
var_name_base = gr # Base name of grains
grain_num = 8 #Number of grains
[]
[Variables]
# Variable block, where all variables in the simulation are declared
[./PolycrystalVariables]
[../]
[]
[UserObjects]
[./voronoi]
type = PolycrystalVoronoi
coloring_algorithm = bt
[../]
[./grain_tracker]
type = GrainTracker
threshold = 0.2
connecting_threshold = 0.08
[../]
[]
[ICs]
[./PolycrystalICs]
[./PolycrystalColoringIC]
polycrystal_ic_uo = voronoi
[../]
[../]
[]
[AuxVariables]
# Dependent variables
[./bnds]
# Variable used to visualize the grain boundaries in the simulation
order = FIRST
family = LAGRANGE
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./var_indices]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
# Kernel block, where the kernels defining the residual equations are set up.
[./PolycrystalKernel]
# Custom action creating all necessary kernels for grain growth. All input parameters are up in GlobalParams
[../]
[]
[AuxKernels]
# AuxKernel block, defining the equations used to calculate the auxvars
[./bnds_aux]
# AuxKernel that calculates the GB term
type = BndsCalcAux
variable = bnds
execute_on = timestep_end
[../]
[./unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
execute_on = timestep_end
flood_counter = grain_tracker
field_display = UNIQUE_REGION
[../]
[./var_indices]
type = FeatureFloodCountAux
variable = var_indices
execute_on = timestep_end
flood_counter = grain_tracker
field_display = VARIABLE_COLORING
[../]
[]
[BCs]
# Boundary Condition block
[./Periodic]
[./top_bottom]
auto_direction = 'x y' # Makes problem periodic in the x and y directions
[../]
[../]
[]
[Materials]
[./CuGrGr]
# Material properties
type = GBEvolution # Quantitative material properties for copper grain growth. Dimensions are nm and ns
block = 0 # Block ID (only one block in this problem)
GBmob0 = 2.5e-6 #Mobility prefactor for Cu from Schonfelder1997
GBenergy = 0.708 # GB energy in J/m^2
Q = 0.23 #Activation energy for grain growth from Schonfelder 1997
T = 450 # K #Constant temperature of the simulation (for mobility calculation)
wGB = 14 # nm #Width of the diffuse GB
outputs = exodus
[../]
[]
[UserObjects]
[./euler_angle_file]
type = EulerAngleFileReader
file_name = grn_8_rand_2D.tex
[../]
[]
[VectorPostprocessors]
[./gbInfo]
type = GrainTextureVectorPostprocessor
unique_grains = unique_grains
euler_angle_provider = euler_angle_file
sort_by = id # sort output by elem id
[../]
[]
[Executioner]
type = Transient # Type of executioner, here it is transient with an adaptive time step
scheme = bdf2 # Type of time integration (2nd order backward euler), defaults to 1st order backward euler
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -mat_mffd_type'
petsc_options_value = 'hypre boomeramg 101 ds'
l_max_its = 30 # Max number of linear iterations
l_tol = 1e-4 # Relative tolerance for linear solves
nl_max_its = 40 # Max number of nonlinear iterations
nl_abs_tol = 1e-11 # Relative tolerance for nonlinear solves
nl_rel_tol = 1e-10 # Absolute tolerance for nonlinear solves
start_time = 0.0
num_steps = 50
[./TimeStepper]
type = IterationAdaptiveDT
dt = 25 # Initial time step. In this simulation it changes.
optimal_iterations = 6 # Time step will adapt to maintain this number of nonlinear iterations
[../]
[]
[Outputs]
execute_on = 'INITIAL TIMESTEP_END'
exodus = true
csv = true
perf_graph = true
[./console]
type = Console
max_rows = 20
[../]
[]
(modules/porous_flow/test/tests/sinks/s05.i)
# apply a half-gaussian sink flux and observe the correct behavior
[Mesh]
type = GeneratedMesh
dim = 3
nx = 1
ny = 1
nz = 1
xmin = 0
xmax = 1
ymin = 0
ymax = 1
zmin = 0
zmax = 2
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = 'pp'
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1.1
[]
[]
[Variables]
[pp]
[]
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = y+1.4
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1.3
density0 = 1.1
thermal_expansion = 0
viscosity = 1.1
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1E-5 0 0 0 1E-5 0 0 0 1E-5'
[]
[relperm]
type = PorousFlowRelativePermeabilityCorey
n = 2
phase = 0
[]
[]
[AuxVariables]
[flux_out]
[]
[]
[Functions]
[mass10]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)*if(pp>=0,1,pow(1+pow(-al*pp,1.0/(1-m)),-m))'
symbol_names = 'vol por dens0 pp bulk al m'
symbol_values = '0.25 0.1 1.1 p10 1.3 1.1 0.5'
[]
[rate10]
type = ParsedFunction
expression = 'if(pp>center,fcn,fcn*exp(-0.5*(pp-center)*(pp-center)/sd/sd))'
symbol_names = 'fcn pp center sd'
symbol_values = '6 p10 0.9 0.5'
[]
[mass10_expect]
type = ParsedFunction
expression = 'mass_prev-rate*area*dt'
symbol_names = 'mass_prev rate area dt'
symbol_values = 'm10_prev m10_rate 0.5 2E-3'
[]
[mass11]
type = ParsedFunction
expression = 'vol*por*dens0*exp(pp/bulk)*if(pp>=0,1,pow(1+pow(-al*pp,1.0/(1-m)),-m))'
symbol_names = 'vol por dens0 pp bulk al m'
symbol_values = '0.25 0.1 1.1 p11 1.3 1.1 0.5'
[]
[rate11]
type = ParsedFunction
expression = 'if(pp>center,fcn,fcn*exp(-0.5*(pp-center)*(pp-center)/sd/sd))'
symbol_names = 'fcn pp center sd'
symbol_values = '6 p11 0.9 0.5'
[]
[mass11_expect]
type = ParsedFunction
expression = 'mass_prev-rate*area*dt'
symbol_names = 'mass_prev rate area dt'
symbol_values = 'm11_prev m11_rate 0.5 2E-3'
[]
[]
[Postprocessors]
[flux10]
type = PointValue
variable = flux_out
point = '1 0 0'
[]
[p00]
type = PointValue
point = '0 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p10]
type = PointValue
point = '1 0 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m10]
type = FunctionValuePostprocessor
function = mass10
execute_on = 'initial timestep_end'
[]
[m10_prev]
type = FunctionValuePostprocessor
function = mass10
execute_on = 'timestep_begin'
outputs = 'console'
[]
[m10_rate]
type = FunctionValuePostprocessor
function = rate10
execute_on = 'timestep_end'
[]
[m10_expect]
type = FunctionValuePostprocessor
function = mass10_expect
execute_on = 'timestep_end'
[]
[p01]
type = PointValue
point = '0 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[p11]
type = PointValue
point = '1 1 0'
variable = pp
execute_on = 'initial timestep_end'
[]
[m11]
type = FunctionValuePostprocessor
function = mass11
execute_on = 'initial timestep_end'
[]
[m11_prev]
type = FunctionValuePostprocessor
function = mass11
execute_on = 'timestep_begin'
outputs = 'console'
[]
[m11_rate]
type = FunctionValuePostprocessor
function = rate11
execute_on = 'timestep_end'
[]
[m11_expect]
type = FunctionValuePostprocessor
function = mass11_expect
execute_on = 'timestep_end'
[]
[]
[BCs]
[flux]
type = PorousFlowHalfGaussianSink
boundary = 'right'
max = 6
sd = 0.5
center = 0.9
variable = pp
use_mobility = false
use_relperm = false
fluid_phase = 0
flux_function = 1
save_in = flux_out
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -snes_max_it -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'gmres asm lu 10000 NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 2E-3
end_time = 6E-2
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[Outputs]
file_base = s05
[console]
type = Console
execute_on = 'nonlinear linear'
time_step_interval = 5
[]
[csv]
type = CSV
execute_on = 'timestep_end'
time_step_interval = 3
[]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_3D_mortar.i)
outer_htc = 10 # W/m^2/K
outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Mesh]
[left_block]
type = GeneratedMeshGenerator
dim = 3
nx = 3
ny = 6
nz = 6
xmin = -1
xmax = -0.5
ymin = -0.5
ymax = 0.5
zmin = -0.5
zmax = 0.5
elem_type = HEX27
[]
[left_block_sidesets]
type = RenameBoundaryGenerator
input = left_block
old_boundary = '0 1 2 3 4 5'
new_boundary = 'left_bottom left_back left_right left_front left_left left_top'
[]
[left_block_id]
type = SubdomainIDGenerator
input = left_block_sidesets
subdomain_id = 1
[]
[right_block]
type = GeneratedMeshGenerator
dim = 3
nx = 4
ny = 8
nz = 8
xmin = 0.5
xmax = 1
ymin = -0.5
ymax = 0.5
zmin = -0.5
zmax = 0.5
elem_type = HEX27
[]
[right_block_sidesets]
type = RenameBoundaryGenerator
input = right_block
old_boundary = '0 1 2 3 4 5'
# new_boundary = 'right_bottom right_back right_right right_front right_left right_top'
new_boundary = '100 101 102 103 104 105'
[]
[right_block_sidesets_rename]
type = RenameBoundaryGenerator
input = right_block_sidesets
old_boundary = '100 101 102 103 104 105'
new_boundary = 'right_bottom right_back right_right right_front right_left right_top'
[]
[right_block_id]
type = SubdomainIDGenerator
input = right_block_sidesets_rename
subdomain_id = 2
[]
[combined_mesh]
type = MeshCollectionGenerator
inputs = 'left_block_id right_block_id'
[]
[left_lower]
type = LowerDBlockFromSidesetGenerator
input = combined_mesh
sidesets = 'left_right'
new_block_id = '10001'
new_block_name = 'secondary_lower'
[]
[right_lower]
type = LowerDBlockFromSidesetGenerator
input = left_lower
sidesets = 'right_left'
new_block_id = '10000'
new_block_name = 'primary_lower'
[]
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[lm]
order = SECOND
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[AuxVariables]
[power_density]
block = 1
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
block = '1 2'
[]
[heat_source]
type = CoupledForce
variable = temp
block = '1'
v = power_density
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 'left_right'
primary_emissivity = 0.0
secondary_emissivity = 0.0
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 'left_right'
gap_conductivity = 5.0
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
primary_boundary = 'right_left'
primary_subdomain = 'primary_lower'
secondary_boundary = 'left_right'
secondary_subdomain = 'secondary_lower'
gap_flux_models = 'radiation conduction'
gap_geometry_type = PLATE
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = 'right_right' # outer RPV
coefficient = ${outer_htc}
T_infinity = ${outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-8
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 'left_right'
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 'right_left'
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 'left_right'
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 'right_left'
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 1
[]
[convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = 'right_right' # outer RVP
T_fluid = ${outer_Tinf}
htc = ${outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(convective_out - ptot) / ptot'
pp_names = 'convective_out ptot'
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = 'left_right right_left'
variable = temp
[]
[]
(modules/xfem/test/tests/solid_mechanics_basic/elliptical_crack.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
file = quarter_sym.e
[]
[DomainIntegral]
integrals = 'InteractionIntegralKI'
crack_direction_method = CurvedCrackFront
radius_inner = '0.1'
radius_outer = '0.2'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 1
crack_front_points_provider = ellip_cut_uo
number_points_from_provider = 12
closed_loop = true
incremental = true
[]
[UserObjects]
[./ellip_cut_uo]
type = EllipseCutUserObject
cut_data = '-0.5 -0.5 0
-0.5 -0.1 0
0.1 -0.5 0'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[Functions]
[./top_trac_z]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_z]
type = FunctionNeumannBC
boundary = 2
variable = disp_z
function = top_trac_z
[../]
[./bottom_x]
type = DirichletBC
boundary = 1
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = 1
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = 1
variable = disp_z
value = 0.0
[../]
[./sym_y]
type = DirichletBC
boundary = 3
variable = disp_y
value = 0.0
[../]
[./sym_x]
type = DirichletBC
boundary = 4
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
file_base = elliptical_crack_out
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/coord_type/coord_type_rz_general.i)
# Tests using different coordinate systems in different blocks:
# block1: XYZ translated by (0,-1,0)
# block2: RZ with origin=(0,0,0) and direction=(0,1,0)
# block3: RZ with origin=(0,0,1) and direction=(1,0,0)
# block4: RZ with origin=(-1,-2,-3) and direction=(1,1,0)
#
# A transient heat conduction equation is solved with uniform properties.
# The same power is applied to each block via a uniform heat flux boundary
# condition on the outer cylindrical surface (top surface for block1).
# Conservation is checked for each via post-processors.
# Blocks block2, block3, and block4 should have identical solutions.
rho = 1000.0
cp = 500.0
k = 15.0
length = 1.5
radius = 0.5
perimeter = ${fparse 2 * pi * radius}
nz = 10
nr = 5
power = 1e3
heat_flux = ${fparse power / (perimeter * length)}
[Mesh]
# block1
[genmesh1]
type = GeneratedMeshGenerator
dim = 2
nx = ${nz}
ny = ${nr}
xmin = 0.0
xmax = ${length}
ymin = -1.0
ymax = ${fparse -1.0 + radius}
boundary_id_offset = 10
[]
[renumberblock1]
type = RenameBlockGenerator
input = genmesh1
old_block = 0
new_block = 1
[]
[renameblock1]
type = RenameBlockGenerator
input = renumberblock1
old_block = 1
new_block = block1
[]
[renameboundary1]
type = RenameBoundaryGenerator
input = renameblock1
old_boundary = '10 11 12 13'
new_boundary = 'bottom1 right1 top1 left1'
[]
# block2
[genmesh2]
type = GeneratedMeshGenerator
dim = 2
nx = ${nr}
ny = ${nz}
xmin = 0.0
xmax = ${radius}
ymin = 0
ymax = ${length}
boundary_id_offset = 20
[]
[renumberblock2]
type = RenameBlockGenerator
input = genmesh2
old_block = 0
new_block = 2
[]
[renameblock2]
type = RenameBlockGenerator
input = renumberblock2
old_block = 2
new_block = block2
[]
[renameboundary2]
type = RenameBoundaryGenerator
input = renameblock2
old_boundary = '20 21 22 23'
new_boundary = 'bottom2 right2 top2 left2'
[]
# block3
[genmesh3]
type = GeneratedMeshGenerator
dim = 2
nx = ${nz}
ny = ${nr}
xmin = 0.0
xmax = ${length}
ymin = 0
ymax = ${radius}
boundary_id_offset = 30
[]
[translate3]
type = TransformGenerator
input = genmesh3
transform = TRANSLATE
vector_value = '0 0 1'
[]
[renumberblock3]
type = RenameBlockGenerator
input = translate3
old_block = 0
new_block = 3
[]
[renameblock3]
type = RenameBlockGenerator
input = renumberblock3
old_block = 3
new_block = block3
[]
[renameboundary3]
type = RenameBoundaryGenerator
input = renameblock3
old_boundary = '30 31 32 33'
new_boundary = 'bottom3 right3 top3 left3'
[]
# block4
[genmesh4]
type = GeneratedMeshGenerator
dim = 2
nx = ${nz}
ny = ${nr}
xmin = 0.0
xmax = ${length}
ymin = 0
ymax = ${radius}
boundary_id_offset = 40
[]
[rotate4]
type = TransformGenerator
input = genmesh4
transform = ROTATE
vector_value = '45 0 0'
[]
[translate4]
type = TransformGenerator
input = rotate4
transform = TRANSLATE
vector_value = '-1 -2 -3'
[]
[renumberblock4]
type = RenameBlockGenerator
input = translate4
old_block = 0
new_block = 4
[]
[renameblock4]
type = RenameBlockGenerator
input = renumberblock4
old_block = 4
new_block = block4
[]
[renameboundary4]
type = RenameBoundaryGenerator
input = renameblock4
old_boundary = '40 41 42 43'
new_boundary = 'bottom4 right4 top4 left4'
[]
[combiner]
type = CombinerGenerator
inputs = 'renameboundary1 renameboundary2 renameboundary3 renameboundary4'
[]
coord_block = 'block1 block2 block3 block4'
coord_type = 'XYZ RZ RZ RZ'
rz_coord_blocks = 'block2 block3 block4'
rz_coord_origins = '0 0 0
0 0 1
-1 -2 -3'
rz_coord_directions = '0 1 0
1 0 0
1 1 0'
[]
[Variables]
[T]
family = LAGRANGE
order = FIRST
[]
[]
[Functions]
[T_ic_fn]
type = ParsedFunction
expression = 'x'
[]
[theoretical_energy_added_fn]
type = ParsedFunction
expression = '${power} * t'
[]
[]
[ICs]
[T_ic]
type = FunctionIC
variable = T
function = T_ic_fn
[]
[]
[Kernels]
[time_derivative]
type = ADTimeDerivative
variable = T
[]
[heat_conduction]
type = CoefDiffusion
variable = T
coef = ${fparse k / (rho * cp)}
[]
[]
[BCs]
[heat_flux_bc]
type = ADFunctionNeumannBC
variable = T
boundary = 'top1 right2 top3 top4'
# The heat conduction equation has been divided by rho*cp
function = '${fparse heat_flux / (rho * cp)}'
[]
[]
[Postprocessors]
[theoretical_energy_change]
type = FunctionValuePostprocessor
function = theoretical_energy_added_fn
execute_on = 'INITIAL TIMESTEP_END'
[]
# block1 conservation
[T_integral1]
type = ElementIntegralVariablePostprocessor
variable = T
block = 'block1'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy1]
type = ParsedPostprocessor
pp_names = 'T_integral1'
expression = 'T_integral1 * ${rho} * ${cp} * ${perimeter}'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change1]
type = ChangeOverTimePostprocessor
postprocessor = energy1
change_with_respect_to_initial = true
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change_error1]
type = RelativeDifferencePostprocessor
value1 = energy_change1
value2 = theoretical_energy_change
execute_on = 'INITIAL TIMESTEP_END'
[]
# block2 conservation
[T_integral2]
type = ElementIntegralVariablePostprocessor
variable = T
block = 'block2'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy2]
type = ParsedPostprocessor
pp_names = 'T_integral2'
expression = 'T_integral2 * ${rho} * ${cp}'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change2]
type = ChangeOverTimePostprocessor
postprocessor = energy2
change_with_respect_to_initial = true
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change_error2]
type = RelativeDifferencePostprocessor
value1 = energy_change2
value2 = theoretical_energy_change
execute_on = 'INITIAL TIMESTEP_END'
[]
# block3 conservation
[T_integral3]
type = ElementIntegralVariablePostprocessor
variable = T
block = 'block3'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy3]
type = ParsedPostprocessor
pp_names = 'T_integral3'
expression = 'T_integral3 * ${rho} * ${cp}'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change3]
type = ChangeOverTimePostprocessor
postprocessor = energy3
change_with_respect_to_initial = true
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change_error3]
type = RelativeDifferencePostprocessor
value1 = energy_change3
value2 = theoretical_energy_change
execute_on = 'INITIAL TIMESTEP_END'
[]
# block4 conservation
[T_integral4]
type = ElementIntegralVariablePostprocessor
variable = T
block = 'block4'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy4]
type = ParsedPostprocessor
pp_names = 'T_integral4'
expression = 'T_integral4 * ${rho} * ${cp}'
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change4]
type = ChangeOverTimePostprocessor
postprocessor = energy4
change_with_respect_to_initial = true
execute_on = 'INITIAL TIMESTEP_END'
[]
[energy_change_error4]
type = RelativeDifferencePostprocessor
value1 = energy_change4
value2 = theoretical_energy_change
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = bdf2
dt = 1.0
num_steps = 10
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-10
[]
[Outputs]
file_base = 'coord_type_rz_general'
[console]
type = Console
show = 'energy_change_error1 energy_change_error2 energy_change_error3 energy_change_error4'
[]
[exodus]
type = Exodus
show = 'T energy_change_error1 energy_change_error2 energy_change_error3 energy_change_error4'
[]
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q4/hertz_cyl_half_1deg_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x226]
type = NodalVariableValue
nodeid = 225
variable = disp_x
[../]
[./disp_y226]
type = NodalVariableValue
nodeid = 225
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-5
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 3.5
l_tol = 1e-3
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x226 disp_y226 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+10
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_2/cyl2_template1.i)
#
# This input file is a template for both the frictionless and glued test
# variations for the current problem geometry. In order to create an input
# file to run outside the runtest framework, look at the tests file and add the
# appropriate input file lines from the cli_args line.
#
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl2_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 1000
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/navier_stokes/test/tests/finite_element/pins/expansion-channel/expansion-channel-slip-wall.i)
# This is an example showing the conservative form with combined velocity inlet condition,
# pressure outlet condition and slip wall boundary condition.
[GlobalParams]
gravity = '0 -9.8 0'
order = FIRST
family = LAGRANGE
u = vel_x
v = vel_y
pressure = p
temperature = T
porosity = porosity
eos = eos
conservative_form = true
p_int_by_parts = true
[]
[Mesh]
[file]
type = FileMeshGenerator
file = expansion-channel.e
[]
[add_corners]
type = ExtraNodesetGenerator
input = file
new_boundary = 'corners'
coord = '-0.05 -0.5 0; 0.05 -0.5 0; -0.1 0.5 0; 0.1 0.5 0'
[]
[]
[NodalNormals]
# boundaries 3 (left) and 4 (right) are walls
boundary = '3 4'
corner_boundary = 'corners'
[]
[FluidProperties]
[eos]
type = SimpleFluidProperties
density0 = 100 # kg/m^3
thermal_expansion = 0.001 # K^{-1}
cp = 100
viscosity = 0.1 # Pa-s, Re=rho*u*L/mu = 100*1*0.1/0.1 = 100
thermal_conductivity = 72
[]
[]
[Variables]
# velocities
[vel_x]
scaling = 1e-1
initial_condition = 0
[]
[vel_y]
scaling = 1e-2
initial_condition = 1
[]
# Pressure
[p]
initial_condition = 1.01e5
[]
# Temperature
[T]
scaling = 1e-4
initial_condition = 630
[]
[]
[AuxVariables]
[rho]
initial_condition = 77.0
[]
[porosity]
initial_condition = 0.6
[]
[vol_heat]
initial_condition = 1e3
[]
[]
[Materials]
[mat]
type = PINSFEMaterial
alpha = 1e3
beta = 100
[]
[]
[Kernels]
# mass balance (continuity) equation
[mass_time]
type = PINSFEFluidPressureTimeDerivative
variable = p
[]
[mass_space]
type = INSFEFluidMassKernel
variable = p
[]
# momentum equations for x- and y- velocities
[x_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_x
[]
[x_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_x
component = 0
[]
[y_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_y
[]
[y_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_y
component = 1
[]
# fluid energy equation
[temperature_time]
type = PINSFEFluidTemperatureTimeDerivative
variable = T
[]
[temperature_space]
type = INSFEFluidEnergyKernel
variable = T
power_density = vol_heat
[]
[]
[AuxKernels]
[rho_aux]
type = FluidDensityAux
variable = rho
p = p
T = T
fp = eos
[]
[]
[BCs]
# BCs for mass equation
# Inlet
[mass_inlet]
type = INSFEFluidMassBC
variable = p
boundary = '1'
[]
# Outlet
[mass_out]
type = INSFEFluidMassBC
variable = p
boundary = '2'
[]
# BCs for x-momentum equation
# Inlet
[vx_in]
type = INSFEFluidMomentumBC
variable = vel_x
boundary = '1'
component = 0
#p_fn = 1.05e5
v_fn = 1
[]
# Outlet
[vx_out]
type = INSFEFluidMomentumBC
variable = vel_x
boundary = '2'
component = 0
p_fn = 1e5
[]
# Walls (left and right walls)
[vx_wall]
type = INSFEFluidWallMomentumBC
variable = vel_x
boundary = '3 4'
component = 0
[]
# BCs for y-momentum equation
# Inlet
[vy_in]
type = INSFEFluidMomentumBC
variable = vel_y
boundary = '1'
component = 1
v_fn = 1
[]
# Outlet
[vy_out]
type = INSFEFluidMomentumBC
variable = vel_y
boundary = '2'
component = 1
p_fn = 1e5
[]
# Walls (left and right walls)
[vy_wall]
type = INSFEFluidWallMomentumBC
variable = vel_y
boundary = '3 4'
component = 1
[]
# Special slip-wall BCs for both x- and y- velocities
[slipwall]
type = INSFEMomentumFreeSlipBC
boundary = '3 4'
variable = vel_x
u = vel_x
v = vel_y
[]
# BCs for fluid energy equation
# Inlet
[T_in]
type = INSFEFluidEnergyBC
variable = T
boundary = '1'
T_fn = 630
[]
# Outlet
[T_out]
type = INSFEFluidEnergyBC
variable = T
boundary = '2'
T_fn = 630
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = FDP
full = true
solve_type = 'PJFNK'
[]
[]
[Executioner]
type = Transient
dt = 0.2
dtmin = 1.e-6
[TimeStepper]
type = IterationAdaptiveDT
growth_factor = 1.25
optimal_iterations = 15
linear_iteration_ratio = 100
dt = 0.1
cutback_factor = 0.5
cutback_factor_at_failure = 0.5
[]
dtmax = 25
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
nl_max_its = 12
l_tol = 1e-5
l_max_its = 100
start_time = 0.0
end_time = 500
num_steps = 2
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
time_step_interval = 1
execute_on = 'initial timestep_end'
[console]
type = Console
output_linear = false
[]
[out]
type = Exodus
use_displaced = false
[]
[]
(modules/thermal_hydraulics/test/tests/components/heat_structure_base/phy.variable_init_t.i)
# Tests that a function can be used to initialize temperature in a heat structure.
[GlobalParams]
[]
[Functions]
[fn-initial_T]
type = ParsedFunction
expression = 'baseT + (dT * sin((pi * x) / length))'
symbol_names = 'baseT dT length'
symbol_values = '560.0 30.0 3.6576'
[]
[]
[SolidProperties]
[fuel-mat]
type = ThermalFunctionSolidProperties
k = 3.65
cp = 288.734
rho = 1.0412e2
[]
[gap-mat]
type = ThermalFunctionSolidProperties
k = 0.1
cp = 1.0
rho = 1.0
[]
[clad-mat]
type = ThermalFunctionSolidProperties
k = 16.48672
cp = 321.384
rho = 6.6e1
[]
[]
[Components]
[hs]
type = HeatStructureCylindrical
position = '0 0 0'
orientation = '1 0 0'
length = 3.6576
n_elems = 100
names = 'FUEL GAP CLAD'
widths = '0.0046955 0.0000955 0.000673'
n_part_elems = '10 3 3'
solid_properties = 'fuel-mat gap-mat clad-mat'
solid_properties_T_ref = '300 300 300'
initial_T = fn-initial_T
[]
[temp_outside]
type = HSBoundarySpecifiedTemperature
hs = hs
boundary = hs:outer
T = 580.0
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
start_time = 0
dt = 0.01
num_steps = 10
abort_on_solve_fail = true
solve_type = 'PJFNK'
nl_rel_tol = 1e-5
nl_abs_tol = 1e-6
nl_max_its = 8
l_tol = 1e-4
l_max_its = 10
[]
[Outputs]
[out]
type = Exodus
[]
[console]
type = Console
execute_scalars_on = none
[]
[]
(test/tests/relationship_managers/default_ghosting/default_ghosting.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
# Show that we can enable and see that libmesh Ghosting Functors are active
[Problem]
default_ghosting = true
[]
(test/tests/time_integrators/actually_explicit_euler_verification/ee-1d-linear.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 200
elem_type = EDGE2
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = x
[../]
[./exact_fn]
type = ParsedFunction
expression = t*x
[../]
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
lumping = true
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1'
function = exact_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
start_time = 0.0
num_steps = 20
dt = 0.00005
[./TimeIntegrator]
type = ActuallyExplicitEuler
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/equal_value.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMEqualValueAtInterface
geometric_cut_userobject = 'line_seg_cut_uo'
use_displaced_mesh = false
variable = u
value = 1
alpha = 1e5
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_3/cyl3_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl3_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = cyl3_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = cyl3_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(test/tests/postprocessors/variable_residual_norm/variable_residual.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = -1
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[Functions]
[./leg1]
type = ParsedFunction
expression = 'x'
[../]
[./leg2]
type = ParsedFunction
expression = '0.5*(3.0*x*x-1.0)'
[../]
[]
[BCs]
[./left_u]
type = DirichletBC
variable = u
preset = false
boundary = 1
value = 0
[../]
[./right_u]
type = DirichletBC
variable = u
preset = false
boundary = 2
value = 1
[../]
[./left_v]
type = DirichletBC
variable = v
preset = false
boundary = 1
value = 200
[../]
[./right_v]
type = DirichletBC
variable = v
preset = false
boundary = 2
value = 100
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
# this is large on purpose so we don't reduce the variable residual to machine zero
# and so that we can compare to larger numbers. This also means this test can run only
# in serial, since parallel runs yield different convergence history.
nl_rel_tol = 1e-4
[]
[Postprocessors]
[./u_res_l2]
type = VariableResidual
variable = u
[../]
[./v_res_l2]
type = VariableResidual
variable = v
[../]
[]
[Outputs]
csv = true
[./console]
type = Console
# turn this on, so we can visually compare the postprocessor value with what is computed by the Console object
all_variable_norms = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_4/ring4_template2.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring4_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
al_penetration_tolerance = 1e-8
[../]
[]
(test/tests/time_integrators/actually_explicit_euler_verification/ee-2d-quadratic.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 10
ny = 10
elem_type = QUAD9
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = ((x*x)+(y*y))-(4*t)
[../]
[./exact_fn]
type = ParsedFunction
expression = t*((x*x)+(y*y))
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1 2 3'
function = exact_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
l_tol = 1e-13
start_time = 0.0
num_steps = 20
dt = 0.00005
[./TimeIntegrator]
type = ActuallyExplicitEuler
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/navier_stokes/test/tests/finite_element/pins/channel-flow/pressure_gradient.i)
# This test case tests the porous-medium flow driven by pressure gradient
#
# At the steady state, eps * grad_p = alpha * u + beta * u^2
# With eps = 0.4, L = 1, grad_p = 1e3/1 = 1e3, alpha = 0, beta = 1000
# u = (eps * grad_p) / beta = 0.4 * 1e3 / 1000 = 0.4 m/s
# This can be verified by check the vel_x at the steady state
[GlobalParams]
gravity = '0 0 0'
order = FIRST
family = LAGRANGE
u = vel_x
v = vel_y
pressure = p
temperature = T
porosity = porosity
eos = eos
conservative_form = false
p_int_by_parts = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
nx = 10
ny = 4
elem_type = QUAD4
[]
[FluidProperties]
[./eos]
type = SimpleFluidProperties
density0 = 100 # kg/m^3
thermal_expansion = 0 # K^{-1}
cp = 100
viscosity = 0.1 # Pa-s, Re=rho*u*L/mu = 100*1*0.1/0.1 = 100
[../]
[]
[Variables]
# velocity
[vel_x]
initial_condition = 1
[]
[vel_y]
initial_condition = 0
[]
# Pressure
[p]
initial_condition = 1e5
[]
[]
[AuxVariables]
[rho]
initial_condition = 100
[]
# Temperature
[T]
initial_condition = 630
[]
[porosity]
initial_condition = 0.4
[]
[]
[Materials]
[mat]
type = PINSFEMaterial
alpha = 0
beta = 1000
[]
[]
[Kernels]
[mass_time]
type = PINSFEFluidPressureTimeDerivative
variable = p
[]
[mass_space]
type = INSFEFluidMassKernel
variable = p
[]
[x_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_x
[]
[x_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_x
component = 0
[]
[y_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_y
[]
[y_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_y
component = 1
[]
[]
[AuxKernels]
[rho_aux]
type = FluidDensityAux
variable = rho
p = p
T = T
fp = eos
[]
[]
[BCs]
# BCs for mass equation
# Inlet
[mass_inlet]
type = INSFEFluidMassBC
variable = p
boundary = 'left'
[]
# Outlet
[mass_outlet]
type = INSFEFluidMassBC
variable = p
boundary = 'right'
[]
# BCs for x-momentum equation
# Inlet
[vx_in]
type = INSFEFluidMomentumBC
variable = vel_x
component = 0
boundary = 'left'
p_fn = 1.01e5
[]
# Outlet
[vx_out]
type = INSFEFluidMomentumBC
variable = vel_x
component = 0
boundary = 'right'
p_fn = 1e5
[]
# BCs for y-momentum equation
# Both Inlet and Outlet, and Top and Bottom
[vy]
type = DirichletBC
variable = vel_y
boundary = 'left right bottom top'
value = 0
[]
[]
[Postprocessors]
[v_in]
type = SideAverageValue
variable = vel_x
boundary = 'left'
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
solve_type = 'PJFNK'
[]
[]
[Executioner]
type = Transient
dt = 5
dtmin = 1.e-3
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
nl_max_its = 20
l_tol = 1e-5
l_max_its = 100
start_time = 0.0
end_time = 50
num_steps = 5
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
time_step_interval = 1
execute_on = 'initial timestep_end'
[console]
type = Console
output_linear = false
[]
[out]
type = Exodus
use_displaced = false
[]
[]
(modules/contact/test/tests/verification/patch_tests/plane_2/plane2_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane2_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_3/ring3_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring3_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
petsc_options = '-mat_superlu_dist_iterrefine -mat_superlu_dist_replacetinypivot'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/xfem/test/tests/bimaterials/inclusion_ad_bimaterials_2d.i)
# This test is for a matrix-inclusion composite materials using AD
# The global stress is determined by switching the stress based on level set values
# The inclusion geometry is marked by a level set function
# The matrix and inclusion are glued together
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'sqrt((y-2.5)*(y-2.5) + (x-2.5)*(x-2.5)) - 1.5'
[../]
[]
[AuxVariables]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
use_automatic_differentiation = true
add_variables = true
generate_output = 'stress_xx stress_yy stress_xy'
[../]
[]
[AuxKernels]
[./a_strain_xx]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = ADDirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = ADDirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = ADFunctionDirichletBC
boundary = top
variable = disp_x
function = '0.03*t'
[../]
[./topy]
type = ADFunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ADComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ADComputeSmallStrain
base_name = A
[../]
[./stress_A]
type = ADComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ADComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e5
poissons_ratio = 0.3
[../]
[./strain_B]
type = ADComputeSmallStrain
base_name = B
[../]
[./stress_B]
type = ADComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = ADLevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-8
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-50 #1e-7
# time control
start_time = 0.0
dt = 0.5
end_time = 1.0
num_steps = 2
max_xfem_update = 1
[]
[Outputs]
exodus = true
file_base = inclusion_bimaterials_2d_out
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/mortar_cartesian_lms/cylinder_friction_cartesian_pg.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '3'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '2'
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
converge_on = 'disp_x disp_y'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[lm_x]
block = 'secondary_lower'
use_dual = true
scaling = 1.0e-5
[]
[lm_y]
block = 'secondary_lower'
use_dual = true
scaling = 1.0e-5
[]
[]
[AuxVariables]
[aux_lm]
block = 'secondary_lower'
use_dual = false
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Modules/TensorMechanics/Master]
[all]
incremental = false
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
strain = SMALL
add_variables = false
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[]
[_dt]
type = TimestepSize
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff1_stress]
type = ComputeLinearElasticStress
block = '1'
[]
[stuff2_stress]
type = ComputeLinearElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason -ksp_converged_reason -pc_svd_monitor '
'-snes_linesearch_monitor'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu NONZERO 1e-12'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 5
nl_rel_tol = 1e-09
start_time = -0.1
end_time = 0.3 # 3.5
l_tol = 1e-8
dt = 0.1
dtmin = 0.001
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[]
[y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[]
[lm_x]
type = NodalValueSampler
variable = lm_x
boundary = '3'
sort_by = id
[]
[lm_y]
type = NodalValueSampler
variable = lm_y
boundary = '3'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = false
[console]
type = Console
max_rows = 5
[]
[chkfile]
type = CSV
show = 'x_disp y_disp lm_x lm_y'
file_base = cylinder_friction_check
create_final_symlink = true
execute_on = 'FINAL'
[]
[]
[Constraints]
[weighted_gap_lm]
type = ComputeFrictionalForceCartesianLMMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
lm_x = lm_x
lm_y = lm_y
variable = lm_x
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
correct_edge_dropping = false
mu = 0.4
c_t = 1.0e6
c = 1.0e6
use_petrov_galerkin = true
aux_lm = aux_lm
[]
[x]
type = CartesianMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = lm_x
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
correct_edge_dropping = false
[]
[y]
type = CartesianMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = lm_y
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
correct_edge_dropping = false
[]
[]
(test/tests/markers/two_circle_marker/two_circle_marker_gaussian_ic.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[ICs]
[./gaussian_ic]
type = FunctionIC
variable = u
function = gaussian_2d
[../]
[]
[Functions]
[./gaussian_2d]
type = ParsedFunction
expression = exp(-((x-x0)*(x-x0)+(y-y0)*(y-y0))/2.0/sigma/sigma)
symbol_names = 'sigma x0 y0'
symbol_values = '0.05 0.35 0.25'
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.02
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Transient
num_steps = 6
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
initial_steps = 1
initial_marker = two_circle_marker
cycles_per_step = 1
marker = two_circle_marker
max_h_level = 1
[./Markers]
[./two_circle_marker]
type = TwoCircleMarker
point1 = '0.5 0.5 0'
radius1 = 0.3
point2 = '0.35 0.25 0'
radius2 = 0.3
shut_off_time = 0.15
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(test/tests/transfers/multiapp_conservative_transfer/parent_conservative_transfer.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[u]
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[]
[BCs]
[left]
type = DirichletBC
variable = u
boundary = left
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[MultiApps]
[sub]
type = FullSolveMultiApp
input_files = sub_conservative_transfer.i
execute_on = timestep_end
[]
[]
[Postprocessors]
[from_postprocessor]
type = ElementIntegralVariablePostprocessor
variable = u
[]
[]
[Transfers]
[to_sub]
type = MultiAppGeneralFieldShapeEvaluationTransfer
source_variable = u
variable = aux_u
to_multi_app = sub
from_postprocessors_to_be_preserved = 'from_postprocessor'
to_postprocessors_to_be_preserved = 'to_postprocessor'
[]
[]
[Outputs]
exodus = true
[console]
type = Console
execute_postprocessors_on = 'INITIAL nonlinear TIMESTEP_END'
[]
[]
(modules/xfem/test/tests/crack_tip_enrichment/edge_crack_2d.i)
[XFEM]
qrule = volfrac
output_cut_plane = true
use_crack_tip_enrichment = true
crack_front_definition = crack_tip
enrichment_displacements = 'enrich1_x enrich2_x enrich3_x enrich4_x enrich1_y enrich2_y enrich3_y enrich4_y'
displacements = 'disp_x disp_y'
cut_off_boundary = all
cut_off_radius = 0.2
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 1.0 0.5 1.0'
time_start_cut = 0.0
time_end_cut = 0.0
[../]
[./crack_tip]
type = CrackFrontDefinition
crack_direction_method = CrackDirectionVector
crack_front_points = '0.5 1.0 0'
crack_direction_vector = '1 0 0'
2d = true
axis_2d = 2
[../]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 9
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 2.0
elem_type = QUAD4
[]
[./all_node]
type = BoundingBoxNodeSetGenerator
new_boundary = 'all'
top_right = '1 2 0'
bottom_left = '0 0 0'
input = gen
[../]
[./right_bottom_node]
type = ExtraNodesetGenerator
new_boundary = 'right_bottom_node'
coord = '1.0 0.0'
input = all_node
[../]
[./right_top_node]
type = ExtraNodesetGenerator
new_boundary = 'right_top_node'
coord = '1.0 2.0'
input = right_bottom_node
[../]
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./vonmises]
type = RankTwoScalarAux
rank_two_tensor = stress
variable = vonmises
scalar_type = vonmisesStress
execute_on = timestep_end
[../]
[]
[BCs]
[./top_y]
type = Pressure
variable = disp_y
boundary = top
factor = -1
displacements = 'disp_x disp_y'
[../]
[./bottom_y]
type = Pressure
variable = disp_y
boundary = bottom
factor = -1
displacements = 'disp_x disp_y'
[../]
[./fix_y]
type = DirichletBC
boundary = right_bottom_node
variable = disp_y
value = 0.0
[../]
[./fix_x]
type = DirichletBC
boundary = right_bottom_node
variable = disp_x
value = 0.0
[../]
[./fix_x2]
type = DirichletBC
boundary = right_top_node
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./strain]
type = ComputeCrackTipEnrichmentSmallStrain
displacements = 'disp_x disp_y'
crack_front_definition = crack_tip
enrichment_displacements = 'enrich1_x enrich2_x enrich3_x enrich4_x enrich1_y enrich2_y enrich3_y enrich4_y'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
# Since we do not sub-triangularize the tip element,
# we need to use higher order quadrature rule to improve
# integration accuracy.
# Here second = SECOND is for regression test only.
# However, order = SIXTH is recommended.
[./Quadrature]
type = GAUSS
order = SECOND
[../]
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 10
l_tol = 1e-4
# controls for nonlinear iterations
nl_max_its = 100
nl_rel_tol = 1e-12 #11
nl_abs_tol = 1e-12 #12
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
dtmin = 1.0
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Outputs]
file_base = edge_crack_2d_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/solid_mechanics/test/tests/crystal_plasticity/cp_eigenstrains/multiple_eigenstrains_test.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
type = GeneratedMesh
dim = 3
elem_type = HEX8
[]
[AuxVariables]
[temperature]
order = FIRST
family = LAGRANGE
[]
[f1_xx]
order = CONSTANT
family = MONOMIAL
[]
[f1_yy]
order = CONSTANT
family = MONOMIAL
[]
[f1_zz]
order = CONSTANT
family = MONOMIAL
[]
[f2_xx]
order = CONSTANT
family = MONOMIAL
[]
[f2_yy]
order = CONSTANT
family = MONOMIAL
[]
[f2_zz]
order = CONSTANT
family = MONOMIAL
[]
[feig_xx]
order = CONSTANT
family = MONOMIAL
[]
[feig_yy]
order = CONSTANT
family = MONOMIAL
[]
[feig_zz]
order = CONSTANT
family = MONOMIAL
[]
[]
[Physics/SolidMechanics/QuasiStatic/all]
strain = FINITE
add_variables = true
generate_output = stress_zz
[]
[AuxKernels]
[temperature]
type = FunctionAux
variable = temperature
function = '300+400*t' # temperature increases at a constant rate
execute_on = timestep_begin
[]
[f1_xx]
type = RankTwoAux
variable = f1_xx
rank_two_tensor = thermal_deformation_gradient_1
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[f1_yy]
type = RankTwoAux
variable = f1_yy
rank_two_tensor = thermal_deformation_gradient_1
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[f1_zz]
type = RankTwoAux
variable = f1_zz
rank_two_tensor = thermal_deformation_gradient_1
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[f2_xx]
type = RankTwoAux
variable = f2_xx
rank_two_tensor = thermal_deformation_gradient_2
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[f2_yy]
type = RankTwoAux
variable = f2_yy
rank_two_tensor = thermal_deformation_gradient_2
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[f2_zz]
type = RankTwoAux
variable = f2_zz
rank_two_tensor = thermal_deformation_gradient_2
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[feig_xx]
type = RankTwoAux
variable = feig_xx
rank_two_tensor = eigenstrain_deformation_gradient
index_j = 0
index_i = 0
execute_on = timestep_end
[]
[feig_yy]
type = RankTwoAux
variable = feig_yy
rank_two_tensor = eigenstrain_deformation_gradient
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[feig_zz]
type = RankTwoAux
variable = feig_zz
rank_two_tensor = eigenstrain_deformation_gradient
index_j = 2
index_i = 2
execute_on = timestep_end
[]
[]
[BCs]
[symmy]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[symmx]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[symmz]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[tdisp]
type = DirichletBC
variable = disp_z
boundary = front
value = 0
[]
[]
[Materials]
[elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '1.684e5 1.214e5 1.214e5 1.684e5 1.214e5 1.684e5 0.754e5 0.754e5 0.754e5'
fill_method = symmetric9
[]
[stress]
type = ComputeMultipleCrystalPlasticityStress
crystal_plasticity_models = 'trial_xtalpl'
eigenstrain_names = "thermal_eigenstrain_1 thermal_eigenstrain_2"
tan_mod_type = exact
maximum_substep_iteration = 5
[]
[trial_xtalpl]
type = CrystalPlasticityKalidindiUpdate
number_slip_systems = 12
slip_sys_file_name = input_slip_sys.txt
[]
[thermal_eigenstrain_1]
type = ComputeCrystalPlasticityThermalEigenstrain
eigenstrain_name = thermal_eigenstrain_1
deformation_gradient_name = thermal_deformation_gradient_1
temperature = temperature
thermal_expansion_coefficients = '1e-05 2e-05 3e-05' # thermal expansion coefficients along three directions
[]
[thermal_eigenstrain_2]
type = ComputeCrystalPlasticityThermalEigenstrain
eigenstrain_name = thermal_eigenstrain_2
deformation_gradient_name = thermal_deformation_gradient_2
temperature = temperature
thermal_expansion_coefficients = '2e-05 3e-05 4e-05' # thermal expansion coefficients along three directions
[]
[]
[Postprocessors]
[stress_zz]
type = ElementAverageValue
variable = stress_zz
[]
[f1_xx]
type = ElementAverageValue
variable = f1_xx
[]
[f1_yy]
type = ElementAverageValue
variable = f1_yy
[]
[f1_zz]
type = ElementAverageValue
variable = f1_zz
[]
[f2_xx]
type = ElementAverageValue
variable = f2_xx
[]
[f2_yy]
type = ElementAverageValue
variable = f2_yy
[]
[f2_zz]
type = ElementAverageValue
variable = f2_zz
[]
[feig_xx]
type = ElementAverageValue
variable = feig_xx
[]
[feig_yy]
type = ElementAverageValue
variable = feig_yy
[]
[feig_zz]
type = ElementAverageValue
variable = feig_zz
[]
[temperature]
type = ElementAverageValue
variable = temperature
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-10
nl_abs_step_tol = 1e-10
dt = 0.1
dtmin = 1e-4
end_time = 10
[]
[Outputs]
csv = true
[console]
type = Console
max_rows = 5
[]
[]
(modules/xfem/test/tests/nucleation_uo/nucleate_2edge_cracks_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh2'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 30
ny = 15
xmin = -2
xmax = -.2
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[dispBlock_top]
type = BoundingBoxNodeSetGenerator
new_boundary = pull_top_y
bottom_left = '-2.1 0.99 0'
top_right = '-1.9 1.01 0'
input = gen
[]
[dispBlock_bot]
type = BoundingBoxNodeSetGenerator
new_boundary = pull_bot_y
bottom_left = '-2.1 -.01 0'
top_right = '-1.9 0.01 0'
input = dispBlock_top
[]
[]
[DomainIntegral]
integrals = 'Jintegral InteractionIntegralKI InteractionIntegralKII'
displacements = 'disp_x disp_y'
crack_front_points_provider = cut_mesh2
2d=true
number_points_from_provider = 1
crack_direction_method = CurvedCrackFront
radius_inner = '0.15'
radius_outer = '0.45'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
incremental = true
used_by_xfem_to_grow_crack = true
[]
[UserObjects]
#fixme, nucleate has to be before cut_mesh2 in the input file or cut_mesh2 can't finde the nucleate_uo
[nucleate]
type = MeshCut2DRankTwoTensorNucleation
tensor = stress
scalar_type = MaxPrincipal
nucleation_threshold = nucleation_threshold
initiate_on_boundary = 'left bottom'
average = true
nucleation_length = .1
[]
[cut_mesh2]
type = MeshCut2DFractureUserObject
mesh_file = make_edge_crack_in.e
k_critical=80
growth_increment = 0.1
nucleate_uo = nucleate
[]
[]
[AuxVariables]
[nucleation_threshold]
order = CONSTANT
family = MONOMIAL
[]
[]
[ICs]
[nucleation]
type = FunctionIC
function = nucleation_x_y
variable = nucleation_threshold
[]
# [nucleation]
# type = VolumeWeightedWeibull
# variable = nucleation_threshold
# reference_volume = 0.01 #This is the volume of an element for a 100x100 mesh
# weibull_modulus = 2
# median = 5000.0
# []
[]
[Functions]
[nucleation_y]
type = ParsedFunction
expression = 'if(y>0.7,10000,if(y<0.5,10000,4000*(1-y)^2-10000))'
[]
[nucleation_x]
type = ParsedFunction
expression = 'if(x>-0.9,10000,if(x<-1.1,10000,1000*(x)^2-10000))'
[]
[nucleation_x_y]
type = LinearCombinationFunction
functions = 'nucleation_x nucleation_y'
w = '1 1'
[]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
generate_output = 'stress_xx stress_yy vonmises_stress max_principal_stress'
[../]
[]
[Functions]
[bc_pull_top]
type = ParsedFunction
expression = 'if(t<6,0.0008*t,0.0008*5+0.0004*(t-6))'
[]
[bc_pull_bot]
type = ParsedFunction
expression = 0.0004*t
[]
[]
[BCs]
[top_left]
type = FunctionDirichletBC
boundary = pull_top_y
variable = disp_y
function = bc_pull_top
[]
[bot_left]
type = FunctionDirichletBC
boundary = pull_bot_y
variable = disp_y
function = bc_pull_bot
[]
[bottom_x]
type = DirichletBC
boundary = right
variable = disp_x
value = 0.0
[]
[bottom_y]
type = DirichletBC
boundary = right
variable = disp_y
value = 0.0
[]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 55
max_xfem_update = 2
[]
[Outputs]
# csv=true
exodus = true
execute_on = TIMESTEP_END
# [xfemcutter]
# type=XFEMCutMeshOutput
# xfem_cutter_uo=cut_mesh2
# []
# console = false
[./console]
type = Console
output_linear = false
output_nonlinear = false
[../]
[]
(modules/contact/test/tests/pdass_problems/ironing_penalty.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = iron.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '10'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '20'
new_block_name = 'primary_lower'
input = secondary
[]
patch_update_strategy = auto
patch_size = 20
allow_renumbering = false
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[penalty_normal_pressure]
order = FIRST
family = LAGRANGE
[]
[penalty_frictional_pressure]
order = FIRST
family = LAGRANGE
[]
[accumulated_slip_one]
order = FIRST
family = LAGRANGE
[]
[tangential_vel_one]
order = FIRST
family = LAGRANGE
[]
[real_weighted_gap]
order = FIRST
family = LAGRANGE
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[von_mises]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 2. 8.'
y = '0. -1.0 -1.0'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 8.'
y = '0. 8.'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
block = '1 2'
strain = FINITE
[]
[]
[AuxKernels]
[penalty_normal_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_normal_pressure
user_object = friction_uo
contact_quantity = normal_pressure
[]
[penalty_frictional_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_frictional_pressure
user_object = friction_uo
contact_quantity = tangential_pressure_one
[]
[penalty_accumulated_slip_auxk]
type = PenaltyMortarUserObjectAux
variable = accumulated_slip_one
user_object = friction_uo
contact_quantity = accumulated_slip_one
[]
[penalty_tangential_vel_auxk]
type = PenaltyMortarUserObjectAux
variable = tangential_vel_one
user_object = friction_uo
contact_quantity = tangential_velocity_one
[]
[real_weighted_gap_auxk]
type = PenaltyMortarUserObjectAux
variable = real_weighted_gap
user_object = friction_uo
contact_quantity = normal_gap
[]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[von_mises_kernel]
#Calculates the von mises stress and assigns it to von_mises
type = RankTwoScalarAux
variable = von_mises
rank_two_tensor = stress
execute_on = timestep_end
scalar_type = VonMisesStress
block = '1 2'
[]
[]
[VectorPostprocessors]
[penalty_normal_pressure]
type = NodalValueSampler
variable = penalty_normal_pressure
boundary = 10
sort_by = id
[]
[]
[BCs]
[bot_x_disp]
type = DirichletBC
variable = disp_x
boundary = '40'
value = 0.0
preset = false
[]
[bot_y_disp]
type = DirichletBC
variable = disp_y
boundary = '40'
value = 0.0
preset = false
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = '30'
function = disp_ramp_vert
preset = false
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = '30'
function = disp_ramp_horz
preset = false
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 6896
poissons_ratio = 0.32
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '2'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 689.6
poissons_ratio = 0.32
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
l_tol = 1e-6
l_max_its = 50
nl_max_its = 30
start_time = 0.0
end_time = 6.5 # 6.5
dt = 0.0125
dtmin = 1e-5
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = true
[chkfile]
type = CSV
start_time = 0.0
execute_vector_postprocessors_on = FINAL
[]
[console]
type = Console
max_rows = 5
[]
[]
[Debug]
show_var_residual_norms = true
[]
[UserObjects]
[friction_uo]
type = PenaltyFrictionUserObject
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
disp_x = disp_x
disp_y = disp_y
friction_coefficient = 0.1 # with 2.0 works
secondary_variable = disp_x
penalty = 1e5
penalty_friction = 1e4
use_physical_gap = true
[]
[]
[Constraints]
[x]
type = NormalMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[t_x]
type = TangentialMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[t_y]
type = TangentialMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[]
(modules/contact/test/tests/pdass_problems/ironing_penalty_al.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = iron.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '10'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '20'
new_block_name = 'primary_lower'
input = secondary
[]
patch_update_strategy = auto
patch_size = 20
allow_renumbering = false
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[penalty_normal_pressure]
order = FIRST
family = LAGRANGE
[]
[penalty_frictional_pressure]
order = FIRST
family = LAGRANGE
[]
[accumulated_slip_one]
order = FIRST
family = LAGRANGE
[]
[tangential_vel_one]
order = FIRST
family = LAGRANGE
[]
[real_weighted_gap]
order = FIRST
family = LAGRANGE
[]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[von_mises]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 2. 8.'
y = '0. -1.0 -1.0'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 8.'
y = '0. 8.'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
block = '1 2'
strain = FINITE
[]
[]
[AuxKernels]
[penalty_normal_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_normal_pressure
user_object = friction_uo
contact_quantity = normal_pressure
[]
[penalty_frictional_pressure_auxk]
type = PenaltyMortarUserObjectAux
variable = penalty_frictional_pressure
user_object = friction_uo
contact_quantity = tangential_pressure_one
[]
[penalty_accumulated_slip_auxk]
type = PenaltyMortarUserObjectAux
variable = accumulated_slip_one
user_object = friction_uo
contact_quantity = accumulated_slip_one
[]
[penalty_tangential_vel_auxk]
type = PenaltyMortarUserObjectAux
variable = tangential_vel_one
user_object = friction_uo
contact_quantity = tangential_velocity_one
[]
[real_weighted_gap_auxk]
type = PenaltyMortarUserObjectAux
variable = real_weighted_gap
user_object = friction_uo
contact_quantity = normal_gap
[]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[von_mises_kernel]
#Calculates the von mises stress and assigns it to von_mises
type = RankTwoScalarAux
variable = von_mises
rank_two_tensor = stress
execute_on = timestep_end
scalar_type = VonMisesStress
block = '1 2'
[]
[]
# [VectorPostprocessors]
# [penalty_normal_pressure]
# type = NodalValueSampler
# variable = penalty_normal_pressure
# boundary = 10
# sort_by = id
# []
# []
[Postprocessors]
[num_nl]
type = NumNonlinearIterations
[]
[cumulative]
type = CumulativeValuePostprocessor
postprocessor = num_nl
[]
[force_x]
type = NodalSum
boundary = 30
variable = saved_x
[]
[force_y]
type = NodalSum
boundary = 30
variable = saved_y
[]
[gap]
type = SideExtremeValue
value_type = min
variable = real_weighted_gap
boundary = 10
[]
[num_al]
type = NumAugmentedLagrangeIterations
[]
[]
[BCs]
[bot_x_disp]
type = DirichletBC
variable = disp_x
boundary = '40'
value = 0.0
preset = false
[]
[bot_y_disp]
type = DirichletBC
variable = disp_y
boundary = '40'
value = 0.0
preset = false
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = '30'
function = disp_ramp_vert
preset = false
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = '30'
function = disp_ramp_horz
preset = false
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 6896
poissons_ratio = 0.32
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '2'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 689.6
poissons_ratio = 0.32
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
l_tol = 1e-6
l_max_its = 7
nl_max_its = 300
start_time = 0.0
end_time = 6.5 # 6.5
dt = 0.0125
dtmin = 1e-5
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = true
# [chkfile]
# type = CSV
# start_time = 0.0
# execute_vector_postprocessors_on = FINAL
# []
[console]
type = Console
max_rows = 5
[]
[]
[Debug]
show_var_residual_norms = true
[]
[Problem]
type = AugmentedLagrangianContactFEProblem
[]
[UserObjects]
[friction_uo]
type = PenaltyFrictionUserObject
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
disp_x = disp_x
disp_y = disp_y
friction_coefficient = 0.4 # with 2.0 works
secondary_variable = disp_x
penalty = 5e5
penalty_friction = 1e4
slip_tolerance = 1e-05
penetration_tolerance = 1e-03
[]
[]
[Constraints]
[x]
type = NormalMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[t_x]
type = TangentialMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[t_y]
type = TangentialMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[]
(modules/contact/test/tests/sliding_block/sliding/frictionless_penalty.i)
# This is a benchmark test that checks constraint based frictionless
# contact using the penalty method. In this test a constant
# displacement is applied in the horizontal direction to simulate
# a small block come sliding down a larger block.
#
# The gold file is run on one processor
# and the benchmark case is run on a minimum of 4 processors to ensure no
# parallel variability in the contact pressure and penetration results.
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./left_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
time_step_interval = 10
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = frictionless
penalty = 1e+7
formulation = penalty
normal_smoothing_distance = 0.1
[../]
[]
(modules/navier_stokes/test/tests/finite_element/pins/channel-flow/pm_friction.i)
# This test case tests the porous-medium flow pressure drop due to friction (both viscous and inertia effect)
#
# At the steady state, eps * grad_p = alpha * u + beta * u^2
# With eps = 0.4, L = 1, u = 1, alpha = 1000, beta = 100
# dp = (1000 + 100) / 0.4 = 2,750
# This can be verified by check the p_in - p_out
[GlobalParams]
gravity = '0 0 0'
order = FIRST
family = LAGRANGE
u = vel_x
v = vel_y
pressure = p
temperature = T
porosity = porosity
eos = eos
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 0.1
nx = 10
ny = 4
elem_type = QUAD4
[]
[FluidProperties]
[./eos]
type = SimpleFluidProperties
density0 = 100 # kg/m^3
thermal_expansion = 0 # K^{-1}
cp = 100
viscosity = 0.1 # Pa-s, Re=rho*u*L/mu = 100*1*0.1/0.1 = 100
[../]
[]
[Functions]
[v_in]
type = PiecewiseLinear
x = '0 1e5'
y = '1 1'
[]
[]
[Variables]
# velocity
[vel_x]
initial_condition = 1
[]
[vel_y]
initial_condition = 0
[]
# Pressure
[p]
initial_condition = 1e5
[]
[]
[AuxVariables]
[rho]
initial_condition = 100
[]
# Temperature
[T]
initial_condition = 630
[]
[porosity]
initial_condition = 0.4
[]
[]
[Materials]
[mat]
type = PINSFEMaterial
alpha = 1000
beta = 100
[]
[]
[Kernels]
[mass_time]
type = PINSFEFluidPressureTimeDerivative
variable = p
[]
[mass_space]
type = INSFEFluidMassKernel
variable = p
[]
[x_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_x
[]
[x_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_x
component = 0
[]
[y_momentum_time]
type = PINSFEFluidVelocityTimeDerivative
variable = vel_y
[]
[y_momentum_space]
type = INSFEFluidMomentumKernel
variable = vel_y
component = 1
[]
[]
[AuxKernels]
[rho_aux]
type = FluidDensityAux
variable = rho
p = p
T = T
fp = eos
[]
[]
[BCs]
# BCs for mass equation
# Inlet
[mass_inlet]
type = INSFEFluidMassBC
variable = p
boundary = 'left'
v_fn = v_in
[]
# Outlet
[./pressure_out]
type = DirichletBC
variable = p
boundary = 'right'
value = 1e5
[../]
# BCs for x-momentum equation
# Inlet
[vx_in]
type = FunctionDirichletBC
variable = vel_x
boundary = 'left'
function = v_in
[]
# Outlet (no BC is needed)
# BCs for y-momentum equation
# Both Inlet and Outlet, and Top and Bottom
[vy]
type = DirichletBC
variable = vel_y
boundary = 'left right bottom top'
value = 0
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
solve_type = 'PJFNK'
[]
[]
[Postprocessors]
[p_in]
type = SideAverageValue
variable = p
boundary = left
[]
[p_out]
type = SideAverageValue
variable = p
boundary = right
[]
[]
[Executioner]
type = Transient
dt = 0.1
dtmin = 1.e-3
petsc_options_iname = '-pc_type -ksp_gmres_restart'
petsc_options_value = 'lu 100'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
nl_max_its = 20
l_tol = 1e-5
l_max_its = 100
start_time = 0.0
end_time = 0.5
num_steps = 10
[]
[Outputs]
perf_graph = true
print_linear_residuals = false
time_step_interval = 1
execute_on = 'initial timestep_end'
[console]
type = Console
output_linear = false
[]
[out]
type = Exodus
use_displaced = false
[]
[]
(test/tests/outputs/format/pps_screen_out_warn.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
active = 'u'
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
active = 'diff'
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
active = 'left right'
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Postprocessors]
[./avg_block]
type = ElementAverageValue
variable = u
outputs = 'console'
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
execute_on = 'timestep_end'
[./console]
type = Console
execute_postprocessors_on = none
[../]
[]
(modules/contact/test/tests/mechanical_constraint/glued_penalty.i)
[Mesh]
file = blocks_2d_nogap.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
#Initial gap is 0.01
value = -0.01
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e7
poissons_ratio = 0.3
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.10
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = glued
formulation = penalty
penalty = 1e+7
[../]
[]
(modules/porous_flow/test/tests/dirackernels/squarepulse1.i)
# Test PorousFlowSquarePulsePointSource DiracKernel
[Mesh]
type = GeneratedMesh
dim = 2
bias_x = 1.1
bias_y = 1.1
ymax = 1
xmax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
[]
[Variables]
[pp]
[]
[]
[Kernels]
[mass0]
type = PorousFlowMassTimeDerivative
fluid_component = 0
variable = pp
[]
[]
[UserObjects]
[dictator]
type = PorousFlowDictator
porous_flow_vars = pp
number_fluid_phases = 1
number_fluid_components = 1
[]
[pc]
type = PorousFlowCapillaryPressureVG
m = 0.5
alpha = 1e-7
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 2e9
density0 = 1000
thermal_expansion = 0
[]
[]
[Materials]
[temperature]
type = PorousFlowTemperature
[]
[ppss]
type = PorousFlow1PhaseP
porepressure = pp
capillary_pressure = pc
[]
[massfrac]
type = PorousFlowMassFraction
[]
[simple_fluid]
type = PorousFlowSingleComponentFluid
fp = simple_fluid
phase = 0
[]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.2
[]
[]
[Postprocessors]
[total_mass]
type = PorousFlowFluidMass
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = Newton
nl_abs_tol = 1e-14
dt = 200
end_time = 2000
[]
[Outputs]
perf_graph = true
file_base = squarepulse1
csv = true
execute_on = 'initial timestep_end'
[con]
output_linear = true
type = Console
[]
[]
[ICs]
[PressureIC]
variable = pp
type = ConstantIC
value = 20e6
[]
[]
[DiracKernels]
[sink1]
type = PorousFlowSquarePulsePointSource
start_time = 100
end_time = 300
point = '0.5 0.5 0'
mass_flux = -0.1
variable = pp
[]
[sink]
type = PorousFlowSquarePulsePointSource
start_time = 600
end_time = 1400
point = '0.5 0.5 0'
mass_flux = -0.1
variable = pp
[]
[source]
point = '0.5 0.5 0'
start_time = 1500
mass_flux = 0.2
end_time = 2000
variable = pp
type = PorousFlowSquarePulsePointSource
[]
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_force_step.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
order = FIRST
family = LAGRANGE
block = 1
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
data_file = blip.csv
format = columns
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 300.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
eigenstrain_names = thermal_expansion
add_variables = true
generate_output = 'vonmises_stress'
temperature = temp
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
start_time = 0.0
num_steps = 50000
end_time = 5.1e3
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e20
force_step_every_function_point = true
dt = 1e2
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[]
(test/tests/problems/eigen_problem/eigensolvers/ipm.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 100
ymin = 0
ymax = 100
elem_type = QUAD4
nx = 8
ny = 8
uniform_refine = 0
displacements = 'x_disp y_disp'
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./x_disp]
[../]
[./y_disp]
[../]
[]
[AuxKernels]
[./x_disp]
type = FunctionAux
variable = x_disp
function = x_disp_func
[../]
[./y_disp]
type = FunctionAux
variable = y_disp
function = y_disp_func
[../]
[]
[Functions]
[./x_disp_func]
type = ParsedFunction
expression = 0
[../]
[./y_disp_func]
type = ParsedFunction
expression = 0
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
use_displaced_mesh = true
[../]
[./rea]
type = CoefReaction
variable = u
coefficient = 2.0
use_displaced_mesh = true
[../]
[]
[BCs]
[./homogeneous]
type = DirichletBC
variable = u
boundary = '0 1 2 3'
value = 0
use_displaced_mesh = true
[../]
[]
[Executioner]
type = Eigenvalue
which_eigen_pairs = largest_magnitude
eigen_problem_type = NON_HERMITIAN
n_eigen_pairs = 5
n_basis_vectors = 15
solve_type = krylovschur
petsc_options = '-eps_view'
[]
[VectorPostprocessors]
[./eigenvalues]
type = Eigenvalues
execute_on = 'timestep_end'
[../]
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[./console]
type = Console
outlier_variable_norms = false
[../]
[]
(modules/contact/test/tests/frictional/sliding_elastic_blocks_2d/sliding_elastic_blocks_2d.i)
[Mesh]
file = sliding_elastic_blocks_2d.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
diag_save_in = 'diag_saved_x diag_saved_y'
[../]
[]
[AuxKernels]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip]
type = PenetrationAux
variable = accum_slip
execute_on = timestep_end
quantity = accumulated_slip
boundary = 3
paired_boundary = 2
[../]
[./tangential_force_x]
type = PenetrationAux
variable = tang_force_x
execute_on = timestep_end
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tangential_force_y]
type = PenetrationAux
variable = tang_force_y
execute_on = timestep_end
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.005
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e7
poissons_ratio = 0.3
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.05
num_steps = 1000
nl_rel_tol = 1e-16
nl_abs_tol = 1e-09
dtmin = 0.01
l_tol = 1e-3
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
file_base = sliding_elastic_blocks_2d_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = coulomb
friction_coefficient = '0.25'
penalty = 1e6
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
secondary = 3
primary = 2
[../]
[]
(modules/contact/test/tests/verification/hertz_cyl/quart_symm_q4/hertz_cyl_qsym_1deg_template1.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_qsym_1deg_q4.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_zero]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0.0 0.0'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 4
paired_boundary = 3
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./disp_x281]
type = NodalVariableValue
nodeid = 280
variable = disp_x
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2 3'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = disp_ramp_vert
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-6
nl_rel_tol = 1e-5
l_max_its = 50
nl_max_its = 100
start_time = 0.0
dt = 0.1
dtmin = 0.1
num_steps = 10
end_time = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '4'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x281 top_react_x top_react_y x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 3
secondary = 4
model = glued
formulation = kinematic
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/solid_mechanics/examples/coal_mining/cosserat_mc_wp_sticky_longitudinal.i)
# Strata deformation and fracturing around a coal mine
#
# A 2D geometry is used that simulates a longitudinal section of
# the coal mine. The model is actually 3D, but the "x"
# dimension is only 10m long, meshed with 1 element, and
# there is no "x" displacement. The mine is 400m deep
# and just the roof is studied (0<=z<=400). The model sits
# between -300<=y<=1800. The excavation sits in 0<=y<=1500. The
# excavation height is 3m (ie, the excavation lies within
# 0<=z<=3).
#
# Time is meaningless in this example
# as quasi-static solutions are sought at each timestep, but
# the number of timesteps controls the resolution of the
# process.
#
# The boundary conditions for this elastic simulation are:
# - disp_x = 0 everywhere
# - disp_y = 0 at y=-300 and y=1800
# - disp_z = 0 at z=0, but there is a time-dependent
# Young's modulus that simulates excavation
# - wc_x = 0 at y=300 and y=1800.
# That is, rollers on the sides, free at top,
# and prescribed at bottom in the unexcavated portion.
#
# The small strain formulation is used.
#
# All stresses are measured in MPa. The initial stress is consistent with
# the weight force from density 2500 kg/m^3, ie, stress_zz = -0.025*(300-z) MPa
# where gravity = 10 m.s^-2 = 1E-5 MPa m^2/kg. The maximum and minimum
# principal horizontal stresses are assumed to be equal to 0.8*stress_zz.
#
# Material properties:
# Young's modulus = 8 GPa
# Poisson's ratio = 0.25
# Cosserat layer thickness = 1 m
# Cosserat-joint normal stiffness = large
# Cosserat-joint shear stiffness = 1 GPa
# MC cohesion = 3 MPa
# MC friction angle = 37 deg
# MC dilation angle = 8 deg
# MC tensile strength = 1 MPa
# MC compressive strength = 100 MPa
#
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 3
nx = 1
xmin = -5
xmax = 5
nz = 40
zmin = 0
zmax = 400
bias_z = 1.1
ny = 140 # 15m elements
ymin = -300
ymax = 1800
[]
[left]
type = SideSetsAroundSubdomainGenerator
block = 0
new_boundary = 11
normal = '0 -1 0'
input = generated_mesh
[]
[right]
type = SideSetsAroundSubdomainGenerator
block = 0
new_boundary = 12
normal = '0 1 0'
input = left
[]
[front]
type = SideSetsAroundSubdomainGenerator
block = 0
new_boundary = 13
normal = '-1 0 0'
input = right
[]
[back]
type = SideSetsAroundSubdomainGenerator
block = 0
new_boundary = 14
normal = '1 0 0'
input = front
[]
[top]
type = SideSetsAroundSubdomainGenerator
block = 0
new_boundary = 15
normal = '0 0 1'
input = back
[]
[bottom]
type = SideSetsAroundSubdomainGenerator
block = 0
new_boundary = 16
normal = '0 0 -1'
input = top
[]
[excav]
type = SubdomainBoundingBoxGenerator
block_id = 1
bottom_left = '-5 0 0'
top_right = '5 1500 3'
input = bottom
[]
[roof]
type = SideSetsAroundSubdomainGenerator
block = 1
new_boundary = 18
normal = '0 0 1'
input = excav
[]
[]
[GlobalParams]
perform_finite_strain_rotations = false
displacements = 'disp_x disp_y disp_z'
Cosserat_rotations = 'wc_x wc_y wc_z'
[]
[Variables]
[./disp_y]
[../]
[./disp_z]
[../]
[./wc_x]
[../]
[]
[Kernels]
[./cy_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_y
component = 1
[../]
[./cz_elastic]
type = CosseratStressDivergenceTensors
use_displaced_mesh = false
variable = disp_z
component = 2
[../]
[./x_couple]
type = StressDivergenceTensors
use_displaced_mesh = false
variable = wc_x
displacements = 'wc_x wc_y wc_z'
component = 0
base_name = couple
[../]
[./x_moment]
type = MomentBalancing
use_displaced_mesh = false
variable = wc_x
component = 0
[../]
[./gravity]
type = Gravity
use_displaced_mesh = false
variable = disp_z
value = -10E-6 # remember this is in MPa
[../]
[]
[AuxVariables]
[./disp_x]
[../]
[./wc_y]
[../]
[./wc_z]
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./wp_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_shear_f]
order = CONSTANT
family = MONOMIAL
[../]
[./mc_tensile_f]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
[../]
[./stress_xz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xz
index_i = 0
index_j = 2
[../]
[./stress_yx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yx
index_i = 1
index_j = 0
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
[../]
[./stress_yz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yz
index_i = 1
index_j = 2
[../]
[./stress_zx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zx
index_i = 2
index_j = 0
[../]
[./stress_zy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zy
index_i = 2
index_j = 1
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
[../]
[./mc_shear]
type = MaterialStdVectorAux
index = 0
property = mc_plastic_internal_parameter
variable = mc_shear
[../]
[./mc_tensile]
type = MaterialStdVectorAux
index = 1
property = mc_plastic_internal_parameter
variable = mc_tensile
[../]
[./wp_shear]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_internal_parameter
variable = wp_shear
[../]
[./wp_tensile]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_internal_parameter
variable = wp_tensile
[../]
[./mc_shear_f]
type = MaterialStdVectorAux
index = 6
property = mc_plastic_yield_function
variable = mc_shear_f
[../]
[./mc_tensile_f]
type = MaterialStdVectorAux
index = 0
property = mc_plastic_yield_function
variable = mc_tensile_f
[../]
[./wp_shear_f]
type = MaterialStdVectorAux
index = 0
property = wp_plastic_yield_function
variable = wp_shear_f
[../]
[./wp_tensile_f]
type = MaterialStdVectorAux
index = 1
property = wp_plastic_yield_function
variable = wp_tensile_f
[../]
[]
[BCs]
[./no_y]
type = DirichletBC
variable = disp_y
boundary = '11 12'
value = 0.0
[../]
[./no_z]
type = DirichletBC
variable = disp_z
boundary = '16'
value = 0.0
[../]
[./no_wc_x]
type = DirichletBC
variable = wc_x
boundary = '11 12'
value = 0.0
[../]
[./roof]
type = StickyBC
variable = disp_z
min_value = -3.0
boundary = '18'
[../]
[]
[Functions]
[./ini_xx]
type = ParsedFunction
expression = '-0.8*2500*10E-6*(400-z)'
[../]
[./ini_zz]
type = ParsedFunction
expression = '-2500*10E-6*(400-z)'
[../]
[./excav_sideways]
type = ParsedFunction
symbol_names = 'end_t ymin ymax minval maxval slope'
symbol_values = '1.0 0 1500.0 1E-9 1 15'
# excavation face at ymin+(ymax-ymin)*min(t/end_t,1)
# slope is the distance over which the modulus reduces from maxval to minval
expression = 'if(y<ymin+(ymax-ymin)*min(t/end_t,1),minval,if(y<ymin+(ymax-ymin)*min(t/end_t,1)+slope,minval+(maxval-minval)*(y-(ymin+(ymax-ymin)*min(t/end_t,1)))/slope,maxval))'
[../]
[./density_sideways]
type = ParsedFunction
symbol_names = 'end_t ymin ymax minval maxval'
symbol_values = '1.0 0 1500.0 0 2500'
expression = 'if(y<ymin+(ymax-ymin)*min(t/end_t,1),minval,maxval)'
[../]
[]
[UserObjects]
[./mc_coh_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 2.99 # MPa
value_residual = 3.01 # MPa
rate = 1.0
[../]
[./mc_fric]
type = SolidMechanicsHardeningConstant
value = 0.65 # 37deg
[../]
[./mc_dil]
type = SolidMechanicsHardeningConstant
value = 0.15 # 8deg
[../]
[./mc_tensile_str_strong_harden]
type = SolidMechanicsHardeningExponential
value_0 = 1.0 # MPa
value_residual = 1.0 # MPa
rate = 1.0
[../]
[./mc_compressive_str]
type = SolidMechanicsHardeningCubic
value_0 = 100 # Large!
value_residual = 100
internal_limit = 0.1
[../]
[./wp_coh_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_tan_fric]
type = SolidMechanicsHardeningConstant
value = 0.36 # 20deg
[../]
[./wp_tan_dil]
type = SolidMechanicsHardeningConstant
value = 0.18 # 10deg
[../]
[./wp_tensile_str_harden]
type = SolidMechanicsHardeningCubic
value_0 = 0.1
value_residual = 0.1
internal_limit = 10
[../]
[./wp_compressive_str_soften]
type = SolidMechanicsHardeningCubic
value_0 = 100
value_residual = 1.0
internal_limit = 1.0
[../]
[]
[Materials]
[./elasticity_tensor_0]
type = ComputeLayeredCosseratElasticityTensor
block = 0
young = 8E3 # MPa
poisson = 0.25
layer_thickness = 1.0
joint_normal_stiffness = 1E9 # huge
joint_shear_stiffness = 1E3 # MPa
[../]
[./elasticity_tensor_1]
type = ComputeLayeredCosseratElasticityTensor
block = 1
young = 8E3 # MPa
poisson = 0.25
layer_thickness = 1.0
joint_normal_stiffness = 1E9 # huge
joint_shear_stiffness = 1E3 # MPa
elasticity_tensor_prefactor = excav_sideways
[../]
[./strain]
type = ComputeCosseratIncrementalSmallStrain
eigenstrain_names = ini_stress
[../]
[./ini_stress]
type = ComputeEigenstrainFromInitialStress
eigenstrain_name = ini_stress
initial_stress = 'ini_xx 0 0 0 ini_xx 0 0 0 ini_zz'
[../]
[./stress_0]
type = ComputeMultipleInelasticCosseratStress
block = 0
inelastic_models = 'mc wp'
cycle_models = true
relative_tolerance = 2.0
absolute_tolerance = 1E6
max_iterations = 1
tangent_operator = nonlinear
perform_finite_strain_rotations = false
[../]
[./stress_1]
# this is needed so as to correctly apply the initial stress
type = ComputeMultipleInelasticCosseratStress
block = 1
inelastic_models = ''
relative_tolerance = 2.0
absolute_tolerance = 1E6
max_iterations = 1
tangent_operator = nonlinear
perform_finite_strain_rotations = false
[../]
[./mc]
type = CappedMohrCoulombCosseratStressUpdate
warn_about_precision_loss = false
host_youngs_modulus = 8E3
host_poissons_ratio = 0.25
base_name = mc
tensile_strength = mc_tensile_str_strong_harden
compressive_strength = mc_compressive_str
cohesion = mc_coh_strong_harden
friction_angle = mc_fric
dilation_angle = mc_dil
max_NR_iterations = 100000
smoothing_tol = 0.1 # MPa # Must be linked to cohesion
yield_function_tol = 1E-9 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0
[../]
[./wp]
type = CappedWeakPlaneCosseratStressUpdate
warn_about_precision_loss = false
base_name = wp
cohesion = wp_coh_harden
tan_friction_angle = wp_tan_fric
tan_dilation_angle = wp_tan_dil
tensile_strength = wp_tensile_str_harden
compressive_strength = wp_compressive_str_soften
max_NR_iterations = 10000
tip_smoother = 0.1
smoothing_tol = 0.1 # MPa # Note, this must be tied to cohesion, otherwise get no possible return at cone apex
yield_function_tol = 1E-11 # MPa. this is essentially the lowest possible without lots of precision loss
perfect_guess = true
min_step_size = 1.0E-3
[../]
[./density_0]
type = GenericConstantMaterial
block = 0
prop_names = density
prop_values = 2500
[../]
[./density_1]
type = GenericFunctionMaterial
block = 1
prop_names = density
prop_values = density_sideways
[../]
[]
[Postprocessors]
[./subs]
type = PointValue
point = '0 0 400'
variable = disp_z
use_displaced_mesh = false
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 2 lu gmres 200'
line_search = bt
nl_abs_tol = 1e-3
nl_rel_tol = 1e-5
l_max_its = 30
nl_max_its = 100
start_time = 0.0
dt = 0.01 # 1 element per step
end_time = 1.0
[]
[Outputs]
file_base = cosserat_mc_wp_sticky_longitudinal
time_step_interval = 1
print_linear_residuals = false
exodus = true
csv = true
console = true
#[./console]
# type = Console
# output_linear = false
#[../]
[]
(modules/xfem/test/tests/moving_interface/verification/2D_rz_lsdep1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: 2D
# Coordinate System: rz
# Material Numbers/Types: level set dep 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# Transient 2D heat transfer problem in cylindrical coordinates designed with
# the Method of Manufactured Solutions. This problem was developed to verify
# XFEM performance on linear elements in the presence of a moving interface
# sweeping across the x-y coordinates of a system with thermal conductivity
# dependent upon the transient level set function. This problem can be
# exactly evaluated by FEM/Moose without the moving interface. Both the
# temperature and level set function are designed to be linear to attempt to
# minimize the error between the Moose/exact solution and XFEM results.
# Results:
# The temperature at the bottom left boundary (x=1, y=1) exhibits the largest
# difference between the FEM/Moose solution and XFEM results. We present the
# XFEM results at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 479.9998717
# 0.6 520 519.9994963
# 0.8 560 559.9989217
# 1.0 600 599.9986735
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 4
xmin = 1.0
xmax = 2.0
ymin = 1.0
ymax = 2.0
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-100*x-100*y+400) + t*(-2.5*y/(2.04*x) + 155/x - t/(2.04*x)
- 7.5/2.04)'
[../]
[./neumann_func]
type = ParsedFunction
expression = '((0.01/2.04)*(-2.5*x-2.5*y-t)+1.55)*100*t'
[../]
[./dirichlet_right_func]
type = ParsedFunction
expression = '(-100*y+200)*t+400'
[../]
[./dirichlet_top_func]
type = ParsedFunction
expression = '(-100*x+200)*t+400'
[../]
[./k_func]
type = ParsedFunction
expression = '(0.01/2.04)*(-2.5*x-2.5*y-t) + 1.55'
[../]
[./ls_func]
type = ParsedFunction
expression = '-0.5*(x+y) + 2.04 -0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericFunctionMaterial
prop_names = 'diffusion_coefficient'
prop_values = 'k_func'
[../]
[]
[BCs]
[./left_du]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = FunctionDirichletBC
variable = u
boundary = 'right'
function = dirichlet_right_func
[../]
[./bottom_du]
type = FunctionNeumannBC
variable = u
boundary = 'bottom'
function = neumann_func
[../]
[./top_u]
type = FunctionDirichletBC
variable = u
boundary = 'top'
function = dirichlet_top_func
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/time_integrators/explicit-euler/ee-1d-quadratic.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 20
elem_type = EDGE3
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = x*x-2*t
[../]
[./exact_fn]
type = ParsedFunction
expression = t*x*x
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
# lumping = true
implicit = true
[../]
[./diff]
type = Diffusion
variable = u
implicit = false
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
implicit = false
[../]
[]
[BCs]
active = 'all'
[./all]
type = FunctionDirichletBC
variable = u
boundary = '0 1'
function = exact_fn
implicit = true
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
scheme = 'explicit-euler'
solve_type = 'LINEAR'
l_tol = 1e-12
start_time = 0.0
num_steps = 20
dt = 0.00005
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/optimization/test/tests/executioners/transient_and_adjoint/nonlinear_diffusivity.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmax = 1
ymax = 1
nx = 10
ny = 10
[]
[]
[Problem]
nl_sys_names = 'nl0 adjoint'
[]
[Variables]
[u]
[]
[u_adjoint]
solver_sys = adjoint
[]
[]
[Kernels]
[time]
type = TimeDerivative
variable = u
[]
[diff]
type = ADMatDiffusion
variable = u
diffusivity = D
[]
[src]
type = ADBodyForce
variable = u
value = 1
[]
[src_adjoint]
type = ADBodyForce
variable = u_adjoint
value = 1
[]
[]
[BCs]
[dirichlet]
type = ADDirichletBC
variable = u
boundary = 'top right'
value = 0
[]
[]
[Materials]
[diffc]
type = ADParsedMaterial
property_name = D
expression = '0.1 + 5 * u'
coupled_variables = 'u'
[]
[]
[Postprocessors]
[u_avg]
type = ElementAverageValue
variable = u
execute_on = 'TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[u_adjoint_avg]
type = ElementAverageValue
variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[inner_product]
type = VariableInnerProduct
variable = u
second_variable = u_adjoint
execute_on = ADJOINT_TIMESTEP_END
[]
[]
[Executioner]
type = TransientAndAdjoint
forward_system = nl0
adjoint_system = adjoint
dt = 0.2
num_steps = 5
nl_rel_tol = 1e-12
l_tol = 1e-12
[]
[Outputs]
[forward]
type = CSV
[]
[adjoint]
type = CSV
execute_on = 'INITIAL ADJOINT_TIMESTEP_END'
[]
[console]
type = Console
execute_postprocessors_on = 'INITIAL TIMESTEP_END ADJOINT_TIMESTEP_END'
[]
[]
(modules/xfem/test/tests/bimaterials/inclusion_bimaterials_2d.i)
# This test is for a matrix-inclusion composite materials
# The global stress is determined by switching the stress based on level set values
# The inclusion geometry is marked by a level set function
# The matrix and inclusion are glued together
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 11
ny = 11
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'sqrt((y-2.5)*(y-2.5) + (x-2.5)*(x-2.5)) - 1.5'
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./a_strain_xx]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
boundary = top
variable = disp_x
function = '0.03*t'
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ComputeSmallStrain
base_name = A
[../]
[./stress_A]
type = ComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e5
poissons_ratio = 0.3
[../]
[./strain_B]
type = ComputeSmallStrain
base_name = B
[../]
[./stress_B]
type = ComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = LevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[./combined_dstressdstrain]
type = LevelSetBiMaterialRankFour
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = Jacobian_mult
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-7
# time control
start_time = 0.0
dt = 0.5
end_time = 1.0
num_steps = 2
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(modules/richards/test/tests/pressure_pulse/pp_fu_lumped_22.i)
# investigating pressure pulse in 1D with 2 phase
# transient
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
xmin = 0
xmax = 100
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E9
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-5
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 3
[../]
[./SatWater]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SatGas]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E3
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./water_ic]
type = ConstantIC
value = 2E6
variable = pwater
[../]
[./gas_ic]
type = ConstantIC
value = 2E6
variable = pgas
[../]
[]
[BCs]
[./left]
type = DirichletBC
boundary = left
value = 3E6
variable = pwater
[../]
[./left_gas]
type = DirichletBC
boundary = left
value = 3E6
variable = pgas
[../]
[]
[AuxVariables]
[./Seff1VG_Aux]
[../]
[]
[Kernels]
active = 'richardsfwater richardstwater richardsfgas richardstgas pconstraint'
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[./pconstraint]
type = RichardsPPenalty
variable = pgas
a = 1E-8
lower_var = pwater
[../]
[]
[AuxKernels]
[./Seff1VG_AuxK]
type = RichardsSeffAux
variable = Seff1VG_Aux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.1
mat_permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
viscosity = '1E-3 1E-5'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
[./andy]
type = SMP
full = true
petsc_options = '-snes_monitor -snes_linesearch_monitor'
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E3
dtmin = 1E3
end_time = 1E4
l_tol = 1.e-4
nl_rel_tol = 1.e-7
nl_max_its = 10
l_max_its = 20
line_search = 'none'
[]
[Outputs]
file_base = pp_fu_lumped_22
execute_on = 'initial timestep_end final'
time_step_interval = 10000
exodus = true
[./console]
type = Console
time_step_interval = 1
[../]
[]
(modules/xfem/test/tests/pressure_bc/edge_3d_pressure.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = false
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 9
nz = 10
xmin = -0.1
xmax = 0.1
ymin = -0.5
ymax = 0.5
zmin = -0.5
zmax = 0.5
elem_type = HEX8
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = '-0.2 0.0 -0.5
-0.2 0.0 0.0
0.2 0.0 0.0
0.2 0.0 -0.5'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 2.0 4.0 6.0 8.0'
y = '0 1000 0 1000 0'
[../]
[]
[DiracKernels]
[./p_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
[../]
[./p_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
[../]
[./p_z]
type = XFEMPressure
variable = disp_z
component = 2
function = pressure
[../]
[]
[BCs]
[./bottom_x]
type = DirichletBC
boundary = 'bottom top'
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = 'bottom top'
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = 'bottom top'
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-12
# time control
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
file_base = edge_3d_pressure_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/cyl_1/cyl1_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = cyl1_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = cyl1_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = cyl1_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/contact/test/tests/verification/patch_tests/brick_2/brick2_aug.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick2_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 100
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_x26]
type = NodalVariableValue
nodeid = 25
variable = disp_x
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_y26]
type = NodalVariableValue
nodeid = 25
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x7 disp_y7 disp_x26 disp_y26 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
tangential_tolerance = 1e-3
formulation = augmented_lagrange
normalize_penalty = true
penalty = 1e8
model = frictionless
al_penetration_tolerance = 1e-8
[../]
[]
(modules/xfem/test/tests/single_var_constraint_3d/stationary_jump_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.25
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.5 -0.001 -0.001
0.5 1.001 -0.001
0.5 1.001 1.001
0.5 -0.001 1.001'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0.5
jump_flux = 0
geometric_cut_userobject = 'square_planar_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/thermal_hydraulics/test/tests/base/simulation/loop_identification.i)
# This test tests the loop identification function, which creates a map of component
# names to a loop name. "Loops" are defined to be sets of components which are
# physically connected - heat exchanger connections do not constitute physical
# connections in this sense. Note that this test is not meant to actually perform
# any physical computations, so dummy values are provided for the required parameters.
#
# The test configuration for this test is the following:
#
# pipe1 -> corechannel:pipe -> pipe2 -> hx:primary -> pipe1
# j1 j2 j3 j4
#
# inlet -> hx:secondary -> outlet
#
# This test uses the command-line option "--print-component-loops" to print out
# the lists of components in each loop, with the desired output being the
# following:
#
# Loop 1:
#
# corechannel:pipe
# hx:primary
# j1
# j2
# j3
# j4
# pipe1
# pipe2
#
# Loop 2:
#
# hx:secondary
# inlet
# outlet
[GlobalParams]
closures = simple_closures
initial_p = 1e6
initial_T = 300
initial_vel = 0
[]
[FluidProperties]
[fp_liquid]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[SolidProperties]
[hx:wall]
type = ThermalFunctionSolidProperties
k = 1
cp = 1
rho = 1
[]
[]
[Components]
# PRIMARY LOOP
[pipe1]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 1
A = 1
f = 1
fp = fp_liquid
[]
[j1]
type = JunctionOneToOne1Phase
connections = 'pipe1:out corechannel:in'
[]
[corechannel]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 1
A = 1
f = 1
fp = fp_liquid
[]
[j2]
type = JunctionOneToOne1Phase
connections = 'corechannel:out pipe2:in'
[]
[pipe2]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 1
A = 1
f = 1
fp = fp_liquid
[]
[j3]
type = JunctionOneToOne1Phase
connections = 'pipe2:out hx:primary:in'
[]
[hx:primary]
type = FlowChannel1Phase
position = '0 1 0'
orientation = '1 0 0'
length = 1
n_elems = 1
A = 1
f = 1
fp = fp_liquid
[]
[j4]
type = JunctionOneToOne1Phase
connections = 'hx:primary:out pipe1:in'
[]
# HEAT EXCHANGER
[hs]
type = HeatStructurePlate
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 1
solid_properties = hx:wall
solid_properties_T_ref = '300'
n_part_elems = 1
names = 0
widths = 1
depth = 1
initial_T = 300
[]
[ht_primary]
type = HeatTransferFromHeatStructure1Phase
hs = hs
flow_channel = hx:primary
hs_side = outer
Hw = 0
[]
[ht_secondary]
type = HeatTransferFromHeatStructure1Phase
hs = hs
flow_channel = hx:secondary
hs_side = inner
Hw = 0
[]
# SECONDARY LOOP
[inlet]
type = SolidWall1Phase
input = 'hx:secondary:out'
[]
[hx:secondary]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 1
A = 1
f = 1
fp = fp_liquid
[]
[outlet]
type = SolidWall1Phase
input = 'hx:secondary:in'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Transient
num_steps = 1
[]
[Outputs]
[console]
type = Console
system_info = ''
enable = false
[]
[]
(modules/thermal_hydraulics/test/tests/misc/adapt/single_block.i)
[GlobalParams]
gravity_vector = '0 0 0'
initial_p = 1e5
initial_T = 300
initial_vel = 0
closures = simple_closures
[]
[FluidProperties]
[eos]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
# geometry
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 20
A = 1.0000000000e-04
D_h = 1.1283791671e-02
f = 0.
fp = eos
[]
[inlet]
type = InletDensityVelocity1Phase
input = 'pipe1:in'
rho = 996.561962436227759
vel = 1
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 1e5
[]
[]
[Outputs]
exodus = true
show = 'rhoA rhouA rhoEA'
[console]
type = Console
print_mesh_changed_info = true
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0.0
dt = 1e-5
num_steps = 5
abort_on_solve_fail = true
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-9
nl_abs_tol = 1e-8
nl_max_its = 10
l_tol = 1e-3
l_max_its = 100
petsc_options_iname = '-pc_type'
petsc_options_value = ' lu'
[Adaptivity]
initial_adaptivity = 0 # There seems to be a bug with non-zero initial adaptivity
refine_fraction = 0.60
coarsen_fraction = 0.30
max_h_level = 4
[]
[]
(modules/xfem/test/tests/solid_mechanics_basic/edge_crack_3d_fatigue.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX8
[]
[UserObjects]
[./cut_mesh]
type = CrackMeshCut3DUserObject
mesh_file = mesh_edge_crack.xda
growth_dir_method = FUNCTION
size_control = 1
n_step_growth = 1
growth_rate_method = FATIGUE
growth_direction_x = growth_func_x
growth_direction_y = growth_func_y
growth_direction_z = growth_func_z
growth_rate = growth_func_v
crack_front_nodes = '7 6 5 4'
[../]
[]
[Functions]
[./growth_func_x]
type = ParsedFunction
expression = 1
[../]
[./growth_func_y]
type = ParsedFunction
expression = 0
[../]
[./growth_func_z]
type = ParsedFunction
expression = 0
[../]
[./growth_func_v]
type = ParsedFunction
symbol_names = 'dN'
symbol_values = 'fatigue'
expression = dN
[../]
[]
[Postprocessors]
[./fatigue]
type = ParisLaw
max_growth_size = 0.1
paris_law_c = 1e-13
paris_law_m = 2.5
[../]
[]
[DomainIntegral]
integrals = 'Jintegral InteractionIntegralKI InteractionIntegralKII'
displacements = 'disp_x disp_y disp_z'
crack_front_points_provider = cut_mesh
number_points_from_provider = 4
crack_direction_method = CurvedCrackFront
radius_inner = '0.15'
radius_outer = '0.45'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
incremental = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[Functions]
[./top_trac_y]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_y]
type = FunctionNeumannBC
boundary = top
variable = disp_y
function = top_trac_y
[../]
[./bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 4.0
max_xfem_update = 1
[]
[Outputs]
file_base = edge_crack_3d_fatigue_out
execute_on = 'timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q8/hertz_cyl_half_1deg_template3.i)
[GlobalParams]
order = SECOND
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x639]
type = NodalVariableValue
nodeid = 638
variable = disp_x
[../]
[./disp_y639]
type = NodalVariableValue
nodeid = 638
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 2.0
l_tol = 5e-4
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x639 disp_y639 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = 0.0
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/contact/test/tests/verification/patch_tests/ring_2/ring2_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring2_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = ring2_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = ring2_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/porous_flow/test/tests/sinks/s13.i)
# Apply a PorousFlowOutflowBC to the right-hand side and watch fluid flow to it
#
# This test has a single phase with two components. The test initialises with
# the porous material fully filled with component=1. The left-hand side is fixed
# at porepressure=1 and mass-fraction of the zeroth component being unity.
# The right-hand side has
# - porepressure fixed at zero via a DirichletBC: physically this removes component=1
# to ensure that porepressure remains fixed
# - a PorousFlowOutflowBC for the component=0 to allow that component to exit the boundary freely
#
# Therefore, the zeroth fluid component will flow from left to right (down the
# pressure gradient).
#
# The important DE is
# porosity * dc/dt = (perm / visc) * grad(P) * grad(c)
# which is true for c = mass-fraction, and very large bulk modulus of the fluid.
# For grad(P) constant in time and space (as in this example) this is just the
# advection equation for c, with velocity = perm / visc / porosity. The parameters
# are chosen to velocity = 1 m/s.
# In the numerical world, and especially with full upwinding, the advection equation
# suffers from diffusion. In this example, the diffusion is obvious when plotting
# the mass-fraction along the line, but the average velocity of the front is still
# correct at 1 m/s.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 100
xmin = 0
xmax = 1
[]
[GlobalParams]
PorousFlowDictator = dictator
gravity = '0 0 0'
[]
[Variables]
[pp]
[]
[frac]
[]
[]
[PorousFlowFullySaturated]
fp = simple_fluid
porepressure = pp
mass_fraction_vars = frac
[]
[ICs]
[pp]
type = FunctionIC
variable = pp
function = 1-x
[]
[]
[FluidProperties]
[simple_fluid]
type = SimpleFluidProperties
bulk_modulus = 1e10 # need large in order for constant-velocity advection
density0 = 1 # irrelevant
thermal_expansion = 0
viscosity = 11
[]
[]
[Materials]
[porosity]
type = PorousFlowPorosityConst
porosity = 0.1
[]
[permeability]
type = PorousFlowPermeabilityConst
permeability = '1.1 0 0 0 1.1 0 0 0 1.1'
[]
[]
[BCs]
[lhs_fixed_b]
type = DirichletBC
boundary = left
variable = pp
value = 1
[]
[rhs_fixed_b]
type = DirichletBC
boundary = right
variable = pp
value = 0
[]
[lhs_fixed_a]
type = DirichletBC
boundary = left
variable = frac
value = 1
[]
[outflow_a]
type = PorousFlowOutflowBC
boundary = right
include_relperm = false # no need for relperm in this fully-saturated simulation
mass_fraction_component = 0
variable = frac
[]
[]
[Preconditioning]
[andy]
type = SMP
full = true
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap'
petsc_options_value = 'asm lu NONZERO 2'
[]
[]
[Executioner]
type = Transient
solve_type = Newton
dt = 1E-2
end_time = 1
nl_rel_tol = 1E-12
nl_abs_tol = 1E-12
[]
[VectorPostprocessors]
[mf]
type = LineValueSampler
start_point = '0 0 0'
end_point = '1 0 0'
num_points = 100
sort_by = x
variable = frac
[]
[]
[Outputs]
[console]
type = Console
execute_on = 'nonlinear linear'
[]
[csv]
type = CSV
sync_times = '0.1 0.5 1'
sync_only = true
[]
time_step_interval = 10
[]
(modules/contact/test/tests/verification/patch_tests/brick_2/brick2_template2.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = brick2_mesh.e
[]
[Problem]
type = AugmentedLagrangianContactProblem
maximum_lagrangian_update_iterations = 200
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./diag_saved_z]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./inc_slip_z]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./accum_slip_z]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y saved_z'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_begin
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_x26]
type = NodalVariableValue
nodeid = 25
variable = disp_x
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./disp_y26]
type = NodalVariableValue
nodeid = 25
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./back_z]
type = DirichletBC
variable = disp_z
boundary = 6
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-9
nl_rel_tol = 1e-8
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '1 3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x7 disp_y7 disp_x26 disp_y26 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+7
al_penetration_tolerance = 1e-8
[../]
[]
(modules/richards/test/tests/buckley_leverett/bl20_lumped_fu.i)
# two-phase version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 30
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.1 0.5 0.5 1 2 4'
x = '0 0.1 1 5 40 42'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-5
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./SatWater]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SatGas]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./w_aux_seff]
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFullyUpwindFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFullyUpwindFlux
variable = pgas
[../]
[]
[AuxKernels]
[./w_aux_seff_auxk]
type = RichardsSeffAux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
variable = w_aux_seff
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -300000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
expression = 1000000*(1-min(x/5,1))-if(x<5,0,300000)
[../]
[./initial_gas]
type = ParsedFunction
expression = 1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'standard'
[./bounded]
# must use --use-petsc-dm command line argument
type = SMP
full = true
petsc_options_iname = '-snes_type -pc_factor_shift_type'
petsc_options_value = 'vinewtonssls nonzero'
[../]
[./standard]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
nl_rel_tol = 1.e-9
nl_max_its = 10
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bl20_lumped_fu
execute_on = 'initial timestep_end final'
time_step_interval = 100000
exodus = true
hide = pgas
[./console_out]
type = Console
time_step_interval = 1
[../]
[]
(test/tests/multiapps/picard_multilevel/2level_picard/sub_level2.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
[]
[Variables]
[w]
[]
[]
[AuxVariables]
[v]
[]
[]
[Kernels]
[time_derivative]
type = TimeDerivative
variable = w
[]
[diffusion]
type = Diffusion
variable = w
[]
[source]
type = CoupledForce
variable = w
v = v
[]
[]
[BCs]
[dirichlet0]
type = DirichletBC
variable = w
boundary = '3'
value = 0
[]
[dirichlet]
type = DirichletBC
variable = w
boundary = '1'
value = 100
[]
[]
[Postprocessors]
[avg_v]
type = ElementAverageValue
variable = v
execute_on = 'initial timestep_begin timestep_end'
[]
[avg_w]
type = ElementAverageValue
variable = w
execute_on = 'initial timestep_begin timestep_end'
[]
[]
[Executioner]
type = Transient
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
petsc_options_value = 'hypre boomeramg 100'
end_time = 0.1
dt = 0.02
[]
[Outputs]
exodus = true
[screen]
type = Console
execute_postprocessors_on= "timestep_end timestep_begin"
[]
[]
(modules/contact/test/tests/sliding_block/sliding/frictionless_kinematic.i)
# This is a benchmark test that checks constraint based frictionless
# contact using the kinematic method. In this test a constant
# displacement is applied in the horizontal direction to simulate
# a small block come sliding down a larger block.
#
# The gold file is run on one processor
# and the benchmark case is run on a minimum of 4 processors to ensure no
# parallel variability in the contact pressure and penetration results.
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./left_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 20 101'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
time_step_interval = 10
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = frictionless
penalty = 1e+6
normal_smoothing_distance = 0.1
[../]
[]
(modules/contact/test/tests/mortar_cartesian_lms/cylinder_friction_cartesian.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '3'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '2'
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
converge_on = 'disp_x disp_y'
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[lm_x]
block = 'secondary_lower'
use_dual = true
scaling = 1.0e-5
[]
[lm_y]
block = 'secondary_lower'
use_dual = true
scaling = 1.0e-5
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Modules/TensorMechanics/Master]
[all]
incremental = false
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
strain = SMALL
add_variables = false
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2 3 4 5 6 7'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[]
[_dt]
type = TimestepSize
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff1_stress]
type = ComputeLinearElasticStress
block = '1'
[]
[stuff2_stress]
type = ComputeLinearElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options = '-snes_converged_reason -ksp_converged_reason -pc_svd_monitor '
'-snes_linesearch_monitor'
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
petsc_options_value = 'lu NONZERO 1e-12'
line_search = 'none'
nl_abs_tol = 1e-7
l_max_its = 5
nl_rel_tol = 1e-09
start_time = -0.1
end_time = 0.3 # 3.5
l_tol = 1e-8
dt = 0.1
dtmin = 0.001
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[]
[y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[]
[lm_x]
type = NodalValueSampler
variable = lm_x
boundary = '3'
sort_by = id
[]
[lm_y]
type = NodalValueSampler
variable = lm_y
boundary = '3'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = false
[console]
type = Console
max_rows = 5
[]
[chkfile]
type = CSV
show = 'x_disp y_disp lm_x lm_y'
file_base = cylinder_friction_check
create_final_symlink = true
execute_on = 'FINAL'
[]
[]
[Constraints]
[weighted_gap_lm]
type = ComputeFrictionalForceCartesianLMMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
lm_x = lm_x
lm_y = lm_y
variable = lm_x
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
correct_edge_dropping = false
mu = 0.4
c_t = 1.0e6
c = 1.0e6
[]
[x]
type = CartesianMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = lm_x
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
correct_edge_dropping = false
[]
[y]
type = CartesianMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = lm_y
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
correct_edge_dropping = false
[]
[]
(modules/contact/examples/3d_berkovich/indenter_berkovich_friction.i)
[Mesh]
file = indenter.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
order = FIRST
family = LAGRANGE
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[./saved_z]
[../]
[]
[AuxKernels]
[]
[Functions]
[./push_down]
type = ParsedFunction
expression = 'if(t < 1.5, -t, t-3.0)'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
block = '1 2'
use_automatic_differentiation = false
generate_output = 'stress_xx stress_xy stress_xz stress_yy stress_zz'
save_in = 'saved_x saved_y saved_z'
use_finite_deform_jacobian = true
[../]
[]
[BCs]
[./botz]
type = DirichletBC
variable = disp_z
boundary = 101
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 101
value = 0.0
[../]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 101
value = 0.0
[../]
[./boty111]
type = DirichletBC
variable = disp_y
boundary = 111
value = 0.0
[../]
[./botx111]
type = DirichletBC
variable = disp_x
boundary = 111
value = 0.0
[../]
[./topz]
type = FunctionDirichletBC
variable = disp_z
boundary = '201'
function = push_down
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 201
value = 0.0
[../]
[./topx]
type = DirichletBC
variable = disp_x
boundary = 201
value = 0.0
[../]
[]
[UserObjects]
[./slip_rate_gss]
type = CrystalPlasticitySlipRateGSS
variable_size = 48
slip_sys_file_name = input_slip_sys_bcc48.txt
num_slip_sys_flowrate_props = 2
flowprops = '1 48 0.0001 0.01'
uo_state_var_name = state_var_gss
slip_incr_tol = 10.0
block = 1
[../]
[./slip_resistance_gss]
type = CrystalPlasticitySlipResistanceGSS
variable_size = 48
uo_state_var_name = state_var_gss
block = 1
[../]
[./state_var_gss]
type = CrystalPlasticityStateVariable
variable_size = 48
groups = '0 24 48'
group_values = '900 1000' #120
uo_state_var_evol_rate_comp_name = state_var_evol_rate_comp_gss
scale_factor = 1.0
block = 1
[../]
[./state_var_evol_rate_comp_gss]
type = CrystalPlasticityStateVarRateComponentGSS
variable_size = 48
hprops = '1.4 1000 1200 2.5'
uo_slip_rate_name = slip_rate_gss
uo_state_var_name = state_var_gss
block = 1
[../]
[]
[Materials]
[./crysp]
type = FiniteStrainUObasedCP
block = 1
stol = 1e-2
tan_mod_type = exact
uo_slip_rates = 'slip_rate_gss'
uo_slip_resistances = 'slip_resistance_gss'
uo_state_vars = 'state_var_gss'
uo_state_var_evol_rate_comps = 'state_var_evol_rate_comp_gss'
maximum_substep_iteration = 25
[../]
[./elasticity_tensor]
type = ComputeElasticityTensorCP
block = 1
C_ijkl = '265190 113650 113650 265190 113650 265190 75769 75769 75760'
fill_method = symmetric9
[../]
[./elasticity_tensor_indenter]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1000000.0
poissons_ratio = 0.3
block = 2
[../]
[./stress_indenter]
type = ComputeFiniteStrainElasticStress
block = 2
[../]
[]
[Postprocessors]
[./stress_zz]
type = ElementAverageValue
variable = stress_zz
block = 1
[../]
[./resid_z]
type = NodalSum
variable = saved_z
boundary = 201
[../]
[./disp_z]
type = NodalExtremeValue
variable = disp_z
boundary = 201
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 60
nl_max_its = 50
dt = 0.004
dtmin = 0.00001
end_time = 1.8
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6 # 6 if no friction
l_tol = 1e-3
automatic_scaling = true
[]
[Outputs]
[./my_checkpoint]
type = Checkpoint
time_step_interval = 50
[../]
exodus = true
csv = true
print_linear_residuals = true
print_perf_log = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '202'
secondary = '102'
[../]
[]
[Contact]
[./ind_base]
primary = 202
secondary = 102
model = coulomb
friction_coefficient = 0.4
normalize_penalty = true
formulation = tangential_penalty
penalty = 1e7
capture_tolerance = 0.0001
[../]
[]
(modules/contact/test/tests/frictional/single_point_2d/single_point_2d_tp.i)
[Mesh]
file = single_point_2d.e
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./horizontal_movement]
type = ParsedFunction
expression = t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
diag_save_in = 'diag_saved_x diag_saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./botx2]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./boty2]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.005
[../]
[]
[Materials]
[./bottom]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e9
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[./top]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.01
num_steps = 1000
nl_rel_tol = 1e-08
nl_abs_tol = 1e-08
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = '0.25'
formulation = tangential_penalty
penalty = 1e10
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(test/tests/outputs/console/console_dtime_format.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
[]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Transient
start_time = -1
end_time = 1e5
[TimeSteppers]
[ts]
type = FunctionDT
function = 'if(t<0,0.3,if(t<60,3,if(t<3600,160,if(t<86400,8000,90000))))'
[]
[]
[]
[Outputs]
[screen]
type = Console
verbose = true
time_format = dtime
time_precision = 6
execute_on = 'failed nonlinear linear timestep_begin timestep_end'
[]
[]
(modules/contact/test/tests/verification/hertz_cyl/half_symm_q4/hertz_cyl_half_1deg_template3.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_half_1deg.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 11.'
y = '0. 0.0 0.0014'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
extra_vector_tags = 'ref'
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 2
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 2
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 2
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./disp_x226]
type = NodalVariableValue
nodeid = 225
variable = disp_x
[../]
[./disp_y226]
type = NodalVariableValue
nodeid = 225
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[../]
[./top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[./stuff5_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '5'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff5_strain]
type = ComputeFiniteStrain
block = '5'
[../]
[./stuff5_stress]
type = ComputeFiniteStrainElasticStress
block = '5'
[../]
[./stuff6_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '6'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff6_strain]
type = ComputeFiniteStrain
block = '6'
[../]
[./stuff6_stress]
type = ComputeFiniteStrainElasticStress
block = '6'
[../]
[./stuff7_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff7_strain]
type = ComputeFiniteStrain
block = '7'
[../]
[./stuff7_stress]
type = ComputeFiniteStrainElasticStress
block = '7'
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 100
nl_max_its = 200
start_time = 0.0
end_time = 2.0
l_tol = 5e-4
dt = 0.1
dtmin = 0.1
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./chkfile2]
type = CSV
show = 'bot_react_x bot_react_y disp_x226 disp_y226 top_react_x top_react_y'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = 0.0
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(test/tests/multiapps/multilevel/time_dt_from_parent_subsub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 100
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 1
dt = 1
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./console]
type = Console
output_file = true
[../]
[]
(test/tests/outputs/postprocessor/show_hide.i)
# Having 2 postprocessors, putting one into hide list and the other one into show list
# We should only see the PPS that is in the show list in the output.
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 10
ny = 10
elem_type = QUAD4
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Functions]
[./bc_fn]
type = ParsedFunction
expression = x
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[BCs]
[./all_u]
type = FunctionDirichletBC
variable = u
boundary = '1 3'
function = bc_fn
[../]
[]
[Postprocessors]
[./elem_56]
type = ElementalVariableValue
variable = u
elementid = 56
[../]
[./elem_12]
type = ElementalVariableValue
variable = u
elementid = 12
[../]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
[./console]
type = Console
show = 'elem_56'
hide = 'elem_12'
[../]
[./out]
type = CSV
show = 'elem_56'
hide = 'elem_12'
[../]
[]
(modules/contact/test/tests/pdass_problems/cylinder_friction_penalty_adaptivity.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = hertz_cyl_coarser.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '3'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '2'
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[AuxVariables]
[penalty_normal_pressure]
[]
[penalty_frictional_pressure]
[]
[accumulated_slip_one]
[]
[tangential_vel_one]
[]
[normal_gap]
[]
[react_x]
[]
[react_y]
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. -0.020 -0.020'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 1. 3.5'
y = '0. 0.0 0.015'
[]
[]
[Modules/TensorMechanics/Master/all]
strain = FINITE
add_variables = true
extra_vector_tags = 'ref'
block = '1 2 3 4 5 6 7'
generate_output = 'stress_xx stress_yy stress_xy'
[]
[AuxKernels]
[penalty_normal_pressure]
type = PenaltyMortarUserObjectAux
variable = penalty_normal_pressure
user_object = friction_uo
contact_quantity = normal_pressure
[]
[penalty_frictional_pressure]
type = PenaltyMortarUserObjectAux
variable = penalty_frictional_pressure
user_object = friction_uo
contact_quantity = tangential_pressure_one
[]
[penalty_accumulated_slip]
type = PenaltyMortarUserObjectAux
variable = accumulated_slip_one
user_object = friction_uo
contact_quantity = accumulated_slip_one
[]
[penalty_tangential_vel]
type = PenaltyMortarUserObjectAux
variable = tangential_vel_one
user_object = friction_uo
contact_quantity = tangential_velocity_one
[]
[penalty_gap]
type = PenaltyMortarUserObjectAux
variable = normal_gap
user_object = friction_uo
contact_quantity = normal_gap
[]
[react_x]
type = TagVectorAux
vector_tag = 'ref'
v = 'disp_x'
variable = 'react_x'
[]
[react_y]
type = TagVectorAux
vector_tag = 'ref'
v = 'disp_y'
variable = 'react_y'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = react_x
boundary = 1
[]
[bot_react_y]
type = NodalSum
variable = react_y
boundary = 1
[]
[top_react_x]
type = NodalSum
variable = react_x
boundary = 4
[]
[top_react_y]
type = NodalSum
variable = react_y
boundary = 4
[]
[_dt]
type = TimestepSize
[]
[num_lin_it]
type = NumLinearIterations
[]
[num_nonlin_it]
type = NumNonlinearIterations
[]
[cumulative]
type = CumulativeValuePostprocessor
postprocessor = num_nonlin_it
[]
[gap]
type = SideExtremeValue
value_type = min
variable = normal_gap
boundary = 3
[]
[num_al]
type = NumAugmentedLagrangeIterations
[]
[]
[BCs]
[side_x]
type = DirichletBC
variable = disp_y
boundary = '1 2'
value = 0.0
[]
[bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0.0
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = disp_ramp_vert
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = disp_ramp_horz
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2 3 4 5 6 7'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2 3 4 5 6 7'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type -pc_factor_shift_amount -mat_mffd_err'
petsc_options_value = 'lu superlu_dist NONZERO 1e-15 1e-5'
line_search = 'none'
nl_abs_tol = 1e-10
start_time = 0.0
end_time = 0.3 # 3.5
l_tol = 1e-4
dt = 0.1
dtmin = 0.001
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[surface]
type = NodalValueSampler
use_displaced_mesh = false
variable = 'disp_x disp_y penalty_normal_pressure penalty_frictional_pressure normal_gap'
boundary = '3'
sort_by = id
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = true
csv = false
[console]
type = Console
max_rows = 5
[]
[vectorpp_output]
type = CSV
create_final_symlink = true
file_base = cylinder_friction_penalty_adaptivity
execute_on = 'INITIAL TIMESTEP_END FINAL'
[]
[]
[UserObjects]
[friction_uo]
type = PenaltyFrictionUserObject
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
disp_x = disp_x
disp_y = disp_y
friction_coefficient = 0.4
secondary_variable = disp_x
penalty = 5e7
penalty_friction = 5e8
[]
[geo]
type = GeometrySphere
boundary = 3
center = '0 4 0'
radius = 3
[]
[]
[Adaptivity]
[Markers]
[contact]
type = BoundaryMarker
mark = REFINE
next_to = 3
[]
[]
initial_marker = contact
initial_steps = 2
[]
[Constraints]
[x]
type = NormalMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = '2'
secondary_boundary = '3'
primary_subdomain = '10000'
secondary_subdomain = '10001'
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = friction_uo
[]
[tangential_x]
type = TangentialMortarMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[tangential_y]
type = TangentialMortarMechanicalContact
primary_boundary = 2
secondary_boundary = 3
primary_subdomain = 10000
secondary_subdomain = 10001
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = friction_uo
[]
[]
(modules/thermal_hydraulics/test/tests/components/free_boundary_1phase/phy.conservation_free_boundary_1phase.i)
# This test tests conservation of mass, momentum, and energy on a transient
# problem with an inlet and outlet (using free boundaries for each). This test
# takes 1 time step with Crank-Nicolson and some boundary flux integral
# post-processors needed for the full conservation statement. Lastly, the
# conservation quantities are shown on the console, which should ideally be zero
# for full conservation.
[GlobalParams]
gravity_vector = '0 0 0'
scaling_factor_1phase = '1 1 1e-6'
closures = simple_closures
[]
[Functions]
[T_fn]
type = ParsedFunction
expression = '300 + 10 * (cos(2*pi*x + pi))'
[]
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[inlet]
type = FreeBoundary1Phase
input = pipe:in
[]
[pipe]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1.0
n_elems = 10
A = 1.0
initial_T = T_fn
initial_p = 1e5
initial_vel = 1
f = 0
fp = fp
[]
[outlet]
type = FreeBoundary1Phase
input = pipe:out
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = crank-nicolson
start_time = 0.0
end_time = 0.01
dt = 0.01
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-4
nl_max_its = 10
l_tol = 1e-2
l_max_its = 20
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
[]
[Postprocessors]
# MASS
[massflux_left]
type = MassFluxIntegral
boundary = inlet
arhouA = rhouA
[]
[massflux_right]
type = MassFluxIntegral
boundary = outlet
arhouA = rhouA
[]
[massflux_difference]
type = DifferencePostprocessor
value1 = massflux_right
value2 = massflux_left
[]
[massflux_integral]
type = TimeIntegratedPostprocessor
value = massflux_difference
[]
[mass]
type = ElementIntegralVariablePostprocessor
variable = rhoA
execute_on = 'initial timestep_end'
[]
[mass_change]
type = ChangeOverTimePostprocessor
postprocessor = mass
change_with_respect_to_initial = true
execute_on = 'initial timestep_end'
[]
[mass_conservation]
type = SumPostprocessor
values = 'mass_change massflux_integral'
[]
# MOMENTUM
[momentumflux_left]
type = MomentumFluxIntegral
boundary = inlet
arhouA = rhouA
vel = vel
p = p
A = A
[]
[momentumflux_right]
type = MomentumFluxIntegral
boundary = outlet
arhouA = rhouA
vel = vel
p = p
A = A
[]
[momentumflux_difference]
type = DifferencePostprocessor
value1 = momentumflux_right
value2 = momentumflux_left
[]
[momentumflux_integral]
type = TimeIntegratedPostprocessor
value = momentumflux_difference
[]
[momentum]
type = ElementIntegralVariablePostprocessor
variable = rhouA
execute_on = 'initial timestep_end'
[]
[momentum_change]
type = ChangeOverTimePostprocessor
postprocessor = momentum
change_with_respect_to_initial = true
execute_on = 'initial timestep_end'
[]
[momentum_conservation]
type = SumPostprocessor
values = 'momentum_change momentumflux_integral'
[]
# ENERGY
[energyflux_left]
type = EnergyFluxIntegral
boundary = inlet
arhouA = rhouA
H = H
[]
[energyflux_right]
type = EnergyFluxIntegral
boundary = outlet
arhouA = rhouA
H = H
[]
[energyflux_difference]
type = DifferencePostprocessor
value1 = energyflux_right
value2 = energyflux_left
[]
[energyflux_integral]
type = TimeIntegratedPostprocessor
value = energyflux_difference
[]
[energy]
type = ElementIntegralVariablePostprocessor
variable = rhoEA
execute_on = 'initial timestep_end'
[]
[energy_change]
type = ChangeOverTimePostprocessor
postprocessor = energy
change_with_respect_to_initial = true
execute_on = 'initial timestep_end'
[]
[energy_conservation]
type = SumPostprocessor
values = 'energy_change energyflux_integral'
[]
[]
[Outputs]
[console]
type = Console
show = 'mass_conservation momentum_conservation energy_conservation'
[]
velocity_as_vector = false
[]
(modules/xfem/test/tests/moving_interface/moving_ad_diffusion.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 3
xmin = 0.0
xmax = 1
ymin = 0.0
ymax = 1
elem_type = QUAD4
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./u]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'x-0.76+0.21*t'
[../]
[]
[Kernels]
[./diff]
type = ADMatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./time_deriv]
type = ADTimeDerivative
variable = u
[../]
[]
[Constraints]
[./u_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = u
jump = 0
use_penalty = true
alpha = 1e5
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./right_u]
type = ADDirichletBC
variable = u
boundary = left
value = 0
[../]
[./left_u]
type = ADDirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Materials]
[./diffusivity_A]
type = ADGenericConstantMaterial
prop_names = A_diffusion_coefficient
prop_values = 5
[../]
[./diffusivity_B]
type = ADGenericConstantMaterial
prop_names = B_diffusion_coefficient
prop_values = 0.5
[../]
[./diff_combined]
type = ADLevelSetBiMaterialReal
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = diffusion_coefficient
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
l_max_its = 20
l_tol = 1e-8
nl_max_its = 15
nl_rel_tol = 2e-12
nl_abs_tol = 1e-50
start_time = 0.0
dt = 1
end_time = 2
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
file_base = moving_diffusion_out
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/square_branch_tri_2d.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = TRI3
[]
[UserObjects]
[./line_seg_cut_uo0]
type = LineSegmentCutUserObject
cut_data = '-1.0000e-10 6.6340e-01 6.6340e-01 -1.0000e-10'
time_start_cut = 0.0
time_end_cut = 1.0
[../]
[./line_seg_cut_uo1]
type = LineSegmentCutUserObject
cut_data = '3.3120e-01 3.3200e-01 1.0001e+00 3.3200e-01'
time_start_cut = 1.0
time_end_cut = 2.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
planar_formulation = PLANE_STRAIN
add_variables = true
[../]
[]
[Functions]
[./right_disp_x]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[./top_disp_y]
type = PiecewiseLinear
x = '0 1.0 2.0 3.0'
y = '0 0.005 0.01 0.01'
[../]
[]
[BCs]
[./right_x]
type = FunctionDirichletBC
boundary = 1
variable = disp_x
function = right_disp_x
[../]
[./top_y]
type = FunctionDirichletBC
boundary = 2
variable = disp_y
function = top_disp_y
[../]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./left_x]
type = DirichletBC
boundary = 3
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-16
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 2.2
num_steps = 5000
[]
[Outputs]
file_base = square_branch_tri_2d_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/phase_field/tutorials/spinodal_decomposition/s5_energycurve.i)
#
# Example simulation of an iron-chromium alloy at 500 C. Equilibrium
# concentrations are at 23.6 and 82.3 mol% Cr. Kappa value, free energy equation,
# and mobility equation were provided by Lars Hoglund. Solved using the split
# form of the Cahn-Hilliard equation.
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
nx = 25
ny = 25
nz = 0
xmin = 0
xmax = 25
ymin = 0
ymax = 25
zmin = 0
zmax = 0
uniform_refine = 2
[]
[Variables]
[./c] # Mole fraction of Cr (unitless)
order = FIRST
family = LAGRANGE
scaling = 1e+04
[../]
[./w] # Chemical potential (eV/mol)
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./f_density] # Local energy density (eV/mol)
order = CONSTANT
family = MONOMIAL
[../]
[]
[ICs]
[./concentrationIC] # 46.774 mol% Cr with variations
type = RandomIC
min = 0.44774
max = 0.48774
seed = 210
variable = c
[../]
[]
[BCs]
[./Periodic]
[./c_bcs]
auto_direction = 'x y'
[../]
[../]
[]
[Kernels]
[./w_dot]
variable = w
v = c
type = CoupledTimeDerivative
[../]
[./coupled_res]
variable = w
type = SplitCHWRes
mob_name = M
[../]
[./coupled_parsed]
variable = c
type = SplitCHParsed
f_name = f_loc
kappa_name = kappa_c
w = w
[../]
[]
[AuxKernels]
# Calculates the energy density by combining the local and gradient energies
[./f_density] # (eV/mol/nm^2)
type = TotalFreeEnergy
variable = f_density
f_name = 'f_loc'
kappa_names = 'kappa_c'
interfacial_vars = c
[../]
[]
[Materials]
# d is a scaling factor that makes it easier for the solution to converge
# without changing the results. It is defined in each of the first three
# materials and must have the same value in each one.
[./kappa] # Gradient energy coefficient (eV nm^2/mol)
type = GenericFunctionMaterial
prop_names = 'kappa_c'
prop_values = '8.125e-16*6.24150934e+18*1e+09^2*1e-27'
# kappa_c *eV_J*nm_m^2* d
[../]
[./mobility] # Mobility (nm^2 mol/eV/s)
# NOTE: This is a fitted equation, so only 'Conv' has units
type = DerivativeParsedMaterial
property_name = M
coupled_variables = c
constant_names = 'Acr Bcr Ccr Dcr
Ecr Fcr Gcr
Afe Bfe Cfe Dfe
Efe Ffe Gfe
nm_m eV_J d'
constant_expressions = '-32.770969 -25.8186669 -3.29612744 17.669757
37.6197853 20.6941796 10.8095813
-31.687117 -26.0291774 0.2286581 24.3633544
44.3334237 8.72990497 20.956768
1e+09 6.24150934e+18 1e-27'
expression = 'nm_m^2/eV_J/d*((1-c)^2*c*10^
(Acr*c+Bcr*(1-c)+Ccr*c*log(c)+Dcr*(1-c)*log(1-c)+
Ecr*c*(1-c)+Fcr*c*(1-c)*(2*c-1)+Gcr*c*(1-c)*(2*c-1)^2)
+c^2*(1-c)*10^
(Afe*c+Bfe*(1-c)+Cfe*c*log(c)+Dfe*(1-c)*log(1-c)+
Efe*c*(1-c)+Ffe*c*(1-c)*(2*c-1)+Gfe*c*(1-c)*(2*c-1)^2))'
derivative_order = 1
outputs = exodus
[../]
[./local_energy] # Local free energy function (eV/mol)
type = DerivativeParsedMaterial
property_name = f_loc
coupled_variables = c
constant_names = 'A B C D E F G eV_J d'
constant_expressions = '-2.446831e+04 -2.827533e+04 4.167994e+03 7.052907e+03
1.208993e+04 2.568625e+03 -2.354293e+03
6.24150934e+18 1e-27'
expression = 'eV_J*d*(A*c+B*(1-c)+C*c*log(c)+D*(1-c)*log(1-c)+
E*c*(1-c)+F*c*(1-c)*(2*c-1)+G*c*(1-c)*(2*c-1)^2)'
derivative_order = 2
[../]
[./precipitate_indicator] # Returns 1/625 if precipitate
type = ParsedMaterial
property_name = prec_indic
coupled_variables = c
expression = if(c>0.6,0.0016,0)
[../]
[]
[Postprocessors]
[./step_size] # Size of the time step
type = TimestepSize
[../]
[./iterations] # Number of iterations needed to converge timestep
type = NumNonlinearIterations
[../]
[./nodes] # Number of nodes in mesh
type = NumNodes
[../]
[./evaluations] # Cumulative residual calculations for simulation
type = NumResidualEvaluations
[../]
[./total_energy] # Total free energy at each timestep
type = ElementIntegralVariablePostprocessor
variable = f_density
execute_on = 'initial timestep_end'
[../]
[./num_features] # Number of precipitates formed
type = FeatureFloodCount
variable = c
threshold = 0.6
[../]
[./precipitate_area] # Fraction of surface devoted to precipitates
type = ElementIntegralMaterialProperty
mat_prop = prec_indic
[../]
[./active_time] # Time computer spent on simulation
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[]
[Preconditioning]
[./coupled]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 30
l_tol = 1e-6
nl_max_its = 50
nl_abs_tol = 1e-9
end_time = 604800 # 7 days
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type
-sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly
ilu 1'
[./TimeStepper]
type = IterationAdaptiveDT
dt = 10
cutback_factor = 0.8
growth_factor = 1.5
optimal_iterations = 7
[../]
[./Adaptivity]
coarsen_fraction = 0.1
refine_fraction = 0.7
max_h_level = 2
[../]
[]
[Outputs]
exodus = true
console = true
csv = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/phase_field/examples/grain_growth/3D_6000_gr.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 180
ny = 180
nz = 180
xmin = 0
xmax = 180
ymin = 0
ymax = 180
zmin = 0
zmax = 180
elem_type = HEX8
[]
[GlobalParams]
op_num = 28
var_name_base = gr
[]
[Variables]
[./PolycrystalVariables]
order = FIRST
family = LAGRANGE
[../]
[]
[UserObjects]
[./voronoi]
type = PolycrystalVoronoi
grain_num = 6000 # Number of grains
rand_seed = 8675 # 301
coloring_algorithm = jp
[../]
[./term]
type = Terminator
expression = 'grain_tracker < 218'
[../]
[]
[ICs]
[./PolycrystalICs]
[./PolycrystalColoringIC]
polycrystal_ic_uo = voronoi
[../]
[../]
[]
[AuxVariables]
[./bnds]
order = FIRST
family = LAGRANGE
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./ghost_elements]
order = CONSTANT
family = MONOMIAL
[../]
[./halos]
order = CONSTANT
family = MONOMIAL
[../]
[./var_indices]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./PolycrystalKernel]
[../]
[]
[AuxKernels]
[./BndsCalc]
type = BndsCalcAux
variable = bnds
execute_on = 'initial timestep_end'
[../]
[./unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
field_display = UNIQUE_REGION
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
[../]
[./ghost_elements]
type = FeatureFloodCountAux
variable = ghost_elements
field_display = GHOSTED_ENTITIES
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
[../]
[./halos]
type = FeatureFloodCountAux
variable = halos
field_display = HALOS
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
[../]
[./var_indices]
type = FeatureFloodCountAux
variable = var_indices
field_display = VARIABLE_COLORING
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
[../]
[]
#[BCs]
# [./Periodic]
# [./All]
# auto_direction = 'x y'
# [../]
# [../]
#[]
[Materials]
[./Copper]
type = GBEvolution
T = 500
wGB = 3 # um
GBmob0 = 2.5e-6 #m^4/(Js) from Schoenfelder 1997
Q = 0.23 #Migration energy in eV
GBenergy = 0.708 #GB energy in J/m^2
molar_volume = 7.11e-6 #Molar volume in m^3/mol
length_scale = 1.0e-6
time_scale = 1.0
[../]
[]
[Postprocessors]
[./dt]
type = TimestepSize
[../]
[./n_elements]
type = NumElems
execute_on = timestep_end
[../]
[./n_nodes]
type = NumNodes
execute_on = timestep_end
[../]
[./DOFs]
type = NumDOFs
[../]
[./grain_tracker]
type = GrainTracker
threshold = 0.1
compute_halo_maps = true
[../]
[]
#[Preconditioning]
# [./SMP]
# type = SMP
# full = true
# [../]
#[]
[Executioner]
type = Transient
scheme = bdf2
solve_type = PJFNK #Preconditioned JFNK (default)
petsc_options_iname = '-pc_type'
petsc_options_value = 'asm'
l_tol = 1.0e-4
l_max_its = 30
nl_max_its = 20
nl_rel_tol = 1.0e-8
start_time = 0.0
num_steps = 500
dt = 0.0002
[./TimeStepper]
type = IterationAdaptiveDT
cutback_factor = 0.9
dt = 0.0002
growth_factor = 1.1
optimal_iterations = 8
[../]
#[./Adaptivity]
# initial_adaptivity = 4
# refine_fraction = 0.6
# coarsen_fraction = 0.1
# max_h_level = 4
# print_changed_info = true
#[../]
[]
[Outputs]
nemesis = true
checkpoint = true
csv = true
[./console]
type = Console
[../]
[]
(modules/contact/test/tests/verification/patch_tests/single_pnt_2d/single_point_2d_contact_line_search.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = single_point_2d.e
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./appl_disp]
type = PiecewiseLinear
x = '0 0.001 0.101'
y = '0 0.0 -0.10'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = appl_disp
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.002001
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputePlaneFiniteStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputePlaneFiniteStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Postprocessors]
[./disp_x]
type = NodalVariableValue
nodeid = 5
variable = disp_x
[../]
[./disp_y]
type = NodalVariableValue
nodeid = 5
variable = disp_y
[../]
[./inc_slip_x]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_x
[../]
[./inc_slip_y]
type = NodalVariableValue
nodeid = 5
variable = inc_slip_y
[../]
[./accum_slip_x]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_x
[../]
[./accum_slip_y]
type = NodalVariableValue
nodeid = 5
variable = accum_slip_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -mat_superlu_dist_iterrefine'
petsc_options_value = 'lu superlu_dist 1'
line_search = 'contact'
contact_line_search_allowed_lambda_cuts = 0
contact_line_search_ltol = 0.5
l_max_its = 15
nl_max_its = 10
dt = 0.001
end_time = 0.002
num_steps = 10000
nl_rel_tol = 1e-6
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
csv = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = frictionless
formulation = kinematic
penalty = 1e12
normalize_penalty = true
tangential_tolerance = 1e-3
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_2/plane2_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane2_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x5]
type = NodalVariableValue
nodeid = 4
variable = disp_x
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_y5]
type = NodalVariableValue
nodeid = 4
variable = disp_y
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = plane2_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = plane2_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x5 disp_y5 disp_x9 disp_y9 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/combined/test/tests/adaptive_timestepping/adapt_tstep_function_change_restart1.i)
# This is a test designed to evaluate the cabability of the
# IterationAdaptiveDT TimeStepper to adjust time step size according to
# a function. For example, if the power input function for a BISON
# simulation rapidly increases or decreases, the IterationAdaptiveDT
# TimeStepper should take time steps small enough to capture the
# oscillation.
[GlobalParams]
order = FIRST
family = LAGRANGE
block = 1
displacements = 'disp_x disp_y disp_z'
[]
[Mesh]
file = 1hex8_10mm_cube.e
[]
[Functions]
[./Fiss_Function]
type = PiecewiseLinear
x = '0 1e6 2e6 2.001e6 2.002e6'
y = '0 3e8 3e8 12e8 0'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[./temp]
initial_condition = 300.0
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
incremental = true
volumetric_locking_correction = true
eigenstrain_names = thermal_expansion
decomposition_method = EigenSolution
add_variables = true
generate_output = 'vonmises_stress'
temperature = temp
[../]
[]
[Kernels]
[./heat]
type = HeatConduction
variable = temp
[../]
[./heat_ie]
type = HeatConductionTimeDerivative
variable = temp
[../]
[./heat_source]
type = HeatSource
variable = temp
value = 1.0
function = Fiss_Function
[../]
[]
[BCs]
[./bottom_temp]
type = DirichletBC
variable = temp
boundary = 1
value = 300
[../]
[./top_bottom_disp_x]
type = DirichletBC
variable = disp_x
boundary = '1'
value = 0
[../]
[./top_bottom_disp_y]
type = DirichletBC
variable = disp_y
boundary = '1'
value = 0
[../]
[./top_bottom_disp_z]
type = DirichletBC
variable = disp_z
boundary = '1'
value = 0
[../]
[]
[Materials]
[./thermal]
type = HeatConductionMaterial
temp = temp
specific_heat = 1.0
thermal_conductivity = 1.0
[../]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 300e6
poissons_ratio = .3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[./thermal_expansion]
type = ComputeThermalExpansionEigenstrain
thermal_expansion_coeff = 5e-6
stress_free_temperature = 300.0
temperature = temp
eigenstrain_name = thermal_expansion
[../]
[./density]
type = Density
density = 10963.0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
verbose = true
nl_abs_tol = 1e-10
start_time = 0.0
num_steps = 65
end_time = 2.002e6
[./TimeStepper]
type = IterationAdaptiveDT
timestep_limiting_function = Fiss_Function
max_function_change = 3e7
dt = 1e6
[../]
[]
[Postprocessors]
[./Temperature_of_Block]
type = ElementAverageValue
variable = temp
execute_on = 'initial timestep_end'
[../]
[./vonMises]
type = ElementAverageValue
variable = vonmises_stress
execute_on = 'initial timestep_end'
[../]
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 10
[../]
[./checkpoint]
type = Checkpoint
num_files = 1
[../]
[]
(modules/contact/test/tests/verification/hertz_cyl/quart_symm_q8/hertz_cyl_qsym_1deg_template1.i)
[GlobalParams]
order = SECOND
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[Mesh]
file = hertz_cyl_qsym_1deg_q8.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Functions]
[./disp_ramp_vert]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. -0.0020 -0.0020'
[../]
[./disp_ramp_zero]
type = PiecewiseLinear
x = '0. 1. 2.'
y = '0. 0.0 0.0'
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 4
paired_boundary = 3
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 4
paired_boundary = 3
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./disp_x281]
type = NodalVariableValue
nodeid = 280
variable = disp_x
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./side_x]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.0
[../]
[./bot_y]
type = DirichletBC
variable = disp_x
boundary = '1 2 3'
value = 0.0
[../]
[./top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = 5
function = disp_ramp_vert
[../]
[]
[Materials]
[./stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e10
poissons_ratio = 0.0
[../]
[./stuff1_strain]
type = ComputeFiniteStrain
block = '1'
[../]
[./stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff2_strain]
type = ComputeFiniteStrain
block = '2'
[../]
[./stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[./stuff3_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '3'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff3_strain]
type = ComputeFiniteStrain
block = '3'
[../]
[./stuff3_stress]
type = ComputeFiniteStrainElasticStress
block = '3'
[../]
[./stuff4_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '4'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stuff4_strain]
type = ComputeFiniteStrain
block = '4'
[../]
[./stuff4_stress]
type = ComputeFiniteStrainElasticStress
block = '4'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-6
l_max_its = 50
nl_max_its = 100
start_time = 0.0
dt = 0.1
dtmin = 0.1
num_steps = 10
end_time = 1.0
l_tol = 1e-4
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '3 4 5'
sort_by = id
[../]
[./y_disp]
type = NodalValueSampler
variable = disp_y
boundary = '3 4 5'
sort_by = id
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '4'
sort_by = id
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x281 top_react_x top_react_y x_disp y_disp cont_press'
start_time = 0.9
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./interface]
primary = 3
secondary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+11
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_3/plane3_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane3_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'asm'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-8
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_sphere_mortar_error.i)
sphere_outer_htc = 10 # W/m^2/K
sphere_outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
coord_type = RZ
kernel_coverage_check = false
material_coverage_check = false
[]
[Mesh]
[file]
type = FileMeshGenerator
file = cyl2D.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '3'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[lm]
order = SECOND
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[AuxVariables]
[power_density]
block = 'fuel'
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
block = '1 2'
[]
[heat_source]
type = CoupledForce
variable = temp
block = 'fuel'
v = power_density
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 2
primary_emissivity = 0.0
secondary_emissivity = 0.0
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 2
gap_conductivity = 5.0
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
primary_boundary = 3
primary_subdomain = 10000
secondary_boundary = 2
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
gap_geometry_type = SPHERE
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = '4' # outer RPV
coefficient = ${sphere_outer_htc}
T_infinity = ${sphere_outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '2 3'
variable = temp
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 'fuel'
[]
[sphere_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = '4' # outer RVP
T_fluid = ${sphere_outer_Tinf}
htc = ${sphere_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(sphere_convective_out - ptot) / ptot'
pp_names = 'sphere_convective_out ptot'
[]
[]
(modules/thermal_hydraulics/test/tests/base/component_groups/test.i)
[GlobalParams]
closures = simple_closures
initial_p = 1e6
initial_T = 300
initial_vel = 0
[]
[FluidProperties]
[fp_liquid]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[SolidProperties]
[hx:wall]
type = ThermalFunctionSolidProperties
k = 1
cp = 1
rho = 1
[]
[]
[Components]
[pri_inlet]
type = SolidWall1Phase
input = 'hx/primary:out'
[]
[pri_outlet]
type = SolidWall1Phase
input = 'hx/primary:in'
[]
# heat exchanger
[hx]
n_elems = 2
length = 1
[primary]
type = FlowChannel1Phase
position = '0 1 0'
orientation = '1 0 0'
n_elems = ${n_elems}
length = ${length}
A = 1
f = 1
fp = fp_liquid
[]
[wall]
type = HeatStructurePlate
position = '0 0 0'
orientation = '1 0 0'
solid_properties = 'hx:wall'
solid_properties_T_ref = '300'
n_elems = ${n_elems}
length = ${length}
n_part_elems = 1
names = 0
widths = 1
depth = 1
initial_T = 300
[]
[ht_primary]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
flow_channel = hx/primary
hs_side = outer
Hw = 0
[]
[ht_secondary]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
flow_channel = hx/secondary
hs_side = inner
Hw = 0
[]
[secondary]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
n_elems = ${n_elems}
length = ${length}
A = 1
f = 1
fp = fp_liquid
[]
[]
[sec_inlet]
type = SolidWall1Phase
input = 'hx/secondary:out'
[]
[sec_outlet]
type = SolidWall1Phase
input = 'hx/secondary:in'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Transient
num_steps = 1
[]
[Outputs]
[console]
type = Console
system_info = ''
enable = false
[]
[]
[Debug]
print_component_loops = true
[]
(modules/thermal_hydraulics/test/tests/problems/brayton_cycle/closed_brayton_cycle.i)
# This input file is used to demonstrate a simple closed, air Brayton cycle using
# a compressor, turbine, shaft, motor, and generator.
# The flow length is divided into 6 segments as illustrated below, where
# - "(C)" denotes the compressor
# - "(T)" denotes the turbine
# - "*" denotes a fictitious junction
#
# Heated section Cooled section
# *-----(C)-----*--------------*-----(T)-----*--------------*
# 1 2 3 4 5 6
#
# Initially the fluid is at rest at ambient conditions, the shaft speed is zero,
# and no heat transfer occurs with the system.
# The transient is controlled as follows:
# * 0 - 100 s: motor ramps up torque linearly from zero
# * 100 - 200 s: motor ramps down torque linearly to zero, HTC ramps up linearly from zero.
# * 200 - 300 s: (no changes; should approach steady condition)
I_motor = 1.0
motor_torque_max = 400.0
I_generator = 1.0
generator_torque_per_shaft_speed = -0.00025
motor_ramp_up_duration = 100.0
motor_ramp_down_duration = 100.0
post_motor_time = 100.0
t1 = ${motor_ramp_up_duration}
t2 = ${fparse t1 + motor_ramp_down_duration}
t3 = ${fparse t2 + post_motor_time}
D1 = 0.15
D2 = ${D1}
D3 = ${D1}
D4 = ${D1}
D5 = ${D1}
D6 = ${D1}
A1 = ${fparse 0.25 * pi * D1^2}
A2 = ${fparse 0.25 * pi * D2^2}
A3 = ${fparse 0.25 * pi * D3^2}
A4 = ${fparse 0.25 * pi * D4^2}
A5 = ${fparse 0.25 * pi * D5^2}
A6 = ${fparse 0.25 * pi * D6^2}
L1 = 10.0
L2 = ${L1}
L3 = ${L1}
L4 = ${L1}
L5 = ${L1}
L6 = ${L1}
x1 = 0.0
x2 = ${fparse x1 + L1}
x3 = ${fparse x2 + L2}
x4 = ${fparse x3 + L3}
x5 = ${fparse x4 + L4}
x6 = ${fparse x5 + L5}
x2_minus = ${fparse x2 - 0.001}
x2_plus = ${fparse x2 + 0.001}
x5_minus = ${fparse x5 - 0.001}
x5_plus = ${fparse x5 + 0.001}
n_elems1 = 10
n_elems2 = ${n_elems1}
n_elems3 = ${n_elems1}
n_elems4 = ${n_elems1}
n_elems5 = ${n_elems1}
n_elems6 = ${n_elems1}
A_ref_comp = ${fparse 0.5 * (A1 + A2)}
V_comp = ${fparse A_ref_comp * 1.0}
I_comp = 1.0
A_ref_turb = ${fparse 0.5 * (A4 + A5)}
V_turb = ${fparse A_ref_turb * 1.0}
I_turb = 1.0
c0_rated_comp = 351.6925137
rho0_rated_comp = 1.146881112
rated_mfr = 0.25
speed_rated_rpm = 96000
speed_rated = ${fparse speed_rated_rpm * 2 * pi / 60.0}
speed_initial = 0
eff_comp = 0.79
eff_turb = 0.843
T_hot = 1000
T_cold = 300
T_ambient = 300
p_ambient = 1e5
[GlobalParams]
orientation = '1 0 0'
gravity_vector = '0 0 0'
initial_p = ${p_ambient}
initial_T = ${T_ambient}
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
fp = fp_air
closures = closures
f = 0
scaling_factor_1phase = '1 1 1e-5'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1
scaling_factor_rhovV = 1
scaling_factor_rhowV = 1
scaling_factor_rhoEV = 1e-5
rdg_slope_reconstruction = none
[]
[Functions]
[motor_torque_fn]
type = PiecewiseLinear
x = '0 ${t1} ${t2}'
y = '0 ${motor_torque_max} 0'
[]
[motor_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'motor_torque shaft:omega'
[]
[generator_torque_fn]
type = ParsedFunction
expression = 'slope * t'
symbol_names = 'slope'
symbol_values = '${generator_torque_per_shaft_speed}'
[]
[generator_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'generator_torque shaft:omega'
[]
[htc_wall_fn]
type = PiecewiseLinear
x = '0 ${t1} ${t2}'
y = '0 0 1e3'
[]
[]
[FluidProperties]
[fp_air]
type = IdealGasFluidProperties
emit_on_nan = none
[]
[]
[Closures]
[closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[shaft]
type = Shaft
connected_components = 'motor compressor turbine generator'
initial_speed = ${speed_initial}
[]
[motor]
type = ShaftConnectedMotor
inertia = ${I_motor}
torque = 0 # controlled
[]
[generator]
type = ShaftConnectedMotor
inertia = ${I_generator}
torque = generator_torque_fn
[]
[pipe1]
type = FlowChannel1Phase
position = '${x1} 0 0'
length = ${L1}
n_elems = ${n_elems1}
A = ${A1}
[]
[compressor]
type = ShaftConnectedCompressor1Phase
position = '${x2} 0 0'
inlet = 'pipe1:out'
outlet = 'pipe2:in'
A_ref = ${A_ref_comp}
volume = ${V_comp}
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
speeds = '0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_comp1 rp_comp2 rp_comp3 rp_comp4 rp_comp5'
eff_functions = 'eff_comp1 eff_comp2 eff_comp3 eff_comp4 eff_comp5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_comp}
inertia_coeff = '${I_comp} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
[pipe2]
type = FlowChannel1Phase
position = '${x2} 0 0'
length = ${L2}
n_elems = ${n_elems2}
A = ${A2}
[]
[junction2_3]
type = JunctionOneToOne1Phase
connections = 'pipe2:out pipe3:in'
[]
[pipe3]
type = FlowChannel1Phase
position = '${x3} 0 0'
length = ${L3}
n_elems = ${n_elems3}
A = ${A3}
[]
[junction3_4]
type = JunctionOneToOne1Phase
connections = 'pipe3:out pipe4:in'
[]
[pipe4]
type = FlowChannel1Phase
position = '${x4} 0 0'
length = ${L4}
n_elems = ${n_elems4}
A = ${A4}
[]
[turbine]
type = ShaftConnectedCompressor1Phase
position = '${x5} 0 0'
inlet = 'pipe4:out'
outlet = 'pipe5:in'
A_ref = ${A_ref_turb}
volume = ${V_turb}
treat_as_turbine = true
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
speeds = '0 0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_turb0 rp_turb1 rp_turb2 rp_turb3 rp_turb4 rp_turb5'
eff_functions = 'eff_turb1 eff_turb1 eff_turb2 eff_turb3 eff_turb4 eff_turb5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_turb}
inertia_coeff = '${I_turb} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
[pipe5]
type = FlowChannel1Phase
position = '${x5} 0 0'
length = ${L5}
n_elems = ${n_elems5}
A = ${A5}
[]
[junction5_6]
type = JunctionOneToOne1Phase
connections = 'pipe5:out pipe6:in'
[]
[pipe6]
type = FlowChannel1Phase
position = '${x6} 0 0'
length = ${L6}
n_elems = ${n_elems6}
A = ${A6}
[]
[junction6_1]
type = JunctionOneToOne1Phase
connections = 'pipe6:out pipe1:in'
[]
[heating]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = pipe3
T_wall = ${T_hot}
Hw = htc_wall_fn
[]
[cooling]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = pipe6
T_wall = ${T_cold}
Hw = htc_wall_fn
[]
[]
[ControlLogic]
[motor_ctrl]
type = TimeFunctionComponentControl
component = motor
parameter = torque
function = motor_torque_fn
[]
[]
[Postprocessors]
[heating_rate]
type = ADHeatRateConvection1Phase
block = 'pipe3'
T = T
T_wall = T_wall
Hw = Hw
P_hf = P_hf
execute_on = 'INITIAL TIMESTEP_END'
[]
[cooling_rate]
type = ADHeatRateConvection1Phase
block = 'pipe6'
T = T
T_wall = T_wall
Hw = Hw
P_hf = P_hf
execute_on = 'INITIAL TIMESTEP_END'
[]
[motor_torque]
type = RealComponentParameterValuePostprocessor
component = motor
parameter = torque
execute_on = 'INITIAL TIMESTEP_END'
[]
[motor_power]
type = FunctionValuePostprocessor
function = motor_power_fn
execute_on = 'INITIAL TIMESTEP_END'
indirect_dependencies = 'motor_torque shaft:omega'
[]
[generator_torque]
type = ShaftConnectedComponentPostprocessor
quantity = torque
shaft_connected_component_uo = generator:shaftconnected_uo
execute_on = 'INITIAL TIMESTEP_END'
[]
[generator_power]
type = FunctionValuePostprocessor
function = generator_power_fn
execute_on = 'INITIAL TIMESTEP_END'
indirect_dependencies = 'generator_torque shaft:omega'
[]
[shaft_speed]
type = ScalarVariable
variable = 'shaft:omega'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_in_comp]
type = PointValue
variable = p
point = '${x2_minus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_comp]
type = PointValue
variable = p
point = '${x2_plus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_comp]
type = ParsedPostprocessor
pp_names = 'p_in_comp p_out_comp'
expression = 'p_out_comp / p_in_comp'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_in_turb]
type = PointValue
variable = p
point = '${x5_minus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_turb]
type = PointValue
variable = p
point = '${x5_plus} 0 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_turb]
type = ParsedPostprocessor
pp_names = 'p_in_turb p_out_turb'
expression = 'p_in_turb / p_out_turb'
execute_on = 'INITIAL TIMESTEP_END'
[]
[mfr_comp]
type = ADFlowJunctionFlux1Phase
boundary = pipe1:out
connection_index = 0
equation = mass
junction = compressor
[]
[mfr_turb]
type = ADFlowJunctionFlux1Phase
boundary = pipe4:out
connection_index = 0
equation = mass
junction = turbine
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
end_time = ${t3}
dt = 0.1
abort_on_solve_fail = true
solve_type = NEWTON
nl_rel_tol = 1e-50
nl_abs_tol = 1e-11
nl_max_its = 15
l_tol = 1e-4
l_max_its = 10
[]
[Outputs]
[csv]
type = CSV
file_base = 'closed_brayton_cycle'
execute_vector_postprocessors_on = 'INITIAL'
[]
[console]
type = Console
show = 'shaft_speed p_ratio_comp p_ratio_turb compressor:pressure_ratio turbine:pressure_ratio'
[]
[]
[Functions]
# compressor pressure ratio
[rp_comp1]
type = PiecewiseLinear
data_file = 'rp_comp1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp2]
type = PiecewiseLinear
data_file = 'rp_comp2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp3]
type = PiecewiseLinear
data_file = 'rp_comp3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp4]
type = PiecewiseLinear
data_file = 'rp_comp4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp5]
type = PiecewiseLinear
data_file = 'rp_comp5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# compressor efficiency
[eff_comp1]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp2]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp3]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp4]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp5]
type = ConstantFunction
value = ${eff_comp}
[]
# turbine pressure ratio
[rp_turb0]
type = ConstantFunction
value = 1
[]
[rp_turb1]
type = PiecewiseLinear
data_file = 'rp_turb1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb2]
type = PiecewiseLinear
data_file = 'rp_turb2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb3]
type = PiecewiseLinear
data_file = 'rp_turb3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb4]
type = PiecewiseLinear
data_file = 'rp_turb4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb5]
type = PiecewiseLinear
data_file = 'rp_turb5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# turbine efficiency
[eff_turb1]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb2]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb3]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb4]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb5]
type = ConstantFunction
value = ${eff_turb}
[]
[]
(modules/thermal_hydraulics/test/tests/problems/brayton_cycle/recuperated_brayton_cycle.i)
# This input file models an open, recuperated Brayton cycle with a PID
# controlled start up using a coupled motor.
#
# Heat is supplied to the system by a volumetric heat source, and a second heat
# source is used to model a recuperator. The recuperator transfers heat from the
# turbine exhaust gas to the compressor outlet gas.
#
# Initially the fluid and heat structures are at rest at ambient conditions,
# and the shaft speed is zero.
# The transient is controlled as follows:
# * 0 - 2000 s: Motor increases shaft speed to approx. 85,000 RPM by PID control
# * 1000 - 8600 s: Power in main heat source increases from 0 - 104 kW
# * 2000 - 200000 s: Torque supplied by turbine increases to steady state level
# as working fluid temperature increases. Torque supplied by
# the motor is ramped down to 0 N-m transitioning shaft control
# to the turbine at its rated speed of 96,000 RPM.
I_motor = 1.0
I_generator = 1.0
generator_torque_per_shaft_speed = -0.00025
motor_ramp_up_duration = 3605
motor_ramp_down_duration = 1800
post_motor_time = 2160000
t1 = ${motor_ramp_up_duration}
t2 = ${fparse t1 + motor_ramp_down_duration}
t3 = ${fparse t2 + post_motor_time}
D1 = 0.15
D2 = ${D1}
D3 = ${D1}
D4 = ${D1}
D5 = ${D1}
D6 = ${D1}
D7 = ${D1}
D8 = ${D1}
A1 = ${fparse 0.25 * pi * D1^2}
A2 = ${fparse 0.25 * pi * D2^2}
A3 = ${fparse 0.25 * pi * D3^2}
A4 = ${fparse 0.25 * pi * D4^2}
A5 = ${fparse 0.25 * pi * D5^2}
A6 = ${fparse 0.25 * pi * D6^2}
A7 = ${fparse 0.25 * pi * D7^2}
A8 = ${fparse 0.25 * pi * D8^2}
recuperator_width = 0.15
L1 = 5.0
L2 = ${L1}
L3 = ${fparse 2 * L1}
L4 = ${fparse 2 * L1}
L5 = ${L1}
L6 = ${L1}
L7 = ${fparse L1 + recuperator_width}
L8 = ${L1}
x1 = 0.0
x2 = ${fparse x1 + L1}
x3 = ${fparse x2 + L2}
x4 = ${x3}
x5 = ${fparse x4 - L4}
x6 = ${x5}
x7 = ${fparse x6 + L6}
x8 = ${fparse x7 + L7}
y1 = 0
y2 = ${y1}
y3 = ${y2}
y4 = ${fparse y3 - L3}
y5 = ${y4}
y6 = ${fparse y5 + L5}
y7 = ${y6}
y8 = ${y7}
x1_out = ${fparse x1 + L1 - 0.001}
x2_in = ${fparse x2 + 0.001}
y5_in = ${fparse y5 + 0.001}
x6_out = ${fparse x6 + L6 - 0.001}
x7_in = ${fparse x7 + 0.001}
y8_in = ${fparse y8 + 0.001}
y8_out = ${fparse y8 + L8 - 0.001}
hot_leg_in = ${y8_in}
hot_leg_out = ${y8_out}
cold_leg_in = ${fparse y3 - 0.001}
cold_leg_out = ${fparse y3 - (L3/2) - 0.001}
n_elems1 = 5
n_elems2 = ${n_elems1}
n_elems3 = ${fparse 2 * n_elems1}
n_elems4 = ${fparse 2 * n_elems1}
n_elems5 = ${n_elems1}
n_elems6 = ${n_elems1}
n_elems7 = ${n_elems1}
n_elems8 = ${n_elems1}
A_ref_comp = ${fparse 0.5 * (A1 + A2)}
V_comp = ${fparse A_ref_comp * 1.0}
I_comp = 1.0
A_ref_turb = ${fparse 0.5 * (A4 + A5)}
V_turb = ${fparse A_ref_turb * 1.0}
I_turb = 1.0
c0_rated_comp = 351.6925137
rho0_rated_comp = 1.146881112
rated_mfr = 0.25
speed_rated_rpm = 96000
speed_rated = ${fparse speed_rated_rpm * 2 * pi / 60.0}
speed_initial = 0
eff_comp = 0.79
eff_turb = 0.843
T_ambient = 300
p_ambient = 1e5
hs_power = 105750
[GlobalParams]
gravity_vector = '0 0 0'
initial_p = ${p_ambient}
initial_T = ${T_ambient}
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
fp = fp_air
closures = closures
f = 0
scaling_factor_1phase = '1 1 1e-5'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1e-2
scaling_factor_rhovV = 1e-2
scaling_factor_rhowV = 1e-2
scaling_factor_rhoEV = 1e-5
scaling_factor_temperature = 1e-2
rdg_slope_reconstruction = none
[]
[FluidProperties]
[fp_air]
type = IdealGasFluidProperties
emit_on_nan = none
[]
[]
[SolidProperties]
[steel]
type = ThermalFunctionSolidProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Closures]
[closures]
type = Closures1PhaseSimple
[]
[]
[Functions]
##########################
# Motor
##########################
# Functions for control logic that determines when to shut off the PID system
[is_tripped_fn]
type = ParsedFunction
symbol_names = 'motor_torque turbine_torque'
symbol_values = 'motor_torque turbine_torque'
expression = 'turbine_torque > motor_torque'
[]
[PID_tripped_constant_value]
type = ConstantFunction
value = 1
[]
[PID_tripped_status_fn]
type = ParsedFunction
symbol_values = 'PID_trip_status'
symbol_names = 'PID_trip_status'
expression = 'PID_trip_status'
[]
[time_fn]
type = ParsedFunction
expression = t
[]
# Shutdown function which ramps down the motor once told by the control logic
[motor_torque_fn_shutdown]
type = ParsedFunction
symbol_values = 'PID_trip_status time_trip'
symbol_names = 'PID_trip_status time_trip'
expression = 'if(PID_trip_status = 1, max(2.4 - (2.4 * ((t - time_trip) / 35000)),0.0), 1)'
[]
# Generates motor power curve
[motor_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'motor_torque shaft:omega'
[]
##########################
# Generator
##########################
# Generates generator torque curve
[generator_torque_fn]
type = ParsedFunction
expression = 'slope * t'
symbol_names = 'slope'
symbol_values = '${generator_torque_per_shaft_speed}'
[]
# Generates generator power curve
[generator_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'generator_torque shaft:omega'
[]
##########################
# Reactor
##########################
# Ramps up reactor power when activated by control logic
[power_fn]
type = PiecewiseLinear
x = '0 1000 8600'
y = '0 0 ${hs_power}'
[]
##########################
# Compressor
##########################
# compressor pressure ratios
[rp_comp1]
type = PiecewiseLinear
data_file = 'rp_comp1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp2]
type = PiecewiseLinear
data_file = 'rp_comp2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp3]
type = PiecewiseLinear
data_file = 'rp_comp3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp4]
type = PiecewiseLinear
data_file = 'rp_comp4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp5]
type = PiecewiseLinear
data_file = 'rp_comp5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# compressor efficiencies
[eff_comp1]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp2]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp3]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp4]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp5]
type = ConstantFunction
value = ${eff_comp}
[]
##########################
# Turbine
##########################
# turbine pressure ratios
[rp_turb0]
type = ConstantFunction
value = 1
[]
[rp_turb1]
type = PiecewiseLinear
data_file = 'rp_turb1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb2]
type = PiecewiseLinear
data_file = 'rp_turb2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb3]
type = PiecewiseLinear
data_file = 'rp_turb3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb4]
type = PiecewiseLinear
data_file = 'rp_turb4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb5]
type = PiecewiseLinear
data_file = 'rp_turb5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# turbine efficiency
[eff_turb1]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb2]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb3]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb4]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb5]
type = ConstantFunction
value = ${eff_turb}
[]
[]
[Components]
# system inlet pulling air from the open atmosphere
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = ${p_ambient}
T0 = ${T_ambient}
[]
# Inlet pipe
[pipe1]
type = FlowChannel1Phase
position = '${x1} ${y1} 0'
orientation = '1 0 0'
length = ${L1}
n_elems = ${n_elems1}
A = ${A1}
[]
# Compressor as defined in MAGNET PCU document (Guillen 2020)
[compressor]
type = ShaftConnectedCompressor1Phase
position = '${x2} ${y2} 0'
inlet = 'pipe1:out'
outlet = 'pipe2:in'
A_ref = ${A_ref_comp}
volume = ${V_comp}
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
# Determines which compression ratio curve and efficiency curve to use depending on ratio of speed/rated_speed
speeds = '0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_comp1 rp_comp2 rp_comp3 rp_comp4 rp_comp5'
eff_functions = 'eff_comp1 eff_comp2 eff_comp3 eff_comp4 eff_comp5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_comp}
inertia_coeff = '${I_comp} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
# Outlet pipe from the compressor
[pipe2]
type = FlowChannel1Phase
position = '${x2} ${y2} 0'
orientation = '1 0 0'
length = ${L2}
n_elems = ${n_elems2}
A = ${A2}
[]
# 90 degree connection between pipe 2 and 3
[junction2_cold_leg]
type = VolumeJunction1Phase
connections = 'pipe2:out cold_leg:in'
position = '${x3} ${y3} 0'
volume = ${fparse A2*0.1}
[]
# Cold leg of the recuperator
[cold_leg]
type = FlowChannel1Phase
position = '${x3} ${y3} 0'
orientation = '0 -1 0'
length = ${fparse L3/2}
n_elems = ${fparse n_elems3/2}
A = ${A3}
[]
# Recuperator which transfers heat from exhaust gas to reactor inlet gas to improve thermal efficency
[recuperator]
type = HeatStructureCylindrical
orientation = '0 -1 0'
position = '${x3} ${y3} 0'
length = ${fparse L3/2}
widths = ${recuperator_width}
n_elems = ${fparse n_elems3/2}
n_part_elems = 2
names = recuperator
solid_properties = steel
solid_properties_T_ref = '300'
inner_radius = ${D1}
[]
# heat transfer from recuperator to cold leg
[heat_transfer_cold_leg]
type = HeatTransferFromHeatStructure1Phase
flow_channel = cold_leg
hs = recuperator
hs_side = OUTER
Hw = 10000
[]
# heat transfer from hot leg to recuperator
[heat_transfer_hot_leg]
type = HeatTransferFromHeatStructure1Phase
flow_channel = hot_leg
hs = recuperator
hs_side = INNER
Hw = 10000
[]
[junction_cold_leg_3]
type = JunctionOneToOne1Phase
connections = 'cold_leg:out pipe3:in'
[]
[pipe3]
type = FlowChannel1Phase
position = '${x3} ${fparse y3 - (L3/2)} 0'
orientation = '0 -1 0'
length = ${fparse L3/2}
n_elems = ${fparse n_elems3/2}
A = ${A3}
[]
# 90 degree connection between pipe 3 and 4
[junction3_4]
type = VolumeJunction1Phase
connections = 'pipe3:out pipe4:in'
position = '${x4} ${y4} 0'
volume = ${fparse A3*0.1}
[]
# Pipe through the "reactor core"
[pipe4]
type = FlowChannel1Phase
position = '${x4} ${y4} 0'
orientation = '-1 0 0'
length = ${L4}
n_elems = ${n_elems4}
A = ${A4}
[]
# "Reactor Core" and it's associated heat transfer to pipe 4
[reactor]
type = HeatStructureCylindrical
orientation = '-1 0 0'
position = '${x4} ${y4} 0'
length = ${L4}
widths = 0.15
n_elems = ${n_elems4}
n_part_elems = 2
names = core
solid_properties = steel
solid_properties_T_ref = '300'
[]
[total_power]
type = TotalPower
power = 0
[]
[heat_generation]
type = HeatSourceFromTotalPower
power = total_power
hs = reactor
regions = core
[]
[heat_transfer]
type = HeatTransferFromHeatStructure1Phase
flow_channel = pipe4
hs = reactor
hs_side = OUTER
Hw = 10000
[]
# 90 degree connection between pipe 4 and 5
[junction4_5]
type = VolumeJunction1Phase
connections = 'pipe4:out pipe5:in'
position = '${x5} ${y5} 0'
volume = ${fparse A4*0.1}
[]
# Pipe carrying hot gas back to the PCU
[pipe5]
type = FlowChannel1Phase
position = '${x5} ${y5} 0'
orientation = '0 1 0'
length = ${L5}
n_elems = ${n_elems5}
A = ${A5}
[]
# 90 degree connection between pipe 5 and 6
[junction5_6]
type = VolumeJunction1Phase
connections = 'pipe5:out pipe6:in'
position = '${x6} ${y6} 0'
volume = ${fparse A5*0.1}
[]
# Inlet pipe to the turbine
[pipe6]
type = FlowChannel1Phase
position = '${x6} ${y6} 0'
orientation = '1 0 0'
length = ${L6}
n_elems = ${n_elems6}
A = ${A6}
[]
# Turbine as defined in MAGNET PCU document (Guillen 2020) and (Wright 2006)
[turbine]
type = ShaftConnectedCompressor1Phase
position = '${x7} ${y7} 0'
inlet = 'pipe6:out'
outlet = 'pipe7:in'
A_ref = ${A_ref_turb}
volume = ${V_turb}
# A turbine is treated as an "inverse" compressor, this value determines if component is to be treated as turbine or compressor
# If treat_as_turbine is omitted, code automatically assumes it is a compressor
treat_as_turbine = true
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
# Determines which compression ratio curve and efficiency curve to use depending on ratio of speed/rated_speed
speeds = '0 0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_turb0 rp_turb1 rp_turb2 rp_turb3 rp_turb4 rp_turb5'
eff_functions = 'eff_turb1 eff_turb1 eff_turb2 eff_turb3 eff_turb4 eff_turb5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_turb}
inertia_coeff = '${I_turb} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
# Outlet pipe from turbine
[pipe7]
type = FlowChannel1Phase
position = '${x7} ${y7} 0'
orientation = '1 0 0'
length = ${L7}
n_elems = ${n_elems7}
A = ${A7}
[]
# 90 degree connection between pipe 7 and 8
[junction7_hot_leg]
type = VolumeJunction1Phase
connections = 'pipe7:out hot_leg:in'
position = '${x8} ${y8} 0'
volume = ${fparse A7*0.1}
[]
# Hot leg of the recuperator
[hot_leg]
type = FlowChannel1Phase
position = '${x8} ${y8} 0'
orientation = '0 1 0'
length = ${L8}
n_elems = ${n_elems8}
A = ${A8}
[]
# System outlet dumping exhaust gas to the atmosphere
[outlet]
type = Outlet1Phase
input = 'hot_leg:out'
p = ${p_ambient}
[]
# Roatating shaft connecting motor, compressor, turbine, and generator
[shaft]
type = Shaft
connected_components = 'motor compressor turbine generator'
initial_speed = ${speed_initial}
[]
# 3-Phase electircal motor used for system start-up, controlled by PID
[motor]
type = ShaftConnectedMotor
inertia = ${I_motor}
torque = 0 # controlled
[]
# Electric generator supplying power to the grid
[generator]
type = ShaftConnectedMotor
inertia = ${I_generator}
torque = generator_torque_fn
[]
[]
# Control logics which govern startup of the motor, startup of the "reactor core", and shutdown of the motor
[ControlLogic]
# Sets desired shaft speed to be reached by motor NOTE: SHOULD BE SET LOWER THAN RATED TURBINE RPM
[set_point]
type = GetFunctionValueControl
function = ${fparse speed_rated_rpm - 9000}
[]
# PID with gains determined by iterative process NOTE: Gain values are system specific
[initial_motor_PID]
type = PIDControl
set_point = set_point:value
input = shaft_RPM
initial_value = 0
K_p = 0.0011
K_i = 0.00000004
K_d = 0
[]
# Determines when the PID system should be running and when it should begin the shutdown cycle. If needed: PID output, else: shutdown function
[logic]
type = ParsedFunctionControl
function = 'if(motor+0.5 > turb, PID, shutdown_fn)'
symbol_names = 'motor turb PID shutdown_fn'
symbol_values = 'motor_torque turbine_torque initial_motor_PID:output motor_torque_fn_shutdown'
[]
# Takes the output generated in [logic] and applies it to the motor torque
[motor_PID]
type = SetComponentRealValueControl
component = motor
parameter = torque
value = logic:value
[]
# Determines when to turn on heat source
[power_logic]
type = ParsedFunctionControl
function = 'power_fn'
symbol_names = 'power_fn'
symbol_values = 'power_fn'
[]
# Applies heat source to the total_power block
[power_applied]
type = SetComponentRealValueControl
component = total_power
parameter = power
value = power_logic:value
[]
[]
[Controls]
# Enables set_PID_tripped
[PID_trip_status]
type = ConditionalFunctionEnableControl
conditional_function = is_tripped_fn
enable_objects = 'AuxScalarKernels::PID_trip_status_aux'
execute_on = 'TIMESTEP_END'
[]
# Enables set_time_PID
[time_PID]
type = ConditionalFunctionEnableControl
conditional_function = PID_tripped_status_fn
disable_objects = 'AuxScalarKernels::time_trip_aux'
execute_on = 'TIMESTEP_END'
[]
[]
[AuxVariables]
# Creates a variable that will later be set to the time when tau_turbine > tau_motor
[time_trip]
order = FIRST
family = SCALAR
[]
# Creates variable which indicates if tau_turbine > tau_motor....... If tau_motor > tau_turbine, 0, else 1
[PID_trip_status]
order = FIRST
family = SCALAR
initial_condition = 0
[]
[]
[AuxScalarKernels]
# Creates variable from time_fn which indicates when tau_turbine > tau_motor
[time_trip_aux]
type = FunctionScalarAux
function = time_fn
variable = time_trip
execute_on = 'TIMESTEP_END'
[]
# Overwrites variable PID_trip_status to the value from PID_tripped_constant_value (changes 0 to 1)
[PID_trip_status_aux]
type = FunctionScalarAux
function = PID_tripped_constant_value
variable = PID_trip_status
execute_on = 'TIMESTEP_END'
enable = false
[]
[]
[Postprocessors]
# Indicates when tau_turbine > tau_motor
[trip_time]
type = ScalarVariable
variable = time_trip
execute_on = 'TIMESTEP_END'
[]
##########################
# Motor
##########################
[motor_torque]
type = RealComponentParameterValuePostprocessor
component = motor
parameter = torque
execute_on = 'INITIAL TIMESTEP_END'
[]
[motor_power]
type = FunctionValuePostprocessor
function = motor_power_fn
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# generator
##########################
[generator_torque]
type = ShaftConnectedComponentPostprocessor
quantity = torque
shaft_connected_component_uo = generator:shaftconnected_uo
execute_on = 'INITIAL TIMESTEP_END'
[]
[generator_power]
type = FunctionValuePostprocessor
function = generator_power_fn
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# Shaft
##########################
# Speed in rad/s
[shaft_speed]
type = ScalarVariable
variable = 'shaft:omega'
execute_on = 'INITIAL TIMESTEP_END'
[]
# speed in RPM
[shaft_RPM]
type = ParsedPostprocessor
pp_names = 'shaft_speed'
expression = '(shaft_speed * 60) /( 2 * ${fparse pi})'
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# Compressor
##########################
[comp_dissipation_torque]
type = ScalarVariable
variable = 'compressor:dissipation_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[comp_isentropic_torque]
type = ScalarVariable
variable = 'compressor:isentropic_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[comp_friction_torque]
type = ScalarVariable
variable = 'compressor:friction_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[compressor_torque]
type = ParsedPostprocessor
pp_names = 'comp_dissipation_torque comp_isentropic_torque comp_friction_torque'
expression = 'comp_dissipation_torque + comp_isentropic_torque + comp_friction_torque'
[]
[p_in_comp]
type = PointValue
variable = p
point = '${x1_out} ${y1} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_comp]
type = PointValue
variable = p
point = '${x2_in} ${y2} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_comp]
type = ParsedPostprocessor
pp_names = 'p_in_comp p_out_comp'
expression = 'p_out_comp / p_in_comp'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_in_comp]
type = PointValue
variable = T
point = '${x1_out} ${y1} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_out_comp]
type = PointValue
variable = T
point = '${x2_in} ${y2} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_ratio_comp]
type = ParsedPostprocessor
pp_names = 'T_in_comp T_out_comp'
expression = '(T_out_comp - T_in_comp) / T_out_comp'
execute_on = 'INITIAL TIMESTEP_END'
[]
[mfr_comp]
type = ADFlowJunctionFlux1Phase
boundary = pipe1:out
connection_index = 0
equation = mass
junction = compressor
[]
##########################
# turbine
##########################
[turb_dissipation_torque]
type = ScalarVariable
variable = 'turbine:dissipation_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[turb_isentropic_torque]
type = ScalarVariable
variable = 'turbine:isentropic_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[turb_friction_torque]
type = ScalarVariable
variable = 'turbine:friction_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[turbine_torque]
type = ParsedPostprocessor
pp_names = 'turb_dissipation_torque turb_isentropic_torque turb_friction_torque'
expression = 'turb_dissipation_torque + turb_isentropic_torque + turb_friction_torque'
[]
[p_in_turb]
type = PointValue
variable = p
point = '${x6_out} ${y6} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_turb]
type = PointValue
variable = p
point = '${x7_in} ${y7} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_turb]
type = ParsedPostprocessor
pp_names = 'p_in_turb p_out_turb'
expression = 'p_in_turb / p_out_turb'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_in_turb]
type = PointValue
variable = T
point = '${x6_out} ${y6} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_out_turb]
type = PointValue
variable = T
point = '${x7_in} ${y7} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[mfr_turb]
type = ADFlowJunctionFlux1Phase
boundary = pipe6:out
connection_index = 0
equation = mass
junction = turbine
[]
##########################
# Recuperator
##########################
[cold_leg_in]
type = PointValue
variable = T
point = '${x3} ${cold_leg_in} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[cold_leg_out]
type = PointValue
variable = T
point = '${x3} ${cold_leg_out} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[hot_leg_in]
type = PointValue
variable = T
point = '${x8} ${hot_leg_in} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[hot_leg_out]
type = PointValue
variable = T
point = '${x8} ${hot_leg_out} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# Reactor
##########################
[reactor_inlet]
type = PointValue
variable = T
point = '${x4} ${y4} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[reactor_outlet]
type = PointValue
variable = T
point = '${x5} ${y5_in} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
end_time = ${t3}
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.01
growth_factor = 1.1
cutback_factor = 0.9
[]
dtmin = 1e-5
dtmax = 1000
steady_state_detection = true
steady_state_start_time = 200000
solve_type = NEWTON
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 15
l_tol = 1e-4
l_max_its = 10
petsc_options_iname = '-pc_type'
petsc_options_value = ' lu '
[]
[Outputs]
[e]
type = Exodus
file_base = 'recuperated_brayton_cycle_out'
[]
[csv]
type = CSV
file_base = 'recuperated_brayton_cycle'
execute_vector_postprocessors_on = 'INITIAL'
[]
[console]
type = Console
show = 'shaft_speed p_ratio_comp p_ratio_turb compressor:pressure_ratio turbine:pressure_ratio'
[]
[]
(modules/xfem/test/tests/pressure_bc/inclined_edge_2d_pressure.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
volumetric_locking_correction = False
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 9
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.0 0.33 0.5 0.67'
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
generate_output = 'stress_xx stress_yy'
[../]
[]
[Functions]
[./pressure]
type = PiecewiseLinear
x = '0 1.0 2.0'
y = '0 500 1000'
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
boundary = 0
variable = disp_y
value = 0.0
[../]
[./top_y]
type = DirichletBC
boundary = 2
variable = disp_y
value = 0.0
[../]
[./bottom_x]
type = DirichletBC
boundary = 0
variable = disp_x
value = 0.0
[../]
[]
[DiracKernels]
[./pressure_x]
type = XFEMPressure
variable = disp_x
component = 0
function = pressure
[../]
[./pressure_y]
type = XFEMPressure
variable = disp_y
component = 1
function = pressure
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 2e-12
# time control
start_time = 0.0
dt = 1
end_time = 2
[]
[Outputs]
file_base = inclined_edge_2d_pressure_out
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_3/plane3_mu_0_2_pen.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane3_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x11]
type = NodalVariableValue
nodeid = 10
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y11]
type = NodalVariableValue
nodeid = 10
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = plane3_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = plane3_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x11 disp_y11 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/thermal_hydraulics/test/tests/components/gate_valve_1phase/gate_valve_1phase.i)
# This input file is used to test the gate valve component.
# This problem consists of a T junction of 3 pipes. The inlet pipe is one of the
# 2 pipes of the "top" of the T. The other 2 pipes each have a gate valve.
# Initially, one of the 2 outlet pipes has an open valve and the other has a
# closed valve. Later in the transient, the valves gradually open/close to switch
# the outlet flow direction.
p = 1.0e5
T = 300.0
rho = 1.161430436 # @ 1e5 Pa, 300 K
D = 0.1
A = ${fparse pi * D^2 / 4.0}
V_junction = ${fparse pi * D^3 / 4.0}
vel_in = 2.0
m_dot = ${fparse rho * vel_in * A}
t_begin = 0.3
delta_t_open = 0.1
[GlobalParams]
gravity_vector = '0 0 0'
closures = simple_closures
fp = fp
f = 0.0
initial_T = ${T}
initial_p = ${p}
initial_vel = 0
[]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
gamma = 1.4
molar_mass = 0.02897
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Functions]
[pipe3_open_fn]
type = TimeRampFunction
initial_value = 1
final_value = 0
initial_time = ${t_begin}
ramp_duration = ${delta_t_open}
[]
[pipe2_open_fn]
type = ParsedFunction
expression = '1 - pipe3_phi'
symbol_names = 'pipe3_phi'
symbol_values = 'pipe3_open_fn'
[]
[]
[Components]
[inlet]
type = InletMassFlowRateTemperature1Phase
input = 'pipe1:in'
m_dot = ${m_dot}
T = ${T}
[]
[pipe1]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1.0
n_elems = 50
A = ${A}
[]
[volume_junction]
type = VolumeJunction1Phase
position = '1 0 0'
connections = 'pipe1:out pipe2A:in pipe3A:in'
volume = ${V_junction}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
[]
[pipe2A]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '0 1 0'
length = 0.5
n_elems = 25
A = ${A}
[]
[pipe2_valve]
type = GateValve1Phase
connections = 'pipe2A:out pipe2B:in'
open_area_fraction = 0 # (controlled via 'pipe2_valve_control')
[]
[pipe2B]
type = FlowChannel1Phase
position = '1 0.5 0'
orientation = '0 1 0'
length = 0.5
n_elems = 25
A = ${A}
[]
[pipe2_outlet]
type = Outlet1Phase
input = 'pipe2B:out'
p = ${p}
[]
[pipe3A]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '1 0 0'
length = 0.5
n_elems = 25
A = ${A}
[]
[pipe3_valve]
type = GateValve1Phase
connections = 'pipe3A:out pipe3B:in'
open_area_fraction = 0 # (controlled via 'pipe3_valve_control')
[]
[pipe3B]
type = FlowChannel1Phase
position = '1.5 0 0'
orientation = '1 0 0'
length = 0.5
n_elems = 25
A = ${A}
[]
[pipe3_outlet]
type = Outlet1Phase
input = 'pipe3B:out'
p = ${p}
[]
[]
[ControlLogic]
[pipe2_valve_control]
type = TimeFunctionComponentControl
component = pipe2_valve
parameter = open_area_fraction
function = pipe2_open_fn
[]
[pipe3_valve_control]
type = TimeFunctionComponentControl
component = pipe3_valve
parameter = open_area_fraction
function = pipe3_open_fn
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = bdf2
solve_type = PJFNK
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 20
l_tol = 1e-4
start_time = 0.0
end_time = 1.0
dt = 0.01
abort_on_solve_fail = true
[]
[Outputs]
exodus = true
show = 'p T vel'
velocity_as_vector = false
print_linear_residuals = false
[console]
type = Console
max_rows = 1
[]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_htonly/sphere2DRZ.i)
#
# 2DRZ Spherical Gap Heat Transfer Test.
#
# This test exercises 2D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid sphere of radius = 1 unit, and outer
# hollow sphere with an inner radius of 2. In other words, the gap between
# them is 1 radial unit in length.
#
# The conductivity of both spheres is set very large to achieve a uniform
# temperature in each sphere. The temperature of the center node of the
# inner sphere is ramped from 100 to 200 over one time unit. The
# temperature of the outside of the outer, hollow sphere is held fixed
# at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer spheres:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r^2*((1/r1)-(1/r2)))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 4 * pi * 1^2 (4*pi*r^2)
#
# The integrated heat flux across the gap at time 1 is then:
#
# 4*pi*k*delta_T/((1/r1)-(1/r2))
# 4*pi*1*100/((1/1) - (1/2)) = 2513.3 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/2 of the spheres is meshed
# As such, the integrated flux from the post processors is 1/2 of the total,
# or 1256.6 watts... i.e. 400*pi.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
file = cyl2D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 1
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(modules/phase_field/examples/rigidbodymotion/AC_CH_Multigrain.i)
# Tests the rigid body motion due to applied force of multiple particles.
# ***COPY AND PASTE THESE AS NEEDED***
# 'gr0 gr1 gr2 gr3 gr4 gr5 gr6 gr7 gr8 gr9 gr10 gr11 gr12 gr13 gr14 gr15 gr16 gr17 gr18 gr19'
# (gr0^2+gr1^2+gr2^2+gr3^2+gr4^2+gr5^2+gr6^2+gr7^2+gr8^2+gr9^2+gr10^2+gr11^2+gr12^2+gr13^2+gr14^2+gr15^2+gr16^2+gr17^2+gr18^2+gr19^2)
# (gr0^3+gr1^3+gr2^3+gr3^3+gr4^3+gr5^3+gr6^3+gr7^3+gr8^3+gr9^3+gr10^3+gr11^3+gr12^3+gr13^3+gr14^3+gr15^3+gr16^3+gr17^3+gr18^3+gr19^3)
[GlobalParams]
op_num = 4
var_name_base = gr
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
xmin = 0
xmax = 600
ymin = 0
ymax = 600
elem_type = QUAD4
uniform_refine = 1
[]
[Variables]
[./c]
[../]
[./w]
[../]
[./PolycrystalVariables] # Automatically creates order parameter variables
[../]
[]
[AuxVariables]
[./bnds]
[../]
[./force]
order = CONSTANT
family = MONOMIAL
[../]
[./free_energy]
order = CONSTANT
family = MONOMIAL
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./var_indices]
order = CONSTANT
family = MONOMIAL
[../]
[./centroids]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./load_x]
# Defines the force on the grains in the x-direction
type = ParsedFunction
expression = 0.005*cos(x*pi/600)
[../]
[./load_y]
# Defines the force on the grains in the y-direction
type = ConstantFunction
value = 0.002
[../]
[]
[Kernels]
[./RigidBodyMultiKernel]
# Creates all of the necessary Allen Cahn kernels automatically
c = c
f_name = f_loc
mob_name = L
kappa_name = kappa_gr
grain_force = grain_force
grain_volumes = grain_volumes
grain_tracker_object = grain_center
[../]
# Cahn Hilliard kernels
[./dt_w]
type = CoupledTimeDerivative
variable = w
v = c
[../]
[./CH_wres]
type = SplitCHWRes
variable = w
mob_name = M
[../]
[./CH_Parsed]
type = SplitCHParsed
variable = c
f_name = f_loc
w = w
kappa_name = kappa_c
coupled_variables = 'gr0 gr1 gr2 gr3' # Must be changed as op_num changes. Copy/paste from line 4
[../]
[./CH_RBM]
type = MultiGrainRigidBodyMotion
variable = w
c = c
v = 'gr0 gr1 gr2 gr3'
grain_force = grain_force
grain_volumes = grain_volumes
grain_tracker_object = grain_center
[../]
[]
[AuxKernels]
[./force_x]
type = FunctionAux
variable = force
function = load_x
[../]
[./force_y]
type = FunctionAux
variable = force
function = load_y
[../]
[./energy_density]
type = TotalFreeEnergy
variable = free_energy
f_name = f_loc
kappa_names = kappa_c
interfacial_vars = c
[../]
[./bnds]
type = BndsCalcAux
variable = bnds
[../]
[]
[BCs]
[./bcs]
#zero flux BC
type = NeumannBC
value = 0
variable = c
boundary = '0 1 2 3'
[../]
[]
[Materials]
[./constants]
type = GenericConstantMaterial
prop_names = 'kappa_gr kappa_c M L'
prop_values = '250 4000 4.5 60'
[../]
[./free_energy]
type = DerivativeParsedMaterial
property_name = f_loc
constant_names = 'A B'
constant_expressions = '450 1.5'
coupled_variables = 'c gr0 gr1 gr2 gr3' #Must be changed as op_num changes. Copy/paste from line 4
expression = 'A*c^2*(1-c)^2+B*(c^2+6*(1-c)*(gr0^2+gr1^2+gr2^2+gr3^2)
-4*(2-c)*(gr0^3+gr1^3+gr2^3+gr3^3)
+3*(gr0^2+gr1^2+gr2^2+gr3^2)^2)'
#Copy/paste from lines 5-6
derivative_order = 2
[../]
[./force_density]
type = ExternalForceDensityMaterial
c = c
k = 10.0
force_x = load_x
force_y = load_y
[../]
[]
[Postprocessors]
[./total_energy]
type = ElementIntegralVariablePostprocessor
variable = free_energy
execute_on = 'initial timestep_end'
[../]
[]
[VectorPostprocessors]
[./forces]
type = GrainForcesPostprocessor
grain_force = grain_force
[../]
[./grain_volumes]
type = FeatureVolumeVectorPostprocessor
flood_counter = grain_center
execute_on = 'initial timestep_begin'
[../]
[]
[UserObjects]
[./grain_center]
type = GrainTracker
outputs = none
compute_var_to_feature_map = true
execute_on = 'initial timestep_begin'
[../]
[./grain_force]
type = ComputeExternalGrainForceAndTorque
grain_data = grain_center
c = c
etas = 'gr0 gr1 gr2 gr3'
force_density = force_density_ext
execute_on = 'linear nonlinear'
[../]
[]
[Preconditioning]
[./coupled]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
scheme = bdf2
solve_type = NEWTON
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type
-sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly
ilu 2'
l_tol = 1e-05
nl_max_its = 30
l_max_its = 30
nl_rel_tol = 1e-07
nl_abs_tol = 1e-09
start_time = 0.0
end_time = 4
dt = 0.05
[]
[Outputs]
exodus = true
perf_graph = true
[./display]
type = Console
max_rows = 12
[../]
[]
[ICs]
[./concentration_IC]
type = SpecifiedSmoothCircleIC
x_positions = '150 450 150 450'
y_positions = '150 150 450 450'
z_positions = '0 0 0 0'
radii = '120 120 120 120'
variable = c
invalue = 1.0
outvalue = 0.0
int_width = 25
[../]
[./gr0_IC]
type = SmoothCircleIC
variable = gr0
x1 = 150
y1 = 150
radius = 120
invalue = 1.0
outvalue = 0.0
int_width = 25
[../]
[./gr1_IC]
type = SmoothCircleIC
variable = gr1
x1 = 450
y1 = 150
radius = 120
invalue = 1.0
outvalue = 0.0
int_width = 25
[../]
[./gr2_IC]
type = SmoothCircleIC
variable = gr2
x1 = 150
y1 = 450
radius = 120
invalue = 1.0
outvalue = 0.0
int_width = 25
[../]
[./gr3_IC]
type = SmoothCircleIC
variable = gr3
x1 = 450
y1 = 450
radius = 120
invalue = 1.0
outvalue = 0.0
int_width = 25
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/propagating_2field_1constraint.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = Diffusion
variable = v
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = 3
value = 1
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/multiapps/multilevel/time_dt_from_parent_sub.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
xmax = 100
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./td]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 1
dt = 1
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
[./console]
type = Console
output_file = true
[../]
[]
[MultiApps]
[./sub]
type = TransientMultiApp
app_type = MooseTestApp
positions = '0 0 0 0.5 0.5 0'
input_files = time_dt_from_parent_subsub.i
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_sphere3D.i)
sphere_outer_htc = 10 # W/m^2/K
sphere_outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = sphere3D.e
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[]
[AuxVariables]
[gap_conductance]
order = CONSTANT
family = MONOMIAL
[]
[power_density]
block = 'fuel'
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
[]
[heat_source]
type = CoupledForce
variable = temp
block = 'fuel'
v = power_density
[]
[]
[AuxKernels]
[gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[ThermalContact]
[thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 5
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = '4' # outer RPV
coefficient = ${sphere_outer_htc}
T_infinity = ${sphere_outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[Quadrature]
order = fifth
side_order = seventh
[]
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 'fuel'
[]
[sphere_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = '4' # outer RVP
T_fluid = ${sphere_outer_Tinf}
htc = ${sphere_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(sphere_convective_out - ptot) / ptot'
pp_names = 'sphere_convective_out ptot'
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '2 3'
variable = temp
[]
[]
(tutorials/darcy_thermo_mech/step10_multiapps/tests/auxkernels/corrosion/corrosion.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
ymax = 0.1
xmax = 0.1
[]
uniform_refine = 0
[]
[Adaptivity]
max_h_level = 3
initial_steps = 5
cycles_per_step = 2
initial_marker = error_marker
marker = error_marker
[Indicators]
[phi_jump]
type = GradientJumpIndicator
variable = phi
[]
[]
[Markers]
[error_marker]
type = ErrorFractionMarker
indicator = phi_jump
refine = 0.9
[]
[]
[]
[Variables]
[temperature]
initial_condition = 300
[]
[]
[AuxVariables]
[phi]
[]
[]
[AuxKernels]
[corrosion]
type = RandomCorrosion
execute_on = 'timestep_end'
variable = phi
reference_temperature = 300
temperature = 301
[]
[]
[Kernels]
[heat_conduction]
type = ADHeatConduction
variable = temperature
[]
[]
[BCs]
[left]
type = PostprocessorDirichletBC
variable = temperature
boundary = left
postprocessor = 301
[]
[right]
type = NeumannBC
variable = temperature
boundary = right
value = 100 # prescribed flux
[]
[]
[Materials]
[column]
type = PackedColumn
temperature = temperature
radius = 1 # mm
phase = phi
outputs = exodus
output_properties = porosity
[]
[]
[Problem]
type = FEProblem
[]
[Postprocessors]
[k_eff]
type = ThermalConductivity
variable = temperature
T_hot = 301
flux = 100
dx = 0.1
boundary = right
length_scale = 1
[]
[]
[Executioner]
type = Transient
num_steps = 5
dt = 0.5
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'initial timestep_end'
exodus = true
[console]
type = Console
execute_postprocessors_on = 'timestep_begin timestep_end'
[]
[]
[ICs]
[close_pack]
radius = 0.01
outvalue = 0 # water
variable = phi
invalue = 1 #steel
type = ClosePackIC
[]
[]
(test/tests/markers/two_circle_marker/two_circle_marker_coarsen.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.02
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./Periodic]
[./all]
variable = u
auto_direction = 'x y'
[../]
[../]
[]
[Executioner]
type = Transient
num_steps = 6
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Adaptivity]
initial_steps = 1
initial_marker = two_circle_marker
cycles_per_step = 1
marker = two_circle_marker
max_h_level = 1
[./Markers]
[./two_circle_marker]
type = TwoCircleMarker
point1 = '0.5 0.5 0'
radius1 = 0.3
point2 = '0.35 0.25 0'
radius2 = 0.3
shut_off_time = 0.15
inside = refine
outside = coarsen
[../]
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
print_mesh_changed_info = true
[../]
[]
(test/tests/problems/eigen_problem/eigensolvers/gipm.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 100
ymin = 0
ymax = 100
elem_type = QUAD4
nx = 64
ny = 64
displacements = 'x_disp y_disp'
[]
#The minimum eigenvalue for this problem is 2*(pi/a)^2 + 2 with a = 100.
#Its inverse will be 0.49950700634518.
[Variables]
[./u]
order = first
family = LAGRANGE
[../]
[]
[AuxVariables]
[./x_disp]
[../]
[./y_disp]
[../]
[]
[AuxKernels]
[./x_disp]
type = FunctionAux
variable = x_disp
function = x_disp_func
[../]
[./y_disp]
type = FunctionAux
variable = y_disp
function = y_disp_func
[../]
[]
[Functions]
[./x_disp_func]
type = ParsedFunction
expression = 0
[../]
[./y_disp_func]
type = ParsedFunction
expression = 0
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
use_displaced_mesh = true
[../]
[./rea]
type = CoefReaction
variable = u
coefficient = 2.0
use_displaced_mesh = true
[../]
[./rhs]
type = CoefReaction
variable = u
coefficient = -1.0
use_displaced_mesh = true
extra_vector_tags = 'eigen'
[../]
[]
[BCs]
[./homogeneous]
type = DirichletBC
variable = u
boundary = '0 1 2 3'
value = 0
use_displaced_mesh = true
[../]
[./eigen_bc]
type = EigenDirichletBC
variable = u
boundary = '0 1 2 3'
use_displaced_mesh = true
[../]
[]
[Executioner]
type = Eigenvalue
eigen_problem_type = gen_non_hermitian
which_eigen_pairs = SMALLEST_MAGNITUDE
n_eigen_pairs = 1
n_basis_vectors = 18
solve_type = jacobi_davidson
petsc_options = '-eps_view'
[]
[VectorPostprocessors]
[./eigenvalues]
type = Eigenvalues
execute_on = 'timestep_end'
[../]
[]
[Outputs]
csv = true
execute_on = 'timestep_end'
[./console]
type = Console
outlier_variable_norms = false
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/edge_crack_3d_mhs.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.2
elem_type = HEX8
[]
[UserObjects]
[./cut_mesh]
type = CrackMeshCut3DUserObject
mesh_file = mesh_edge_crack.xda
growth_dir_method = MAX_HOOP_STRESS
size_control = 1
n_step_growth = 1
growth_rate = growth_func_v
crack_front_nodes = '7 6 5 4'
[../]
[]
[Functions]
[./growth_func_v]
type = ParsedFunction
expression = 0.15
[../]
[]
[DomainIntegral]
integrals = 'Jintegral InteractionIntegralKI InteractionIntegralKII'
displacements = 'disp_x disp_y disp_z'
crack_front_points_provider = cut_mesh
number_points_from_provider = 4
crack_direction_method = CurvedCrackFront
radius_inner = '0.15'
radius_outer = '0.45'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
incremental = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[Functions]
[./top_trac_x]
type = ConstantFunction
value = 100
[../]
[./top_trac_y]
type = ConstantFunction
value = 0
[../]
[]
[BCs]
[./top_x]
type = FunctionNeumannBC
boundary = top
variable = disp_x
function = top_trac_x
[../]
[./top_y]
type = FunctionNeumannBC
boundary = top
variable = disp_y
function = top_trac_y
[../]
[./bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = bottom
variable = disp_z
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-12
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 4.0
max_xfem_update = 1
[]
[Outputs]
file_base = edge_crack_3d_mhs_out
execute_on = 'timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/single_var_constraint_2d/propagating_1field.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
time_start_cut = 0.0
time_end_cut = 2.0
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = 0
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/single_var_constraint_3d/stationary_jump_fluxjump_3d.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 3
nx = 5
ny = 5
nz = 2
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
zmin = 0.0
zmax = 0.25
elem_type = HEX8
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./square_planar_cut_uo]
type = RectangleCutUserObject
cut_data = ' 0.5 -0.001 -0.001
0.5 1.001 -0.001
0.5 1.001 1.001
0.5 -0.001 1.001'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0.5
jump_flux = 1
geometric_cut_userobject = 'square_planar_cut_uo'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/1D_rz_homog1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: quasi-1D
# Coordinate System: rz
# Material Numbers/Types: homogeneous 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed level set function
# Description:
# A simple transient heat transfer problem in cylindrical coordinates designed
# with the Method of Manufactured Solutions. This problem was developed to
# verify XFEM performance in the presence of a moving interface for linear
# element models that can be exactly evaluated by FEM/Moose. Both the
# temperature solution and level set function are designed to be linear to
# attempt to minimize error between the Moose/exact solution and XFEM results.
# Thermal conductivity is a single, constant value at all points in the system.
# Results:
# The temperature at the left boundary (x=1) exhibits the largest difference
# between the FEM/Moose solution and XFEM results. We present the XFEM results
# at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 480.0008118
# 0.6 520 520.0038529
# 0.8 560 560.0089177
# 1.0 600 600.0133344
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Problem]
coord_type = RZ
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 1
xmin = 1.0
xmax = 2.0
ymin = 0.0
ymax = 0.5
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-200*x+400) + 200*1.5*t/x'
[../]
[./neumann_func]
type = ParsedFunction
expression = '1.5*200*t'
[../]
[./ls_func]
type = ParsedFunction
expression = '2.04 - x - 0.2*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericConstantMaterial
prop_names = 'diffusion_coefficient'
prop_values = 1.5
[../]
[]
[BCs]
[./left_u]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 'right'
value = 400
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/sliding_block/sliding/frictional_02_penalty.i)
# This is a benchmark test that checks constraint based frictional
# contact using the penalty method. In this test a constant
# displacement is applied in the horizontal direction to simulate
# a small block come sliding down a larger block.
#
# A friction coefficient of 0.2 is used. The gold file is run on one processor
# and the benchmark case is run on a minimum of 4 processors to ensure no
# parallel variability in the contact pressure and penetration results.
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[penetration]
[]
[inc_slip_x]
[]
[inc_slip_y]
[]
[accum_slip_x]
[]
[accum_slip_y]
[]
[]
[Functions]
[vertical_movement]
type = ParsedFunction
expression = -t
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
[]
[]
[AuxKernels]
[zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[]
[accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[]
[penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[]
[]
[Postprocessors]
[nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[]
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[]
[]
[BCs]
[left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[]
[left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[]
[right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[]
[]
[Materials]
[left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[]
[stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Outputs]
time_step_interval = 10
[out]
type = Exodus
elemental_as_nodal = true
[]
[console]
type = Console
max_rows = 5
[]
[]
[Contact]
[leftright]
secondary = 3
primary = 2
model = coulomb
penalty = 4e+6
friction_coefficient = 0.2
formulation = penalty
normal_smoothing_distance = 0.1
[]
[]
(modules/contact/test/tests/mechanical_constraint/frictionless_kinematic_gap_offsets.i)
# this test is the same as frictionless_kinematic test but designed to test the gap offset capability
# gap offsets with value of 0.01 were introduced to both primary and secondary sides in the initial mesh
# these values were accounted using the gap offset capability to produce the same result as if no gap offsets were introduced
[Mesh]
file = blocks_2d_gap_offset.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./primary_gap_offset]
[../]
[./secondary_gap_offset]
[../]
[./mapped_primary_gap_offset]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./primary_gap_offset]
type = ConstantAux
variable = primary_gap_offset
value = -0.01
boundary = 2
[../]
[./mapped_primary_gap_offset]
type = GapValueAux
variable = mapped_primary_gap_offset
paired_variable = primary_gap_offset
boundary = 3
paired_boundary = 2
[../]
[./secondary_gap_offset]
type = ConstantAux
variable = secondary_gap_offset
value = -0.01
boundary = 3
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = 1
poissons_ratio = 0.3
youngs_modulus = 1e7
[../]
[./right]
type = ComputeIsotropicElasticityTensor
block = 2
poissons_ratio = 0.3
youngs_modulus = 1e6
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.01
end_time = 0.10
num_steps = 1000
l_tol = 1e-6
nl_rel_tol = 1e-10
nl_abs_tol = 1e-8
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
file_base = frictionless_kinematic_gap_offsets_out
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = frictionless
penalty = 1e+6
secondary_gap_offset = secondary_gap_offset
mapped_primary_gap_offset = mapped_primary_gap_offset
[../]
[]
(modules/richards/test/tests/buckley_leverett/bl20_lumped.i)
# two-phase version
[Mesh]
type = GeneratedMesh
dim = 1
nx = 30
xmin = 0
xmax = 15
[]
[GlobalParams]
richardsVarNames_UO = PPNames
density_UO = 'DensityWater DensityGas'
relperm_UO = 'RelPermWater RelPermGas'
SUPG_UO = 'SUPGwater SUPGgas'
sat_UO = 'SatWater SatGas'
seff_UO = 'SeffWater SeffGas'
[]
[Functions]
[./dts]
type = PiecewiseLinear
y = '0.1 0.5 0.5 1 2 4'
x = '0 0.1 1 5 40 42'
[../]
[]
[UserObjects]
[./PPNames]
type = RichardsVarNames
richards_vars = 'pwater pgas'
[../]
[./DensityWater]
type = RichardsDensityConstBulk
dens0 = 1000
bulk_mod = 2E6
[../]
[./DensityGas]
type = RichardsDensityConstBulk
dens0 = 1
bulk_mod = 2E6
[../]
[./SeffWater]
type = RichardsSeff2waterVG
m = 0.8
al = 1E-5
[../]
[./SeffGas]
type = RichardsSeff2gasVG
m = 0.8
al = 1E-5
[../]
[./RelPermWater]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./RelPermGas]
type = RichardsRelPermPower
simm = 0.0
n = 2
[../]
[./SatWater]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SatGas]
type = RichardsSat
s_res = 0.0
sum_s_res = 0.0
[../]
[./SUPGwater]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[./SUPGgas]
type = RichardsSUPGstandard
p_SUPG = 1E-5
[../]
[]
[Variables]
[./pwater]
order = FIRST
family = LAGRANGE
[../]
[./pgas]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./w_aux_seff]
[../]
[]
[Kernels]
[./richardstwater]
type = RichardsLumpedMassChange
variable = pwater
[../]
[./richardsfwater]
type = RichardsFlux
variable = pwater
[../]
[./richardstgas]
type = RichardsLumpedMassChange
variable = pgas
[../]
[./richardsfgas]
type = RichardsFlux
variable = pgas
[../]
[]
[AuxKernels]
[./w_aux_seff_auxk]
type = RichardsSeffAux
seff_UO = SeffWater
pressure_vars = 'pwater pgas'
variable = w_aux_seff
[../]
[]
[ICs]
[./water_ic]
type = FunctionIC
variable = pwater
function = initial_water
[../]
[./gas_ic]
type = FunctionIC
variable = pgas
function = initial_gas
[../]
[]
[BCs]
[./left_w]
type = DirichletBC
variable = pwater
boundary = left
value = 1E6
[../]
[./left_g]
type = DirichletBC
variable = pgas
boundary = left
value = 1000
[../]
[./right_w]
type = DirichletBC
variable = pwater
boundary = right
value = -300000
[../]
[./right_g]
type = DirichletBC
variable = pgas
boundary = right
value = 0
[../]
[]
[Functions]
[./initial_water]
type = ParsedFunction
expression = 1000000*(1-min(x/5,1))-if(x<5,0,300000)
[../]
[./initial_gas]
type = ParsedFunction
expression = 1000
[../]
[]
[Materials]
[./rock]
type = RichardsMaterial
block = 0
mat_porosity = 0.15
mat_permeability = '1E-10 0 0 0 1E-10 0 0 0 1E-10'
viscosity = '1E-3 1E-6'
gravity = '0 0 0'
linear_shape_fcns = true
[../]
[]
[Preconditioning]
active = 'standard'
[./bounded]
# must use --use-petsc-dm command line argument
type = SMP
full = true
petsc_options_iname = '-snes_type -pc_factor_shift_type'
petsc_options_value = 'vinewtonssls nonzero'
[../]
[./standard]
type = SMP
full = true
petsc_options_iname = '-pc_factor_shift_type'
petsc_options_value = 'nonzero'
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
end_time = 50
nl_rel_tol = 1.e-9
nl_max_its = 10
[./TimeStepper]
type = FunctionDT
function = dts
[../]
[]
[Outputs]
file_base = bl20_lumped
execute_on = 'initial timestep_end final'
time_step_interval = 100000
exodus = true
hide = pgas
[./console_out]
type = Console
time_step_interval = 1
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/penny_crack.i)
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
volumetric_locking_correction = true
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
file = quarter_sym.e
[]
[UserObjects]
[./circle_cut_uo]
type = CircleCutUserObject
cut_data = '-0.5 -0.5 0
0.0 -0.5 0
-0.5 0 0'
[../]
[]
[AuxVariables]
[./SED]
order = CONSTANT
family = MONOMIAL
[../]
[]
[DomainIntegral]
integrals = 'Jintegral'
crack_front_points = '-0.5 0.0 0.0
-0.25 -0.07 0
-0.15 -0.15 0
-0.07 -0.25 0
0 -0.5 0'
crack_end_direction_method = CrackDirectionVector
crack_direction_vector_end_1 = '0 1 0'
crack_direction_vector_end_2 = '1 0 0'
crack_direction_method = CurvedCrackFront
intersecting_boundary = '3 4' #It would be ideal to use this, but can't use with XFEM yet
radius_inner = '0.3'
radius_outer = '0.6'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 1
incremental = true
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
[../]
[]
[AuxKernels]
[./SED]
type = MaterialRealAux
variable = SED
property = strain_energy_density
execute_on = timestep_end
block = 1
[../]
[]
[Functions]
[./top_trac_z]
type = ConstantFunction
value = 10
[../]
[]
[BCs]
[./top_z]
type = FunctionNeumannBC
boundary = 2
variable = disp_z
function = top_trac_z
[../]
[./bottom_x]
type = DirichletBC
boundary = 1
variable = disp_x
value = 0.0
[../]
[./bottom_y]
type = DirichletBC
boundary = 1
variable = disp_y
value = 0.0
[../]
[./bottom_z]
type = DirichletBC
boundary = 1
variable = disp_z
value = 0.0
[../]
[./sym_y]
type = DirichletBC
boundary = 3
variable = disp_y
value = 0.0
[../]
[./sym_x]
type = DirichletBC
boundary = 4
variable = disp_x
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
# time control
start_time = 0.0
dt = 1.0
end_time = 1.0
[]
[Outputs]
file_base = penny_crack_out
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/overclosure_removal/overclosure.i)
# ---------------------------------------------------------------------------------------------------------
# REGRESSION TEST FOR OVERCLOSURE REMOVAL
# =======================================
# THIS TEST DEMONSTRATES THAT THE CODE IS CAPABLE OF REMOVING A SIZEABLE OVERCLOSURE IN A SINGLE TIME-STEP
# --------------------------------------------------------------------------------------------------------
[Mesh]
file = oc_mesh.e
[]
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./penetration]
order = FIRST
family = LAGRANGE
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
use_finite_deform_jacobian = true
[../]
[]
[AuxKernels]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./_dt]
type = TimestepSize
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side1_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = 5
value = 0.0
[../]
[./top_x]
type = DirichletBC
variable = disp_x
boundary = 1001 #nodeset 1001 top central node
value = 0.0
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeFiniteStrain
decomposition_method = EigenSolution
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e5
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeFiniteStrain
decomposition_method = EigenSolution
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-8
nl_rel_tol = 1e-9
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
dtmin = 1.0
l_tol = 1e-3
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
secondary = 4
primary = 3
model = frictionless
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(test/tests/time_integrators/actually_explicit_euler_verification/ee-1d-quadratic.i)
[Mesh]
type = GeneratedMesh
dim = 1
xmin = -1
xmax = 1
nx = 20
elem_type = EDGE3
[]
[Functions]
[./ic]
type = ParsedFunction
expression = 0
[../]
[./forcing_fn]
type = ParsedFunction
expression = x*x-2*t
[../]
[./exact_fn]
type = ParsedFunction
expression = t*x*x
[../]
[]
[Variables]
[./u]
order = SECOND
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = ic
[../]
[../]
[]
[Kernels]
[./ie]
type = TimeDerivative
variable = u
[../]
[./diff]
type = Diffusion
variable = u
[../]
[./ffn]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[BCs]
[./all]
type = FunctionDirichletBC
variable = u
preset = false
boundary = '0 1'
function = exact_fn
[../]
[]
[Postprocessors]
[./l2_err]
type = ElementL2Error
variable = u
function = exact_fn
[../]
[]
[Executioner]
type = Transient
l_tol = 1e-12
start_time = 0.0
num_steps = 20
dt = 0.00005
[./TimeIntegrator]
type = ActuallyExplicitEuler
[../]
[]
[Outputs]
exodus = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/contact/test/tests/frictional/single_point_2d/single_point_2d_predictor.i)
[Mesh]
file = single_point_2d.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = false
[]
[AuxVariables]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./horizontal_movement]
type = ParsedFunction
expression = t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
diag_save_in = 'diag_saved_x diag_saved_y'
[../]
[]
[AuxKernels]
[./incslip_x]
type = PenetrationAux
variable = inc_slip_x
quantity = incremental_slip_x
boundary = 3
paired_boundary = 2
[../]
[./incslip_y]
type = PenetrationAux
variable = inc_slip_y
quantity = incremental_slip_y
boundary = 3
paired_boundary = 2
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[BCs]
[./botx]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./boty]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./botx2]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./boty2]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[../]
[./topy]
type = DirichletBC
variable = disp_y
boundary = 4
value = -0.005
[../]
[]
[Materials]
[./bottom]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1.0e9
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[./top]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1.0e6
poissons_ratio = 0.3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 4
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 4
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 200
dt = 0.001
end_time = 0.01
num_steps = 1000
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
dtmin = 0.001
l_tol = 1e-3
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
exodus = true
print_linear_residuals = true
perf_graph = true
[./console]
type = Console
max_rows = 5
[../]
[]
[Contact]
[./leftright]
primary = 2
secondary = 3
model = coulomb
friction_coefficient = '0.25'
[../]
[]
[Dampers]
[./contact_slip]
type = ContactSlipDamper
primary = '2'
secondary = '3'
[../]
[]
(modules/phase_field/tutorials/spinodal_decomposition/s4_mobility.i)
#
# Example simulation of an iron-chromium alloy at 500 C. Equilibrium
# concentrations are at 23.6 and 82.3 mol% Cr. Kappa value, free energy equation,
# and mobility equation were provided by Lars Hoglund. Solved using the split
# form of the Cahn-Hilliard equation.
#
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
nx = 25
ny = 25
nz = 0
xmin = 0
xmax = 25
ymin = 0
ymax = 25
zmin = 0
zmax = 0
uniform_refine = 2
[]
[Variables]
[./c] # Mole fraction of Cr (unitless)
order = FIRST
family = LAGRANGE
[../]
[./w] # Chemical potential (eV/mol)
order = FIRST
family = LAGRANGE
[../]
[]
[ICs]
[./concentrationIC] # 46.774 mol% Cr with variations
type = RandomIC
min = 0.44774
max = 0.48774
seed = 210
variable = c
[../]
[]
[BCs]
[./Periodic]
[./c_bcs]
auto_direction = 'x y'
[../]
[../]
[]
[Kernels]
[./w_dot]
variable = w
v = c
type = CoupledTimeDerivative
[../]
[./coupled_res]
variable = w
type = SplitCHWRes
mob_name = M
[../]
[./coupled_parsed]
variable = c
type = SplitCHParsed
f_name = f_loc
kappa_name = kappa_c
w = w
[../]
[]
[Materials]
# d is a scaling factor that makes it easier for the solution to converge
# without changing the results. It is defined in each of the first three
# materials and must have the same value in each one.
[./kappa] # Gradient energy coefficient (eV nm^2/mol)
type = GenericFunctionMaterial
prop_names = 'kappa_c'
prop_values = '8.125e-16*6.24150934e+18*1e+09^2*1e-27'
# kappa_c *eV_J*nm_m^2* d
[../]
[./mobility] # Mobility (nm^2 mol/eV/s)
# NOTE: This is a fitted equation, so only 'Conv' has units
type = DerivativeParsedMaterial
property_name = M
coupled_variables = c
constant_names = 'Acr Bcr Ccr Dcr
Ecr Fcr Gcr
Afe Bfe Cfe Dfe
Efe Ffe Gfe
nm_m eV_J d'
constant_expressions = '-32.770969 -25.8186669 -3.29612744 17.669757
37.6197853 20.6941796 10.8095813
-31.687117 -26.0291774 0.2286581 24.3633544
44.3334237 8.72990497 20.956768
1e+09 6.24150934e+18 1e-27'
expression = 'nm_m^2/eV_J/d*((1-c)^2*c*10^
(Acr*c+Bcr*(1-c)+Ccr*c*log(c)+Dcr*(1-c)*log(1-c)+
Ecr*c*(1-c)+Fcr*c*(1-c)*(2*c-1)+Gcr*c*(1-c)*(2*c-1)^2)
+c^2*(1-c)*10^
(Afe*c+Bfe*(1-c)+Cfe*c*log(c)+Dfe*(1-c)*log(1-c)+
Efe*c*(1-c)+Ffe*c*(1-c)*(2*c-1)+Gfe*c*(1-c)*(2*c-1)^2))'
derivative_order = 1
outputs = exodus
[../]
[./local_energy] # Local free energy function (eV/mol)
type = DerivativeParsedMaterial
property_name = f_loc
coupled_variables = c
constant_names = 'A B C D E F G eV_J d'
constant_expressions = '-2.446831e+04 -2.827533e+04 4.167994e+03 7.052907e+03
1.208993e+04 2.568625e+03 -2.354293e+03
6.24150934e+18 1e-27'
expression = 'eV_J*d*(A*c+B*(1-c)+C*c*log(c)+D*(1-c)*log(1-c)+
E*c*(1-c)+F*c*(1-c)*(2*c-1)+G*c*(1-c)*(2*c-1)^2)'
derivative_order = 2
[../]
[./precipitate_indicator] # Returns 1/625 if precipitate
type = ParsedMaterial
property_name = prec_indic
coupled_variables = c
expression = if(c>0.6,0.0016,0)
[../]
[]
[Postprocessors]
[./step_size] # Size of the time step
type = TimestepSize
[../]
[./iterations] # Number of iterations needed to converge timestep
type = NumNonlinearIterations
[../]
[./nodes] # Number of nodes in mesh
type = NumNodes
[../]
[./evaluations] # Cumulative residual calculations for simulation
type = NumResidualEvaluations
[../]
[./precipitate_area] # Fraction of surface devoted to precipitates
type = ElementIntegralMaterialProperty
mat_prop = prec_indic
[../]
[./active_time] # Time computer spent on simulation
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[]
[Preconditioning]
[./coupled]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
l_max_its = 30
l_tol = 1e-6
nl_max_its = 50
nl_abs_tol = 1e-9
end_time = 604800 # 7 days
petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_ksp_type
-sub_pc_type -pc_asm_overlap'
petsc_options_value = 'asm 31 preonly
ilu 1'
[./TimeStepper]
type = IterationAdaptiveDT
dt = 10
cutback_factor = 0.8
growth_factor = 1.5
optimal_iterations = 7
[../]
[./Adaptivity]
coarsen_fraction = 0.1
refine_fraction = 0.7
max_h_level = 2
[../]
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
exodus = true
console = true
csv = true
[./console]
type = Console
max_rows = 10
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/large_gap_heat_transfer_test_sphere_mortar.i)
sphere_outer_htc = 10 # W/m^2/K
sphere_outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
coord_type = RZ
kernel_coverage_check = false
material_coverage_check = false
[]
[Mesh]
[file]
type = FileMeshGenerator
file = cyl2D.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '3'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
allow_renumbering = false
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[lm]
order = SECOND
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[AuxVariables]
[power_density]
block = 'fuel'
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
block = '1 2'
[]
[heat_source]
type = CoupledForce
variable = temp
block = 'fuel'
v = power_density
[]
[]
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 2
primary_emissivity = 0.0
secondary_emissivity = 0.0
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 2
gap_conductivity = 5.0
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
primary_boundary = 3
primary_subdomain = 10000
secondary_boundary = 2
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = '4' # outer RPV
coefficient = ${sphere_outer_htc}
T_infinity = ${sphere_outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '2 3'
variable = temp
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 'fuel'
[]
[sphere_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = '4' # outer RVP
T_fluid = ${sphere_outer_Tinf}
htc = ${sphere_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(sphere_convective_out - ptot) / ptot'
pp_names = 'sphere_convective_out ptot'
[]
[]
(modules/xfem/test/tests/moving_interface/moving_ad_bimaterial.i)
# This test is for two layer materials with different youngs modulus with AD
# The global stress is determined by switching the stress based on level set values
# The material interface is marked by a level set function
# The two layer materials are glued together
# This case is also meant to test for a bug in moving interfaces on displaced meshes
# It should fail during the healing step of the 2nd timestep if the bug is present.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Mesh]
displacements = 'disp_x disp_y'
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
[]
[./left_bottom]
type = ExtraNodesetGenerator
new_boundary = 'left_bottom'
coord = '0.0 0.0'
input = generated_mesh
[../]
[./left_top]
type = ExtraNodesetGenerator
new_boundary = 'left_top'
coord = '0.0 5.'
input = left_bottom
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'y-3.153 + t'
[../]
[]
[AuxVariables]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
use_automatic_differentiation = true
add_variables = true
generate_output = 'stress_xx stress_yy stress_xy'
[../]
[]
[AuxKernels]
[./a_strain_xx]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = ADDirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = ADDirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = ADFunctionDirichletBC
boundary = top
variable = disp_x
function = 0.03*t
[../]
[./topy]
type = ADFunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ADComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ADComputeSmallStrain
base_name = A
displacements = 'disp_x disp_y'
[../]
[./stress_A]
type = ADComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ADComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e7
poissons_ratio = 0.3
[../]
[./strain_B]
type = ADComputeSmallStrain
base_name = B
displacements = 'disp_x disp_y'
[../]
[./stress_B]
type = ADComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = ADLevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[./combined_elasticity_tensor]
type = ADLevelSetBiMaterialRankFour
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = elasticity_tensor
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'bt'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-8
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-50
# time control
start_time = 0.0
dt = 0.15
num_steps = 3
max_xfem_update = 1
[]
[Outputs]
exodus = true
execute_on = timestep_end
file_base = moving_bimaterial_out
perf_graph = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/xfem/test/tests/moving_interface/verification/1D_xy_homog1mat.i)
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
# XFEM Moving Interface Verification Problem
# Dimensionality: quasi-1D
# Coordinate System: xy
# Material Numbers/Types: homogeneous 1 material, 2 region
# Element Order: 1st
# Interface Characteristics: u independent, prescribed linear level set function
# Description:
# A simple transient heat transfer problem in Cartesian coordinates designed
# with the Method of Manufactured Solutions. This problem was developed to
# verify XFEM performance in the presence of a moving interface for linear
# element models that can be exactly evaluated by FEM/Moose. Both the
# temperature solution and level set function are designed to be linear to
# attempt to minimize error between the Moose/exact solution and XFEM results.
# Thermal conductivity is a single, constant value at all points in the system.
# Results:
# The temperature at the left boundary (x=0) exhibits the largest difference
# between the FEM/Moose solution and XFEM results. We present the XFEM results
# at this location with 10 digits of precision:
# Time Expected Temperature XFEM Calculated Temperature
# 0.2 440 440
# 0.4 480 480.0000064
# 0.6 520 520.0000323
# 0.8 560 560.0000896
# 1.0 600 600.0001870
# ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ #
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 4
ny = 1
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 0.5
elem_type = QUAD4
[]
[XFEM]
qrule = moment_fitting
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
heal_always = true
[../]
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./heat_cond]
type = MatDiffusion
variable = u
diffusivity = diffusion_coefficient
[../]
[./vol_heat_src]
type = BodyForce
variable = u
function = src_func
[../]
[./mat_time_deriv]
type = TestMatTimeDerivative
variable = u
mat_prop_value = rhoCp
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
geometric_cut_userobject = 'level_set_cut_uo'
use_penalty = true
alpha = 1e5
[../]
[]
[Functions]
[./src_func]
type = ParsedFunction
expression = '10*(-200*x+200)'
[../]
[./ls_func]
type = ParsedFunction
expression = '1-(x-0.04)-0.2*t'
[../]
[./neumann_func]
type = ParsedFunction
expression = '1.5*200*t'
[../]
[]
[Materials]
[./mat_time_deriv_prop]
type = GenericConstantMaterial
prop_names = 'rhoCp'
prop_values = 10
[../]
[./therm_cond_prop]
type = GenericConstantMaterial
prop_names = 'diffusion_coefficient'
prop_values = 1.5
[../]
[]
[BCs]
[./left_du]
type = FunctionNeumannBC
variable = u
boundary = 'left'
function = neumann_func
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 'right'
value = 400
[../]
[]
[ICs]
[./u_ic]
type = ConstantIC
value = 400
variable = u
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
line_search = 'none'
l_tol = 1.0e-6
nl_max_its = 15
nl_rel_tol = 1.0e-10
nl_abs_tol = 1.0e-9
start_time = 0.0
dt = 0.2
end_time = 1.0
max_xfem_update = 1
[]
[Outputs]
time_step_interval = 1
execute_on = 'initial timestep_end'
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_htonly/cyl3D.i)
#
# 3D Cylindrical Gap Heat Transfer Test.
#
# This test exercises 3D gap heat transfer for a constant conductivity gap.
#
# The mesh consists of an inner solid cylinder of radius = 1 unit, and outer
# hollow cylinder with an inner radius of 2. In other words, the gap between
# them is 1 radial unit in length.
#
# The conductivity of both cylinders is set very large to achieve a uniform
# temperature in each cylinder. The temperature of the center node of the
# inner cylinder is ramped from 100 to 200 over one time unit. The temperature
# of the outside of the outer, hollow cylinder is held fixed at 100.
#
# A simple analytical solution is possible for the integrated heat flux
# between the inner and outer cylinders:
#
# Integrated Flux = (T_left - T_right) * (gapK/(r*ln(r2/r1))) * Area
#
# For gapK = 1 (default value)
#
# The area is taken as the area of the secondary (inner) surface:
#
# Area = 2 * pi * h * r, where h is the height of the cylinder.
#
# The integrated heat flux across the gap at time 1 is then:
#
# 2*pi*h*k*delta_T/(ln(r2/r1))
# 2*pi*1*1*100/(ln(2/1)) = 906.5 watts
#
# For comparison, see results from the integrated flux post processors.
# This simulation makes use of symmetry, so only 1/4 of the cylinders is meshed
# As such, the integrated flux from the post processors is 1/4 of the total,
# or 226.6 watts.
# The value coming from the post processor is slightly less than this
# but converges as mesh refinement increases.
#
# Simulating contact is challenging. Regression tests that exercise
# contact features can be difficult to solve consistently across multiple
# platforms. While designing these tests, we felt it worth while to note
# some aspects of these tests. The following applies to:
# sphere3D.i, sphere2DRZ.i, cyl2D.i, and cyl3D.i.
# 1. We decided that to perform consistently across multiple platforms we
# would use very small convergence tolerance. In this test we chose an
# nl_rel_tol of 1e-12.
# 2. Due to such a high value for thermal conductivity (used here so that the
# domains come to a uniform temperature) the integrated flux at time = 0
# was relatively large (the value coming from SideIntegralFlux =
# -_diffusion_coef[_qp]*_grad_u[_qp]*_normals[_qp] where the diffusion coefficient
# here is thermal conductivity).
# Even though _grad_u[_qp] is small, in this case the diffusion coefficient
# is large. The result is a number that isn't exactly zero and tends to
# fail exodiff. For this reason the parameter execute_on = initial should not
# be used. That parameter is left to default settings in these regression tests.
#
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Mesh]
file = cyl3D.e
[]
[Functions]
[./temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[../]
[]
[Variables]
[./temp]
initial_condition = 100
[../]
[]
[AuxVariables]
[./gap_conductance]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./heat_conduction]
type = HeatConduction
variable = temp
[../]
[]
[AuxKernels]
[./gap_cond]
type = MaterialRealAux
property = gap_conductance
variable = gap_conductance
boundary = 2
[../]
[]
[Materials]
[./heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 1000000.0
[../]
[]
[ThermalContact]
[./thermal_contact]
type = GapHeatTransfer
variable = temp
primary = 3
secondary = 2
emissivity_primary = 0
emissivity_secondary = 0
gap_conductivity = 1
quadrature = true
gap_geometry_type = CYLINDER
cylinder_axis_point_1 = '0 0 0'
cylinder_axis_point_2 = '0 1 0'
[../]
[]
[BCs]
[./mid]
type = FunctionDirichletBC
boundary = 5
variable = temp
function = temp
[../]
[./temp_far_right]
type = DirichletBC
boundary = 4
variable = temp
value = 100
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[./Quadrature]
order = fifth
side_order = seventh
[../]
[]
[Outputs]
exodus = true
[./Console]
type = Console
[../]
[]
[Postprocessors]
[./temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[../]
[./temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[../]
[./flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[../]
[./flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[../]
[]
(test/tests/dgkernels/2d_diffusion_dg/no_functor_additions.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
elem_type = QUAD4
[]
[Variables]
[./u]
order = FIRST
family = MONOMIAL
[./InitialCondition]
type = ConstantIC
value = 1
[../]
[../]
[]
[AuxVariables]
[v]
order = FIRST
family = MONOMIAL
[]
[]
[Functions]
[./forcing_fn]
type = ParsedFunction
expression = 2*pow(e,-x-(y*y))*(1-2*y*y)
[../]
[./exact_fn]
type = ParsedGradFunction
expression = pow(e,-x-(y*y))
grad_x = -pow(e,-x-(y*y))
grad_y = -2*y*pow(e,-x-(y*y))
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[./abs] # u * v
type = Reaction
variable = u
[../]
[./forcing]
type = BodyForce
variable = u
function = forcing_fn
[../]
[]
[DGKernels]
[regular_dg_diffusion]
type = DGDiffusion
variable = u
epsilon = -1
sigma = 6
[]
[]
[DGDiffusionAction]
variable = u
kernels_to_add = 'COUPLED'
coupled_var = v
[]
[BCs]
[./all]
type = DGFunctionDiffusionDirichletBC
variable = u
boundary = '0 1 2 3'
function = exact_fn
epsilon = -1
sigma = 6
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[console]
type = Console
system_info = 'framework mesh aux nonlinear relationship execution'
[]
[]
[Problem]
error_on_jacobian_nonzero_reallocation = true
[]
[Postprocessors]
[num_rm]
type = NumRelationshipManagers
[]
[]
(modules/xfem/test/tests/single_var_constraint_2d/stationary_fluxjump_func.i)
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./line_seg_cut_uo]
type = LineSegmentCutUserObject
cut_data = '0.5 1.0 0.5 0.0'
[../]
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[Constraints]
[./xfem_constraint]
type = XFEMSingleVariableConstraint
variable = u
jump = 0
jump_flux = jump_flux_func
geometric_cut_userobject = 'line_seg_cut_uo'
[../]
[]
[Functions]
[./jump_flux_func]
type = ParsedFunction
expression = '1'
[../]
[]
[BCs]
# Define boundary conditions
[./left_u]
type = DirichletBC
variable = u
boundary = 3
value = 1
[../]
[./right_u]
type = DirichletBC
variable = u
boundary = 1
value = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
line_search = 'none'
l_tol = 1e-3
nl_max_its = 15
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
start_time = 0.0
dt = 1.0
end_time = 2.0
[]
[Outputs]
time_step_interval = 1
execute_on = timestep_end
exodus = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/sliding_block/in_and_out/frictional_02_penalty.i)
# This is a benchmark test that checks constraint based frictional
# contact using the penalty method. In this test a sinusoidal
# displacement is applied in the horizontal direction to simulate
# a small block come in and out of contact as it slides down a larger block.
#
# The sinusoid is of the form 0.4sin(4t)+0.2 and a friction coefficient
# of 0.2 is used. The gold file is run on one processor and the benchmark
# case is run on a minimum of 4 processors to ensure no parallel variability
# in the contact pressure and penetration results. Further documentation can
# found in moose/modules/contact/doc/sliding_block/
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[penetration]
[]
[inc_slip_x]
[]
[inc_slip_y]
[]
[accum_slip_x]
[]
[accum_slip_y]
[]
[]
[Functions]
[vertical_movement]
type = ParsedFunction
expression = -t
[]
[horizontal_movement]
type = ParsedFunction
expression = -0.04*sin(4*t)+0.02
[]
[]
[Modules/TensorMechanics/Master]
[all]
add_variables = true
strain = FINITE
[]
[]
[AuxKernels]
[zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[]
[accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[]
[accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[]
[penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[]
[]
[Postprocessors]
[nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[]
[penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[]
[contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[]
[]
[BCs]
[left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[]
[left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[]
[right_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = horizontal_movement
[]
[right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[]
[]
[Materials]
[left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
constant_on = SUBDOMAIN
[]
[left_stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
petsc_options_value = 'asm lu 20 101'
line_search = 'none'
l_max_its = 100
nl_max_its = 1000
dt = 0.1
end_time = 15
num_steps = 1000
l_tol = 1e-3
nl_rel_tol = 1e-10
nl_abs_tol = 1e-6
dtmin = 0.01
[Predictor]
type = SimplePredictor
scale = 1.0
[]
[]
[Outputs]
time_step_interval = 10
[out]
type = Exodus
elemental_as_nodal = true
[]
[console]
type = Console
max_rows = 5
[]
[]
[Contact]
[leftright]
secondary = 3
primary = 2
model = coulomb
penalty = 4e+6
friction_coefficient = 0.2
formulation = penalty
normal_smoothing_distance = 0.1
[]
[]
(modules/contact/test/tests/verification/patch_tests/ring_1/ring1_mu_0_2_pen.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
file = ring1_mesh.e
[]
[Problem]
type = FEProblem
coord_type = RZ
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./inc_slip_x]
type = PenetrationAux
variable = inc_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./inc_slip_y]
type = PenetrationAux
variable = inc_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_x]
type = PenetrationAux
variable = accum_slip_x
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./accum_slip_y]
type = PenetrationAux
variable = accum_slip_y
execute_on = timestep_end
boundary = 3
paired_boundary = 4
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 4
[../]
[./tang_force_x]
type = PenetrationAux
variable = tang_force_x
quantity = tangential_force_x
boundary = 3
paired_boundary = 4
[../]
[./tang_force_y]
type = PenetrationAux
variable = tang_force_y
quantity = tangential_force_y
boundary = 3
paired_boundary = 4
[../]
[] # AuxKernels
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x2]
type = NodalVariableValue
nodeid = 1
variable = disp_x
[../]
[./disp_x7]
type = NodalVariableValue
nodeid = 6
variable = disp_x
[../]
[./disp_y2]
type = NodalVariableValue
nodeid = 1
variable = disp_y
[../]
[./disp_y7]
type = NodalVariableValue
nodeid = 6
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeAxisymmetricRZIncrementalStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-9
l_max_its = 50
nl_max_its = 100
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-5
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
file_base = ring1_mu_0_2_pen_out
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
file_base = ring1_mu_0_2_pen_check
show = 'bot_react_x bot_react_y disp_x2 disp_y2 disp_x7 disp_y7 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
model = coulomb
formulation = penalty
normalize_penalty = true
tangential_tolerance = 1e-3
friction_coefficient = 0.2
penalty = 1e+9
[../]
[]
(modules/heat_transfer/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_sphere3D_mortar.i)
sphere_outer_htc = 10 # W/m^2/K
sphere_outer_Tinf = 300 # K
[GlobalParams]
order = SECOND
family = LAGRANGE
[]
[Problem]
kernel_coverage_check = false
material_coverage_check = false
[]
[Mesh]
[file]
type = FileMeshGenerator
file = sphere3D.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
sidesets = '2'
new_block_id = 10001
new_block_name = 'secondary_lower'
input = file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
sidesets = '3'
new_block_id = 10000
new_block_name = 'primary_lower'
input = secondary
[]
[]
[Functions]
[temp]
type = PiecewiseLinear
x = '0 1'
y = '100 200'
[]
[]
[Variables]
[temp]
initial_condition = 500
[]
[lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
[]
[]
[AuxVariables]
# [gap_conductance]
# order = CONSTANT
# family = MONOMIAL
# []
[power_density]
block = 'fuel'
initial_condition = 50e3
[]
[]
[Kernels]
[heat_conduction]
type = HeatConduction
variable = temp
block = '1 2'
[]
[heat_source]
type = CoupledForce
variable = temp
block = 'fuel'
v = power_density
[]
[]
# [AuxKernels]
# [gap_cond]
# type = MaterialRealAux
# property = gap_conductance
# variable = gap_conductance
# boundary = 2
# []
# []
[Materials]
[heat1]
type = HeatConductionMaterial
block = '1 2'
specific_heat = 1.0
thermal_conductivity = 34.6
[]
[]
[UserObjects]
[radiation]
type = GapFluxModelRadiation
temperature = temp
boundary = 2
primary_emissivity = 0.0
secondary_emissivity = 0.0
[]
[conduction]
type = GapFluxModelConduction
temperature = temp
boundary = 2
gap_conductivity = 5.0
[]
[]
[Constraints]
[ced]
type = ModularGapConductanceConstraint
variable = lm
secondary_variable = temp
primary_boundary = 3
primary_subdomain = 10000
secondary_boundary = 2
secondary_subdomain = 10001
gap_flux_models = 'radiation conduction'
gap_geometry_type = SPHERE
sphere_origin = '0 0 0'
[]
[]
[BCs]
[RPV_out_BC] # k \nabla T = h (T- T_inf) at RPV outer boundary
type = ConvectiveFluxFunction # (Robin BC)
variable = temp
boundary = '4' # outer RPV
coefficient = ${sphere_outer_htc}
T_infinity = ${sphere_outer_Tinf}
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
petsc_options_value = 'lu superlu_dist'
dt = 1
dtmin = 0.01
end_time = 1
nl_rel_tol = 1e-12
nl_abs_tol = 1e-7
[]
[Outputs]
exodus = true
csv = true
[Console]
type = Console
[]
[]
[Postprocessors]
[temp_left]
type = SideAverageValue
boundary = 2
variable = temp
[]
[temp_right]
type = SideAverageValue
boundary = 3
variable = temp
[]
[flux_left]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 2
diffusivity = thermal_conductivity
[]
[flux_right]
type = SideDiffusiveFluxIntegral
variable = temp
boundary = 3
diffusivity = thermal_conductivity
[]
[ptot]
type = ElementIntegralVariablePostprocessor
variable = power_density
block = 'fuel'
[]
[sphere_convective_out]
type = ConvectiveHeatTransferSideIntegral
T_solid = temp
boundary = '4' # outer RVP
T_fluid = ${sphere_outer_Tinf}
htc = ${sphere_outer_htc}
[]
[heat_balance] # should be equal to 0 upon convergence
type = ParsedPostprocessor
expression = '(sphere_convective_out - ptot) / ptot'
pp_names = 'sphere_convective_out ptot'
[]
[]
[VectorPostprocessors]
[NodalTemperature]
type = NodalValueSampler
sort_by = id
boundary = '2 3'
variable = temp
[]
[]
(modules/xfem/test/tests/checkpoint/checkpoint.i)
# This test is for two layer materials with different youngs modulus
# The global stress is determined by switching the stress based on level set values
# The material interface is marked by a level set function
# The two layer materials are glued together
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Mesh]
displacements = 'disp_x disp_y'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
[]
[./left_bottom]
type = ExtraNodesetGenerator
new_boundary = 'left_bottom'
coord = '0.0 0.0'
input = gen
[../]
[./left_top]
type = ExtraNodesetGenerator
new_boundary = 'left_top'
coord = '0.0 5.'
input = left_bottom
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'y-2.5'
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./TensorMechanics]
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 0
variable = stress_xx
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 1
index_j = 1
variable = stress_yy
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
index_i = 0
index_j = 1
variable = stress_xy
[../]
[./a_strain_xx]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = RankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = RankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = FunctionDirichletBC
boundary = top
variable = disp_x
function = 0.03*t
[../]
[./topy]
type = FunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ComputeSmallStrain
base_name = A
[../]
[./stress_A]
type = ComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e5
poissons_ratio = 0.3
[../]
[./strain_B]
type = ComputeSmallStrain
base_name = B
[../]
[./stress_B]
type = ComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = LevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[./combined_dstressdstrain]
type = LevelSetBiMaterialRankFour
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = Jacobian_mult
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'bt'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-3
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-7
# time control
start_time = 0.0
dt = 0.1
num_steps = 2
max_xfem_update = 1
[]
[Outputs]
checkpoint = true
exodus = true
execute_on = timestep_end
csv = true
[./console]
type = Console
output_linear = true
[../]
[]
(modules/contact/test/tests/verification/patch_tests/plane_4/plane4_template1.i)
[GlobalParams]
order = SECOND
displacements = 'disp_x disp_y'
[]
[Mesh]
file = plane4_mesh.e
[]
[Problem]
type = ReferenceResidualProblem
extra_tag_vectors = 'ref'
reference_vector = 'ref'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./penetration]
[../]
[./saved_x]
[../]
[./saved_y]
[../]
[./diag_saved_x]
[../]
[./diag_saved_y]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[./tang_force_x]
[../]
[./tang_force_y]
[../]
[]
[Kernels]
[./TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./stress_zz]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 4
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 4
paired_boundary = 3
[../]
[]
[Postprocessors]
[./bot_react_x]
type = NodalSum
variable = saved_x
boundary = 1
[../]
[./bot_react_y]
type = NodalSum
variable = saved_y
boundary = 1
[../]
[./top_react_x]
type = NodalSum
variable = saved_x
boundary = 5
[../]
[./top_react_y]
type = NodalSum
variable = saved_y
boundary = 5
[../]
[./ref_resid_x]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_x
[../]
[./ref_resid_y]
type = NodalL2Norm
execute_on = timestep_end
variable = saved_y
[../]
[./sigma_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./sigma_zz]
type = ElementAverageValue
variable = stress_zz
[../]
[./disp_x9]
type = NodalVariableValue
nodeid = 8
variable = disp_x
[../]
[./disp_x16]
type = NodalVariableValue
nodeid = 15
variable = disp_x
[../]
[./disp_y9]
type = NodalVariableValue
nodeid = 8
variable = disp_y
[../]
[./disp_y16]
type = NodalVariableValue
nodeid = 15
variable = disp_y
[../]
[./_dt]
type = TimestepSize
[../]
[./num_lin_it]
type = NumLinearIterations
[../]
[./num_nonlin_it]
type = NumNonlinearIterations
[../]
[]
[BCs]
[./bot_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./side_x]
type = DirichletBC
variable = disp_x
boundary = 2
value = 0.0
[../]
[./top_press]
type = Pressure
variable = disp_y
boundary = 5
factor = 109.89
[../]
[]
[Materials]
[./bot_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./bot_strain]
type = ComputeIncrementalSmallStrain
block = '1'
[../]
[./bot_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[../]
[./top_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./top_strain]
type = ComputeIncrementalSmallStrain
block = '2'
[../]
[./top_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-7
l_max_its = 100
nl_max_its = 200
dt = 1.0
end_time = 1.0
num_steps = 10
dtmin = 1.0
l_tol = 1e-3
[]
[VectorPostprocessors]
[./x_disp]
type = NodalValueSampler
variable = disp_x
boundary = '1 3 4 5'
sort_by = x
[../]
[./cont_press]
type = NodalValueSampler
variable = contact_pressure
boundary = '3'
sort_by = x
[../]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
[./exodus]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[./chkfile]
type = CSV
show = 'bot_react_x bot_react_y disp_x9 disp_y9 disp_x16 disp_y16 sigma_yy sigma_zz top_react_x top_react_y x_disp cont_press'
execute_vector_postprocessors_on = timestep_end
[../]
[./outfile]
type = CSV
delimiter = ' '
execute_vector_postprocessors_on = none
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 4
normalize_penalty = true
tangential_tolerance = 1e-3
penalty = 1e+9
[../]
[]
(modules/xfem/test/tests/bimaterials/glued_ad_bimaterials_2d.i)
# This test is for two layer materials with different youngs modulus using AD
# The global stress is determined by switching the stress based on level set values
# The material interface is marked by a level set function
# The two layer materials are glued together
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y'
[]
[XFEM]
qrule = volfrac
output_cut_plane = true
[]
[UserObjects]
[./level_set_cut_uo]
type = LevelSetCutUserObject
level_set_var = ls
[../]
[]
[Mesh]
displacements = 'disp_x disp_y'
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
xmin = 0.0
xmax = 5.
ymin = 0.0
ymax = 5.
elem_type = QUAD4
[]
[./left_bottom]
type = ExtraNodesetGenerator
new_boundary = 'left_bottom'
coord = '0.0 0.0'
input = gen
[../]
[./left_top]
type = ExtraNodesetGenerator
new_boundary = 'left_top'
coord = '0.0 5.'
input = left_bottom
[../]
[]
[AuxVariables]
[./ls]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxKernels]
[./ls_function]
type = FunctionAux
variable = ls
function = ls_func
[../]
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[Functions]
[./ls_func]
type = ParsedFunction
expression = 'y-2.5'
[../]
[]
[AuxVariables]
[./a_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./a_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./b_strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = SMALL
use_automatic_differentiation = true
add_variables = true
generate_output = 'stress_xx stress_yy stress_xy'
[../]
[]
[AuxKernels]
[./a_strain_xx]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 0
variable = a_strain_xx
[../]
[./a_strain_yy]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 1
index_j = 1
variable = a_strain_yy
[../]
[./a_strain_xy]
type = ADRankTwoAux
rank_two_tensor = A_total_strain
index_i = 0
index_j = 1
variable = a_strain_xy
[../]
[./b_strain_xx]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 0
variable = b_strain_xx
[../]
[./b_strain_yy]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 1
index_j = 1
variable = b_strain_yy
[../]
[./b_strain_xy]
type = ADRankTwoAux
rank_two_tensor = B_total_strain
index_i = 0
index_j = 1
variable = b_strain_xy
[../]
[]
[Constraints]
[./dispx_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_x
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[./dispy_constraint]
type = XFEMSingleVariableConstraint
use_displaced_mesh = false
variable = disp_y
alpha = 1e8
geometric_cut_userobject = 'level_set_cut_uo'
[../]
[]
[BCs]
[./bottomx]
type = ADDirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[../]
[./bottomy]
type = ADDirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[../]
[./topx]
type = ADFunctionDirichletBC
boundary = top
variable = disp_x
function = 0.03*t
[../]
[./topy]
type = ADFunctionDirichletBC
boundary = top
variable = disp_y
function = '0.03*t'
[../]
[]
[Materials]
[./elasticity_tensor_A]
type = ADComputeIsotropicElasticityTensor
base_name = A
youngs_modulus = 1e9
poissons_ratio = 0.3
[../]
[./strain_A]
type = ADComputeSmallStrain
base_name = A
[../]
[./stress_A]
type = ADComputeLinearElasticStress
base_name = A
[../]
[./elasticity_tensor_B]
type = ADComputeIsotropicElasticityTensor
base_name = B
youngs_modulus = 1e5
poissons_ratio = 0.3
[../]
[./strain_B]
type = ADComputeSmallStrain
base_name = B
[../]
[./stress_B]
type = ADComputeLinearElasticStress
base_name = B
[../]
[./combined_stress]
type = ADLevelSetBiMaterialRankTwo
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = stress
[../]
[./combined_elasticity_tensor]
type = ADLevelSetBiMaterialRankFour
levelset_positive_base = 'A'
levelset_negative_base = 'B'
level_set_var = ls
prop_name = elasticity_tensor
[../]
[]
[Executioner]
type = Transient
solve_type = NEWTON
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'bt'
# controls for linear iterations
l_max_its = 20
l_tol = 1e-8
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-14
nl_abs_tol = 1e-50
# time control
start_time = 0.0
dt = 0.1
num_steps = 2
max_xfem_update = 1
[]
[Outputs]
exodus = true
file_base = glued_bimaterials_2d_out
execute_on = timestep_end
[./console]
type = Console
output_linear = true
[../]
[]
(test/tests/outputs/console/console.i)
###########################################################
# This test exercises console Output control. Various
# controls are implemented using this input file including
# turning off color, changing Postprocessor output,
# toggling the performance logging, and verifying
# simulation information on the console.
#
# @Requirement U1.40
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[AuxVariables]
[./aux0]
order = SECOND
family = SCALAR
[../]
[./aux1]
family = SCALAR
initial_condition = 5
[../]
[./aux2]
family = SCALAR
initial_condition = 10
[../]
[]
[Kernels]
[./diff_u]
type = Diffusion
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 2
[../]
[]
[BCs]
[./right_u]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[./left_u]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right_v]
type = DirichletBC
variable = v
boundary = right
value = 3
[../]
[./left_v]
type = DirichletBC
variable = v
boundary = left
value = 2
[../]
[]
[Postprocessors]
[./num_vars]
type = NumVars
system = 'NL'
[../]
[./num_aux]
type = NumVars
system = 'AUX'
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
execute_on = 'timestep_end'
color = false
[./screen]
type = Console
fit_mode = 40
[../]
[]
[ICs]
[./aux0_IC]
variable = aux0
values = '12 13'
type = ScalarComponentIC
[../]
[]
(modules/xfem/test/tests/solid_mechanics_basic/edge_crack_2d_propagation_mhs.i)
[GlobalParams]
displacements = 'disp_x disp_y'
volumetric_locking_correction = true
[]
[XFEM]
geometric_cut_userobjects = 'cut_mesh2'
qrule = volfrac
output_cut_plane = true
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = 45
ny = 15
xmin = -1.5
xmax = 1.5
ymin = 0.0
ymax = 1.0
elem_type = QUAD4
[]
[dispBlock]
type = BoundingBoxNodeSetGenerator
new_boundary = pull_set
bottom_left = '-0.1 0.99 0'
top_right = '0.1 1.01 0'
input = gen
[]
[]
[DomainIntegral]
integrals = 'Jintegral InteractionIntegralKI InteractionIntegralKII'
displacements = 'disp_x disp_y'
crack_front_points_provider = cut_mesh2
2d=true
number_points_from_provider = 2
crack_direction_method = CurvedCrackFront
radius_inner = '0.15'
radius_outer = '0.45'
poissons_ratio = 0.3
youngs_modulus = 207000
block = 0
incremental = true
used_by_xfem_to_grow_crack = true
[]
[UserObjects]
[cut_mesh2]
type = MeshCut2DFractureUserObject
mesh_file = make_edge_crack_in.e
k_critical=80
growth_increment = 0.1
[]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
planar_formulation = plane_strain
add_variables = true
generate_output = 'stress_xx stress_yy vonmises_stress'
[../]
[]
[BCs]
[top_y]
type = DirichletBC
boundary = pull_set
variable = disp_y
value = 0.001
[]
[bottom_x]
type = DirichletBC
boundary = bottom
variable = disp_x
value = 0.0
[]
[bottom_y]
type = DirichletBC
boundary = bottom
variable = disp_y
value = 0.0
[]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 207000
poissons_ratio = 0.3
block = 0
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = 0
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
petsc_options_value = '201 hypre boomeramg 8'
line_search = 'none'
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
# controls for linear iterations
l_max_its = 100
l_tol = 1e-2
# controls for nonlinear iterations
nl_max_its = 15
nl_rel_tol = 1e-8
nl_abs_tol = 1e-9
# time control
start_time = 0.0
dt = 1.0
end_time = 1
max_xfem_update = 100
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[xfemcutter]
type=XFEMCutMeshOutput
xfem_cutter_uo=cut_mesh2
[]
# console = false
[./console]
type = Console
output_linear = false
output_nonlinear = false
[../]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/06_custom_closures.i)
T_in = 300. # K
m_dot_in = 1e-2 # kg/s
press = 10e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 25
core_dia = '${units 2. cm -> m}'
core_pitch = '${units 8.7 cm -> m}'
A_core = '${fparse core_pitch^2 - 0.25 *pi * core_dia^2}'
P_wet_core = '${fparse 4*core_pitch + pi * core_dia}'
Dh_core = '${fparse 4 * A_core / P_wet_core}'
# pipe parameters
pipe_dia = '${units 10. cm -> m}'
A_pipe = '${fparse 0.25 * pi * pipe_dia^2}'
tot_power = 2000 # W
# heat exchanger parameters
hx_dia_inner = '${units 12. cm -> m}'
hx_wall_thickness = '${units 5. mm -> m}'
hx_dia_outer = '${units 50. cm -> m}'
hx_radius_wall = '${fparse hx_dia_inner / 2. + hx_wall_thickness}'
hx_length = 1.5 # m
hx_n_elems = 25
m_dot_sec_in = 1. # kg/s
[GlobalParams]
initial_p = ${press}
initial_vel = 0.0001
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
gravity_vector = '0 0 0'
rdg_slope_reconstruction = minmod
scaling_factor_1phase = '1 1e-2 1e-4'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1e-2
scaling_factor_rhovV = 1e-2
scaling_factor_rhowV = 1e-2
scaling_factor_rhoEV = 1e-4
closures = thm_closures
fp = he
[]
[Functions]
[m_dot_sec_fn]
type = PiecewiseLinear
xy_data = '
0 0
10 ${m_dot_sec_in}'
[]
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[water]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[thm_closures]
type = Closures1PhaseTHM
[]
[none_closures]
type = Closures1PhaseNone
[]
[]
[Materials]
[Re_mat]
type = ADReynoldsNumberMaterial
Re = Re
rho = rho
vel = vel
D_h = D_h
mu = mu
block = hx/pri
[]
[f_mat]
type = ADParsedMaterial
property_name = f_D
constant_names = 'a b c'
constant_expressions = '1 0.1 -0.5'
material_property_names = 'Re'
expression = 'a + b * Re^c'
block = hx/pri
[]
[Pr_mat]
type = ADPrandtlNumberMaterial
Pr = Pr
cp = cp
mu = mu
k = k
block = hx/pri
[]
[Nu_mat]
type = ADParsedMaterial
property_name = 'Nu'
constant_names = 'a b c'
constant_expressions = '0.03 0.9 0.5'
material_property_names = 'Re Pr'
expression = 'a * Re ^b * Pr^c'
block = hx/pri
[]
[Hw_mat]
type = ADConvectiveHeatTransferCoefficientMaterial
D_h = D_h
k = k
Nu = Nu
Hw = Hw
block = hx/pri
[]
[]
[SolidProperties]
[steel]
type = ThermalFunctionSolidProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[up_pipe_1]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = 0.5
n_elems = 15
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 0.5'
connections = 'up_pipe_1:out core_chan:in'
volume = 1e-5
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
roughness = .0001
A = ${A_core}
D_h = ${Dh_core}
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0.5'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
solid_properties = 'steel'
solid_properties_T_ref = '300'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = '${fparse pi * core_dia}'
[]
[jct2]
type = JunctionParallelChannels1Phase
position = '0 0 1.5'
connections = 'core_chan:out up_pipe_2:in'
volume = 1e-5
[]
[up_pipe_2]
type = FlowChannel1Phase
position = '0 0 1.5'
orientation = '0 0 1'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct3]
type = JunctionOneToOne1Phase
connections = 'up_pipe_2:out top_pipe_1:in'
[]
[top_pipe_1]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[top_pipe_2]
type = FlowChannel1Phase
position = '0.5 0 2'
orientation = '1 0 0'
length = 0.5
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct4]
type = VolumeJunction1Phase
position = '0.5 0 2'
volume = 1e-5
connections = 'top_pipe_1:out top_pipe_2:in press_pipe:in'
[]
[press_pipe]
type = FlowChannel1Phase
position = '0.5 0 2'
orientation = '0 1 0'
length = 0.2
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[pressurizer]
type = InletStagnationPressureTemperature1Phase
p0 = ${press}
T0 = ${T_in}
input = press_pipe:out
[]
[jct5]
type = JunctionOneToOne1Phase
connections = 'top_pipe_2:out down_pipe_1:in'
[]
[down_pipe_1]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = 0.25
A = ${A_pipe}
n_elems = 5
[]
[jct6]
type = JunctionParallelChannels1Phase
position = '1 0 1.75'
connections = 'down_pipe_1:out hx/pri:in'
volume = 1e-5
[]
[hx]
[pri]
type = FlowChannel1Phase
position = '1 0 1.75'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
roughness = 1e-5
A = '${fparse pi * hx_dia_inner * hx_dia_inner / 4.}'
D_h = ${hx_dia_inner}
closures = none_closures
[]
[ht_pri]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = inner
flow_channel = hx/pri
P_hf = '${fparse pi * hx_dia_inner}'
[]
[wall]
type = HeatStructureCylindrical
position = '1 0 1.75'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
widths = '${hx_wall_thickness}'
n_part_elems = '3'
solid_properties = 'steel'
solid_properties_T_ref = '300'
names = '0'
inner_radius = '${fparse hx_dia_inner / 2.}'
[]
[ht_sec]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = outer
flow_channel = hx/sec
P_hf = '${fparse 2 * pi * hx_radius_wall}'
[]
[sec]
type = FlowChannel1Phase
position = '${fparse 1 + hx_wall_thickness} 0 0.25'
orientation = '0 0 1'
length = ${hx_length}
n_elems = ${hx_n_elems}
A = '${fparse pi * (hx_dia_outer * hx_dia_outer / 4. - hx_radius_wall * hx_radius_wall)}'
D_h = '${fparse hx_dia_outer - (2 * hx_radius_wall)}'
fp = water
initial_T = 300
[]
[]
[jct7]
type = JunctionParallelChannels1Phase
position = '1 0 0.5'
connections = 'hx/pri:out down_pipe_2:in'
volume = 1e-5
[]
[down_pipe_2]
type = FlowChannel1Phase
position = '1 0 0.25'
orientation = '0 0 -1'
length = 0.25
n_elems = 10
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct8]
type = JunctionOneToOne1Phase
connections = 'down_pipe_2:out bottom_1:in'
[]
[bottom_1]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[pump]
type = Pump1Phase
position = '0.5 0 0'
connections = 'bottom_1:out bottom_2:in'
volume = 1e-4
A_ref = ${A_pipe}
head = 0
[]
[bottom_2]
type = FlowChannel1Phase
position = '0.5 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${A_pipe}
D_h = ${pipe_dia}
[]
[jct9]
type = JunctionOneToOne1Phase
connections = 'bottom_2:out up_pipe_1:in'
[]
[inlet_sec]
type = InletMassFlowRateTemperature1Phase
input = 'hx/sec:in'
m_dot = 0
T = 300
[]
[outlet_sec]
type = Outlet1Phase
input = 'hx/sec:out'
p = 1e5
[]
[]
[ControlLogic]
[set_point]
type = GetFunctionValueControl
function = ${m_dot_in}
[]
[pid]
type = PIDControl
initial_value = 0.0
set_point = set_point:value
input = m_dot_pump
K_p = 1.
K_i = 4.
K_d = 0
[]
[set_pump_head]
type = SetComponentRealValueControl
component = pump
parameter = head
value = pid:output
[]
[m_dot_sec_inlet_ctrl]
type = GetFunctionValueControl
function = m_dot_sec_fn
[]
[set_m_dot_sec_ctrl]
type = SetComponentRealValueControl
component = inlet_sec
parameter = m_dot
value = m_dot_sec_inlet_ctrl:value
[]
[]
[Postprocessors]
[power_to_coolant]
type = ADHeatRateConvection1Phase
block = core_chan
P_hf = '${fparse pi *core_dia}'
[]
[m_dot_pump]
type = ADFlowJunctionFlux1Phase
boundary = core_chan:in
connection_index = 1
equation = mass
junction = jct7
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[core_p_in]
type = SideAverageValue
boundary = core_chan:in
variable = p
[]
[core_p_out]
type = SideAverageValue
boundary = core_chan:out
variable = p
[]
[core_delta_p]
type = ParsedPostprocessor
pp_names = 'core_p_in core_p_out'
expression = 'core_p_in - core_p_out'
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = hx/pri:out
variable = T
[]
[hx_sec_T_in]
type = SideAverageValue
boundary = inlet_sec
variable = T
[]
[hx_sec_T_out]
type = SideAverageValue
boundary = outlet_sec
variable = T
[]
[m_dot_sec]
type = ADFlowBoundaryFlux1Phase
boundary = inlet_sec
equation = mass
[]
[Hw_hx_pri]
type = ADElementAverageMaterialProperty
mat_prop = Hw
block = hx/pri
[]
[fD_hx_pri]
type = ADElementAverageMaterialProperty
mat_prop = f_D
block = hx/pri
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = IterationAdaptiveDT
dt = 1
[]
dtmax = 5
end_time = 500
line_search = basic
solve_type = NEWTON
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 25
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/test/tests/components/volume_junction_1phase/phy.shower.i)
# This problem models a "shower": water from two pipes, one hot and one cold,
# mixes together to produce a temperature between the two.
[GlobalParams]
gravity_vector = '0 0 0'
initial_T = 300
initial_p = 1e5
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
# global parameters for pipes
fp = eos
orientation = '1 0 0'
length = 1
n_elems = 20
f = 0
scaling_factor_1phase = '1 1 1e-6'
closures = simple_closures
[]
[FluidProperties]
[eos]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[inlet_hot]
type = InletDensityVelocity1Phase
input = 'pipe_hot:in'
# rho @ (p = 1e5, T = 310 K)
rho = 1315.9279785683
vel = 1
[]
[inlet_cold]
type = InletDensityVelocity1Phase
input = 'pipe_cold:in'
# rho @ (p = 1e5, T = 280 K)
rho = 1456.9202619863
vel = 1
[]
[outlet]
type = Outlet1Phase
input = 'pipe_warm:out'
p = 1e5
[]
[pipe_hot]
type = FlowChannel1Phase
position = '0 1 0'
A = 1
[]
[pipe_cold]
type = FlowChannel1Phase
position = '0 0 0'
A = 1
[]
[pipe_warm]
type = FlowChannel1Phase
position = '1 0.5 0'
A = 2
[]
[junction]
type = VolumeJunction1Phase
connections = 'pipe_cold:out pipe_hot:out pipe_warm:in'
position = '1 0.5 0'
volume = 1e-8
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-5
nl_max_its = 10
l_tol = 1e-2
l_max_its = 10
start_time = 0
end_time = 5
dt = 0.05
# abort_on_solve_fail = true
[]
[Postprocessors]
# These post-processors are used to test that the energy flux on
# the warm side of the junction is equal to the sum of the energy
# fluxes of the hot and cold inlets to the junction.
[energy_flux_hot]
type = EnergyFluxIntegral
boundary = pipe_hot:out
arhouA = rhouA
H = H
[]
[energy_flux_cold]
type = EnergyFluxIntegral
boundary = pipe_cold:out
arhouA = rhouA
H = H
[]
[energy_flux_warm]
type = EnergyFluxIntegral
boundary = pipe_warm:in
arhouA = rhouA
H = H
[]
[energy_flux_inlet_sum]
type = SumPostprocessor
values = 'energy_flux_hot energy_flux_cold'
[]
[test_rel_err]
type = RelativeDifferencePostprocessor
value1 = energy_flux_warm
value2 = energy_flux_inlet_sum
[]
[]
[Outputs]
[out]
type = CSV
show = test_rel_err
sync_only = true
sync_times = '3 4 5'
[]
[console]
type = Console
max_rows = 1
[]
print_linear_residuals = false
[]
(modules/contact/test/tests/sliding_block/sliding/frictionless_aug.i)
# This is a benchmark test that checks constraint based frictionless
# contact using the augmented lagrangian method. In this test a constant
# displacement is applied in the horizontal direction to simulate
# a small block come sliding down a larger block.
#
# The gold file is run on one processor
# and the benchmark case is run on a minimum of 4 processors to ensure no
# parallel variability in the contact pressure and penetration results.
#
[Mesh]
file = sliding_elastic_blocks_2d.e
patch_size = 80
[]
[GlobalParams]
volumetric_locking_correction = false
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./saved_x]
[../]
[./saved_y]
[../]
[./contact_traction]
[../]
[./penetration]
[../]
[./inc_slip_x]
[../]
[./inc_slip_y]
[../]
[./accum_slip_x]
[../]
[./accum_slip_y]
[../]
[]
[Functions]
[./vertical_movement]
type = ParsedFunction
expression = -t
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
add_variables = true
strain = FINITE
save_in = 'saved_x saved_y'
extra_vector_tags = 'ref'
[../]
[]
[AuxKernels]
[./zeroslip_x]
type = ConstantAux
variable = inc_slip_x
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./zeroslip_y]
type = ConstantAux
variable = inc_slip_y
boundary = 3
execute_on = timestep_begin
value = 0.0
[../]
[./accum_slip_x]
type = AccumulateAux
variable = accum_slip_x
accumulate_from_variable = inc_slip_x
execute_on = timestep_end
[../]
[./accum_slip_y]
type = AccumulateAux
variable = accum_slip_y
accumulate_from_variable = inc_slip_y
execute_on = timestep_end
[../]
[./penetration]
type = PenetrationAux
variable = penetration
boundary = 3
paired_boundary = 2
[../]
[]
[Postprocessors]
[./nonlinear_its]
type = NumNonlinearIterations
execute_on = timestep_end
[../]
[./penetration]
type = NodalVariableValue
variable = penetration
nodeid = 222
[../]
[./contact_pressure]
type = NodalVariableValue
variable = contact_pressure
nodeid = 222
[../]
[]
[BCs]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./left_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = 4
value = -0.02
[../]
[./right_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = vertical_movement
[../]
[]
[Materials]
[./left]
type = ComputeIsotropicElasticityTensor
block = '1 2'
youngs_modulus = 1e6
poissons_ratio = 0.3
[../]
[./stress]
type = ComputeFiniteStrainElasticStress
block = '1 2'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
dt = 0.1
end_time = 15
num_steps = 200
l_tol = 1e-6
nl_rel_tol = 1e-7
nl_abs_tol = 1e-6
dtmin = 0.01
[./Predictor]
type = SimplePredictor
scale = 1.0
[../]
[]
[Outputs]
time_step_interval = 10
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
max_rows = 5
[../]
[]
[Problem]
type = AugmentedLagrangianContactProblem
solution_variables = 'disp_x disp_y'
extra_tag_vectors = 'ref'
reference_vector = 'ref'
maximum_lagrangian_update_iterations = 25
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Contact]
[./leftright]
secondary = 3
primary = 2
model = frictionless
penalty = 1e+7
normalize_penalty = true
formulation = augmented_lagrange
tangential_tolerance = 1e-3
normal_smoothing_distance = 0.1
al_penetration_tolerance = 1e-9
[../]
[]
(modules/contact/test/tests/pdass_problems/ironing.i)
[GlobalParams]
volumetric_locking_correction = true
displacements = 'disp_x disp_y'
[]
[Mesh]
[input_file]
type = FileMeshGenerator
file = iron.e
[]
[secondary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10001
new_block_name = 'secondary_lower'
sidesets = '10'
input = input_file
[]
[primary]
type = LowerDBlockFromSidesetGenerator
new_block_id = 10000
sidesets = '20'
new_block_name = 'primary_lower'
input = secondary
[]
patch_update_strategy = auto
patch_size = 20
[]
[Variables]
[disp_x]
[]
[disp_y]
[]
[frictionless_normal_lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
use_dual = true
[]
[tangential_lm]
order = FIRST
family = LAGRANGE
block = 'secondary_lower'
use_dual = true
[]
[]
[AuxVariables]
[stress_xx]
order = CONSTANT
family = MONOMIAL
[]
[stress_yy]
order = CONSTANT
family = MONOMIAL
[]
[stress_xy]
order = CONSTANT
family = MONOMIAL
[]
[saved_x]
[]
[saved_y]
[]
[diag_saved_x]
[]
[diag_saved_y]
[]
[von_mises]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[disp_ramp_vert]
type = PiecewiseLinear
x = '0. 2. 8.'
y = '0. -1.0 -1.0'
[]
[disp_ramp_horz]
type = PiecewiseLinear
x = '0. 8.' # x = '0. 2. 8.'
y = '0. 8.' # y = '0. 0. 8'
[]
[]
[Kernels]
[TensorMechanics]
use_displaced_mesh = true
save_in = 'saved_x saved_y'
block = '1 2'
strain = FINITE
[]
[]
[AuxKernels]
[stress_xx]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xx
index_i = 0
index_j = 0
execute_on = timestep_end
block = '1 2'
[]
[stress_yy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_yy
index_i = 1
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[stress_xy]
type = RankTwoAux
rank_two_tensor = stress
variable = stress_xy
index_i = 0
index_j = 1
execute_on = timestep_end
block = '1 2'
[]
[von_mises_kernel]
#Calculates the von mises stress and assigns it to von_mises
type = RankTwoScalarAux
variable = von_mises
rank_two_tensor = stress
execute_on = timestep_end
scalar_type = VonMisesStress
block = '1 2'
[]
[]
[Postprocessors]
[bot_react_x]
type = NodalSum
variable = saved_x
boundary = 20
[]
[bot_react_y]
type = NodalSum
variable = saved_y
boundary = 20
[]
[top_react_x]
type = NodalSum
variable = saved_x
boundary = 10
[]
[top_react_y]
type = NodalSum
variable = saved_y
boundary = 10
[]
[_dt]
type = TimestepSize
[]
[contact_pressure]
type = NodalVariableValue
variable = frictionless_normal_lm
nodeid = 805
[]
[]
[BCs]
[bot_x_disp]
type = DirichletBC
variable = disp_x
boundary = '40'
value = 0.0
preset = false
[]
[bot_y_disp]
type = DirichletBC
variable = disp_y
boundary = '40'
value = 0.0
preset = false
[]
[top_y_disp]
type = FunctionDirichletBC
variable = disp_y
boundary = '30'
function = disp_ramp_vert
preset = false
[]
[top_x_disp]
type = FunctionDirichletBC
variable = disp_x
boundary = '30'
function = disp_ramp_horz
preset = false
[]
[]
[Materials]
[stuff1_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '2'
youngs_modulus = 6896
poissons_ratio = 0.32
[]
[stuff1_strain]
type = ComputeFiniteStrain
block = '2'
[]
[stuff1_stress]
type = ComputeFiniteStrainElasticStress
block = '2'
[]
[stuff2_elas_tens]
type = ComputeIsotropicElasticityTensor
block = '1'
youngs_modulus = 689.6
poissons_ratio = 0.32
[]
[stuff2_strain]
type = ComputeFiniteStrain
block = '1'
[]
[stuff2_stress]
type = ComputeFiniteStrainElasticStress
block = '1'
[]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options = '-snes_ksp_ew'
petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
petsc_options_value = 'lu superlu_dist'
line_search = 'none'
nl_abs_tol = 1e-7
nl_rel_tol = 1e-7
l_tol = 1e-6
l_max_its = 50
nl_max_its = 30
start_time = 0.0
end_time = 0.1 # 6.5
dt = 0.0125
dtmin = 1e-5
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[VectorPostprocessors]
[cont_press]
type = NodalValueSampler
variable = frictionless_normal_lm
boundary = '10'
sort_by = id
execute_on = FINAL
[]
[friction]
type = NodalValueSampler
variable = tangential_lm
boundary = '10'
sort_by = id
execute_on = FINAL
[]
[]
[Outputs]
print_linear_residuals = true
perf_graph = true
exodus = false
csv = true
[chkfile]
type = CSV
show = 'cont_press friction'
start_time = 0.0
execute_vector_postprocessors_on = FINAL
[]
[console]
type = Console
max_rows = 5
[]
[]
[Debug]
show_var_residual_norms = true
[]
[UserObjects]
[weighted_vel_uo]
type = LMWeightedVelocitiesUserObject
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
lm_variable_normal = frictionless_normal_lm
lm_variable_tangential_one = tangential_lm
secondary_variable = disp_x
disp_x = disp_x
disp_y = disp_y
[]
[]
[Constraints]
# All constraints below for mechanical contact (Mortar)
[weighted_gap_lm]
type = ComputeFrictionalForceLMMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = 10000
secondary_subdomain = 10001
variable = frictionless_normal_lm
disp_x = disp_x
disp_y = disp_y
use_displaced_mesh = true
friction_lm = tangential_lm
mu = 0.5
c_t = 1.0e1
c = 1.0e3
weighted_gap_uo = weighted_vel_uo
weighted_velocities_uo = weighted_vel_uo
[]
[x]
type = NormalMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = frictionless_normal_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = weighted_vel_uo
[]
[y]
type = NormalMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = frictionless_normal_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_gap_uo = weighted_vel_uo
[]
[tangential_x]
type = TangentialMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = tangential_lm
secondary_variable = disp_x
component = x
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = weighted_vel_uo
[]
[tangential_y]
type = TangentialMortarMechanicalContact
primary_boundary = 20
secondary_boundary = 10
primary_subdomain = '10000'
secondary_subdomain = '10001'
variable = tangential_lm
secondary_variable = disp_y
component = y
use_displaced_mesh = true
compute_lm_residuals = false
weighted_velocities_uo = weighted_vel_uo
[]
[]
(test/include/outputs/OutputObjectTest.h)
// This file is part of the MOOSE framework
// https://www.mooseframework.org
//
// All rights reserved, see COPYRIGHT for full restrictions
// https://github.com/idaholab/moose/blob/master/COPYRIGHT
//
// Licensed under LGPL 2.1, please see LICENSE for details
// https://www.gnu.org/licenses/lgpl-2.1.html
#pragma once
// MOOSE includes
#include "Console.h"
class OutputObjectTest : public Console
{
public:
/**
* Class constructor
* @param name
* @param InputParameters
*/
static InputParameters validParams();
OutputObjectTest(const InputParameters & parameters);
/**
* Class destructor
*/
virtual ~OutputObjectTest();
void initialSetup();
private:
MooseEnum _type;
};