PatchSidesetGenerator

Description

This mesh generator splits a given sideset (sideset parameter) into n pieces (n_patches). The pieces are referred to as patches. Patches are used for net radiation transfer method via view factors. The sideset is divided into n patches using partitioner that are available from libMesh. The new sidesets are named <old_side_name>_<id>, where <id> is a number running from 0 to n - 1.

In addition to libMesh partitioners, this mesh generator also supports a grid partitioner. The grid partitioner superimposes a 3-dimensional (where $var element = document.getElementById("moose-equation-c497cf1d-e151-4b17-a53d-5742afe0383e");katex.render("d", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ is the dimensionality of the problem) uniform, orthogonal grid over the sideset and partitions the elements according to where the centroids of the sideset faces fall on the orthogonal grid. The superimposed grid is congruent to the bounding box of the sideset to ensure that the sideset is completely encompassed within the superimposed grid.

The superimposed orthogonal grid is _always_ 3-dimensional because the sideset (surface in 3D and line in 2D problems) does not need to be orthogonal to any of the coordinate axes. The superimposed 3-dimensional mesh is aligned with the coordinate axis and will have a single element in 1 (2) directions for 3 (2)-dimensional problems. These are discussed in turn:

for 2-dimensional problems, sidesets are a collection of line segments so sidesets are 1-dimensional. The bounding box of the sideset is computed and the largest distance along any of the three axes is computed (i.e. $var element = document.getElementById("moose-equation-b0b07589-d08f-4d30-bb64-79a3574eab1f");katex.render("\\max (x_{\\text{max}}-x_{\\text{min}}, y_{\\text{max}}-z_{\\text{min}},x_{\\text{max}}-z_{\\text{min}})", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ ). The superimposed mesh has n_patches subdivisions along the longest axis and a single subdivision along the two shorter axes.
for 3-dimensional problems, sidesets are a collection of faces so sidesets are 2-dimensional. The bounding box of the sideset is computed and the two largest distance along any of the three axes is computed (i.e. two largest from set $var element = document.getElementById("moose-equation-d5649c4c-1882-45fd-aa21-9eef53a66a69");katex.render("\\{x_{\\text{max}}-x_{\\text{min}}, y_{\\text{max}}-z_{\\text{min}},x_{\\text{max}}-z_{\\text{min}}\\}", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ ). The superimposed mesh has a single subdivision along the axes with the smallest extent. The number of elements along the two larger dimensions are determined as follows:
$var element = document.getElementById("moose-equation-36b61fd1-fb14-4019-b763-9840f86d3bfb");katex.render("\\begin{aligned} n_1 &= \\lfloor \\sqrt{\\frac{\\Delta_1}{\\Delta_2} n_p} \\rfloor \\\\ n_2 &= \\lfloor \\sqrt{\\frac{\\Delta_2}{\\Delta_1} n_p} \\rfloor, \\end{aligned} ", element, {displayMode:true,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$
where $var element = document.getElementById("moose-equation-843f3472-72f6-4d7c-be09-f3676313649c");katex.render("n_1", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ and $var element = document.getElementById("moose-equation-cf9089bb-7792-4e4e-94f0-9b931c448737");katex.render("n_2", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ are the subdivisions along the longest and second longest axes and $var element = document.getElementById("moose-equation-e4488e9f-729a-4869-b0c2-7ade162603fe");katex.render("n_p", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ is equal to n_patches. Due to the rounding, the $var element = document.getElementById("moose-equation-2281520b-75a1-4ce8-9b7a-f7184891a004");katex.render("n_1 \\cdot n_2", element, {displayMode:false,throwOnError:false,macros:{"\\eqc":"\\,,","\\eqp":"\\,.","\\pd":"\\frac{\\partial #1}{\\partial #2}","\\pr":"\\left(#1\\right)","\\ddt":"\\frac{d #1}{d t}"}});$ does not need to be equal to n_patches so the number of patches might be adjusted. A warning is printed if that happens.

Example Input Syntax

  [patch]
    type = PatchSidesetGenerator
    boundary = 0
    n_patches = 10
    input = cmg
  []

Input Parameters

boundaryThe boundary that will be divided into patches
C++ Type:BoundaryName
Controllable:No
Description:The boundary that will be divided into patches
inputThe mesh we want to modify
C++ Type:MeshGeneratorName
Controllable:No
Description:The mesh we want to modify
n_patchesNumber of patches
C++ Type:unsigned int
Controllable:No
Description:Number of patches

Required Parameters

centroid_partitioner_directionSpecifies the sort direction if using the centroid partitioner. Available options: x, y, z, radial
C++ Type:MooseEnum
Options:x, y, z, radial
Controllable:No
Description:Specifies the sort direction if using the centroid partitioner. Available options: x, y, z, radial
partitionerdefaultSpecifies a mesh partitioner to use when splitting the mesh for a parallel computation.
Default:default
C++ Type:MooseEnum
Options:default, metis, parmetis, linear, centroid, hilbert_sfc, morton_sfc, grid
Controllable:No
Description:Specifies a mesh partitioner to use when splitting the mesh for a parallel computation.

Partitioning 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:No
Description:Set the enabled status of the MooseObject.
save_with_nameKeep the mesh from this mesh generator in memory with the name specified
C++ Type:std::string
Controllable:No
Description:Keep the mesh from this mesh generator in memory with the name specified

Advanced Parameters

nemesisFalseWhether or not to output the mesh file in the nemesisformat (only if output = true)
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not to output the mesh file in the nemesisformat (only if output = true)
outputFalseWhether or not to output the mesh file after generating the mesh
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not to output the mesh file after generating the mesh
show_infoFalseWhether or not to show mesh info after generating the mesh (bounding box, element types, sidesets, nodesets, subdomains, etc)
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not to show mesh info after generating the mesh (bounding box, element types, sidesets, nodesets, subdomains, etc)

Debugging Parameters

Input Files

(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch_grid.i)
(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch.i)
(modules/navier_stokes/test/tests/finite_volume/ins/exceptions/bad-restriction.i)
(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch_grid_2D.i)
(modules/heat_transfer/test/tests/radiation_transfer_action/radiative_transfer_no_action.i)
(modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/2d-rc.i)
(modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/segregated/2d-segregated-block.i)

(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch.i)

[Mesh]
  type = MeshGeneratorMesh

  [cmg]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 1
    nx = 25
    ymin = 0
    ymax = 1
    ny = 25
    zmin = 0
    zmax = 1
    nz = 25
  []

  [patch]
    type = PatchSidesetGenerator
    boundary = 0
    n_patches = 10
    input = cmg
  []
[]

(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch_grid.i)

[Mesh]
  type = MeshGeneratorMesh

  [cmg]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 3
    nx = 25
    ymin = 0
    ymax = 2
    ny = 25
    zmin = 0
    zmax = 4
    nz = 25
  []

  [patch]
    type = PatchSidesetGenerator
    boundary = back
    n_patches = 19
    input = cmg
    partitioner = grid
  []
[]

(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch.i)

[Mesh]
  type = MeshGeneratorMesh

  [cmg]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 1
    nx = 25
    ymin = 0
    ymax = 1
    ny = 25
    zmin = 0
    zmax = 1
    nz = 25
  []

  [patch]
    type = PatchSidesetGenerator
    boundary = 0
    n_patches = 10
    input = cmg
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/exceptions/bad-restriction.i)

mu=1.1
rho=1.1
advected_interp_method='average'
velocity_interp_method='rc'

restricted_blocks = '1'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    block = '1 2'
    pressure = pressure
  []
[]

[Mesh]
  parallel_type = 'replicated'
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1'
    dy = '1'
    ix = '7 7'
    iy = 10
    subdomain_id = '1 2'
  []
  [mid]
    type = SideSetsBetweenSubdomainsGenerator
    primary_block = 1
    paired_block = 2
    input = mesh
    new_boundary = 'middle'
  []
  [break_top]
    type = PatchSidesetGenerator
    boundary = 'top'
    n_patches = 2
    input = mid
  []
  [break_bottom]
    type = PatchSidesetGenerator
    boundary = 'bottom'
    n_patches = 2
    input = break_top
  []
[]

[Problem]
  kernel_coverage_check = false
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    block = ${restricted_blocks}
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
    block = ${restricted_blocks}
  []
  [pressure]
    type = INSFVPressureVariable
    block = ${restricted_blocks}
  []
  [temperature]
    type = INSFVEnergyVariable
    block = ${restricted_blocks}
  []
  [scalar]
    type = INSFVScalarFieldVariable
    block = ${restricted_blocks}
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []

  [energy_advection]
    type = INSFVEnergyAdvection
    variable = temperature
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = 1.1
    variable = temperature
  []
  [energy_loss]
    type = FVBodyForce
    variable = temperature
    value = -0.1
  []

  [scalar_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_diffusion]
    type = FVDiffusion
    coeff = 1
    variable = scalar
  []
  [scalar_src]
    type = FVBodyForce
    variable = scalar
    value = 0.1
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []
  [top-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'top_0'
    variable = u
    function = 0
  []
  [top-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'top_0'
    variable = v
    function = 0
  []
  [bottom-wall-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom_0'
    variable = u
    mu = ${mu}
    u = u
    v = v
    momentum_component = 'x'
  []
  [bottom-wall-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom_0'
    variable = v
    mu = ${mu}
    u = u
    v = v
    momentum_component = 'y'
  []
  [bottom-wall-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom_0'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'middle'
    variable = pressure
    function = 0
  []
  [inlet_t]
    type = FVDirichletBC
    boundary = 'left'
    variable = temperature
    value = 1
  []
  [outlet_scalar]
    type = FVDirichletBC
    boundary = 'middle'
    variable = scalar
    value = 1
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'temperature'
    rho = ${rho}
    block = ${restricted_blocks}
  []
  [const]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '2'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      100                lu           NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

(modules/heat_transfer/test/tests/generate_radiation_patch/generate_radiation_patch_grid_2D.i)

[Mesh]
  [cartesian]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1   2  3'
    ix = '20 20 20'
    dy = '5'
    iy = '10'
    subdomain_id = '1 2 3'
  []

  [rotate]
    type = TransformGenerator
    transform = ROTATE
    vector_value = '0 0 -45'
    input = cartesian
  []

  [patch]
    type = PatchSidesetGenerator
    boundary = 0
    n_patches = 4
    input = rotate
    partitioner = grid
  []
[]

(modules/heat_transfer/test/tests/radiation_transfer_action/radiative_transfer_no_action.i)

[Problem]
  kernel_coverage_check = false
[]

[Mesh]
  type = MeshGeneratorMesh

  [./cmg]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1.3 1.9'
    ix = '3 3 3'
    dy = '2 1.2 0.9'
    iy = '3 3 3'
    subdomain_id = '0 1 0
                    4 5 2
                    0 3 0'
  [../]

  [./inner_bottom]
    type = SideSetsBetweenSubdomainsGenerator
    input = cmg
    primary_block = 1
    paired_block = 5
    new_boundary = 'inner_bottom'
  [../]

  [./inner_left]
    type = SideSetsBetweenSubdomainsGenerator
    input = inner_bottom
    primary_block = 4
    paired_block = 5
    new_boundary = 'inner_left'
  [../]

  [./inner_right]
    type = SideSetsBetweenSubdomainsGenerator
    input = inner_left
    primary_block = 2
    paired_block = 5
    new_boundary = 'inner_right'
  [../]

  [./inner_top]
    type = SideSetsBetweenSubdomainsGenerator
    input = inner_right
    primary_block = 3
    paired_block = 5
    new_boundary = 'inner_top'
  [../]

  [./rename]
    type = RenameBlockGenerator
    old_block = '1 2 3 4'
    new_block = '0 0 0 0'
    input = inner_top
  [../]

  [./split_inner_bottom]
    type = PatchSidesetGenerator
    boundary = 4
    n_patches = 2
    partitioner = centroid
    centroid_partitioner_direction = x
    input = rename
  [../]

  [./split_inner_left]
    type = PatchSidesetGenerator
    boundary = 5
    n_patches = 2
    partitioner = centroid
    centroid_partitioner_direction = y
    input = split_inner_bottom
  [../]

  [./split_inner_right]
    type = PatchSidesetGenerator
    boundary = 6
    n_patches = 2
    partitioner = centroid
    centroid_partitioner_direction = y
    input = split_inner_left
  [../]

  [./split_inner_top]
    type = PatchSidesetGenerator
    boundary = 7
    n_patches = 3
    partitioner = centroid
    centroid_partitioner_direction = x
    input = split_inner_right
  [../]
[]

[Variables]
  [./temperature]
    block = 0
  [../]
[]

[Kernels]
  [./heat_conduction]
    type = HeatConduction
    variable = temperature
    block = 0
    diffusion_coefficient = 5
  [../]
[]

[UserObjects]
  [./gray_lambert]
    type = ViewFactorObjectSurfaceRadiation
    boundary = 'inner_bottom_0 inner_bottom_1
                inner_left_0 inner_left_1
                inner_right_0 inner_right_1
                inner_top_0 inner_top_1 inner_top_2'
    fixed_temperature_boundary = 'inner_bottom_0 inner_bottom_1'
    fixed_boundary_temperatures = '1200          1200'
    adiabatic_boundary = 'inner_top_0 inner_top_1 inner_top_2'
    emissivity = '0.9 0.9
                  0.8 0.8
                  0.4 0.4
                  1 1 1'
    temperature = temperature
    view_factor_object_name = view_factor
    execute_on = 'LINEAR TIMESTEP_END'
  [../]

  [./view_factor]
    type = UnobstructedPlanarViewFactor
    boundary = 'inner_bottom_0 inner_bottom_1
                inner_left_0 inner_left_1
                inner_right_0 inner_right_1
                inner_top_0 inner_top_1 inner_top_2'
    normalize_view_factor = true
    execute_on = 'INITIAL'
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = temperature
    boundary = left
    value = 600
  [../]

  [./right]
    type = DirichletBC
    variable = temperature
    boundary = right
    value = 300
  [../]

  [./radiation]
    type = GrayLambertNeumannBC
    variable = temperature
    surface_radiation_object_name = gray_lambert
    boundary = 'inner_left_0 inner_left_1
                inner_right_0 inner_right_1'
  [../]
[]

[Postprocessors]
  [./average_T_inner_right]
    type = SideAverageValue
    variable = temperature
    boundary = inner_right
  [../]
[]

[Executioner]
  type = Steady
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/2d-rc.i)

mu = 1.1
rho = 1.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'

restricted_blocks = '1'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    block = ${restricted_blocks}
    pressure = pressure
  []
[]

[Mesh]
  parallel_type = 'replicated'
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1'
    dy = '1'
    ix = '7 7'
    iy = 10
    subdomain_id = '1 2'
  []
  [mid]
    type = SideSetsBetweenSubdomainsGenerator
    primary_block = 1
    paired_block = 2
    input = mesh
    new_boundary = 'middle'
  []
  [break_top]
    type = PatchSidesetGenerator
    boundary = 'top'
    n_patches = 2
    input = mid
  []
  [break_bottom]
    type = PatchSidesetGenerator
    boundary = 'bottom'
    n_patches = 2
    input = break_top
  []
[]

[Problem]
  kernel_coverage_check = false
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    block = ${restricted_blocks}
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
    block = ${restricted_blocks}
  []
  [pressure]
    type = INSFVPressureVariable
    block = ${restricted_blocks}
  []
  [temperature]
    type = INSFVEnergyVariable
    block = ${restricted_blocks}
  []
  [scalar]
    type = INSFVScalarFieldVariable
    block = ${restricted_blocks}
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []

  [energy_advection]
    type = INSFVEnergyAdvection
    variable = temperature
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = 1.1
    variable = temperature
  []
  [energy_loss]
    type = FVBodyForce
    variable = temperature
    value = -0.1
  []

  [scalar_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_diffusion]
    type = FVDiffusion
    coeff = 1
    variable = scalar
  []
  [scalar_src]
    type = FVBodyForce
    variable = scalar
    value = 0.1
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []
  [top-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'top_0'
    variable = u
    function = 0
  []
  [top-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'top_0'
    variable = v
    function = 0
  []
  [bottom-wall-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom_0'
    variable = u
    mu = ${mu}
    u = u
    v = v
    momentum_component = 'x'
  []
  [bottom-wall-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom_0'
    variable = v
    mu = ${mu}
    u = u
    v = v
    momentum_component = 'y'
  []
  [bottom-wall-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom_0'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'middle'
    variable = pressure
    function = 0
  []
  [inlet_t]
    type = FVDirichletBC
    boundary = 'left'
    variable = temperature
    value = 1
  []
  [outlet_scalar]
    type = FVDirichletBC
    boundary = 'middle'
    variable = scalar
    value = 1
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'temperature'
    rho = ${rho}
    block = ${restricted_blocks}
  []
  [const]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '2'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/block_restriction/segregated/2d-segregated-block.i)

mu = 1.1
rho = 1.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

restricted_blocks = '1'

[Mesh]
  parallel_type = 'replicated'
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1'
    dy = '1'
    ix = '7 7'
    iy = 10
    subdomain_id = '1 2'
  []
  [mid]
    type = SideSetsBetweenSubdomainsGenerator
    primary_block = 1
    paired_block = 2
    input = mesh
    new_boundary = 'middle'
  []
  [break_top]
    type = PatchSidesetGenerator
    boundary = 'top'
    n_patches = 2
    input = mid
  []
  [break_bottom]
    type = PatchSidesetGenerator
    boundary = 'bottom'
    n_patches = 2
    input = break_top
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system energy_system scalar_system'
  previous_nl_solution_required = true
  kernel_coverage_check = false
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    pressure = pressure
    block = ${restricted_blocks}
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1.0
    solver_sys = u_system
    two_term_boundary_expansion = false
    block = ${restricted_blocks}
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 0.0
    solver_sys = v_system
    two_term_boundary_expansion = false
    block = ${restricted_blocks}
  []
  [pressure]
    type = INSFVPressureVariable
    solver_sys = pressure_system
    initial_condition = 0.2
    two_term_boundary_expansion = false
    block = ${restricted_blocks}
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = 300
    solver_sys = energy_system
    two_term_boundary_expansion = false
    block = ${restricted_blocks}
  []
  [scalar]
    type = INSFVScalarFieldVariable
    block = ${restricted_blocks}
    solver_sys = scalar_system
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = '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
  []

  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
    boundaries_to_force = 'bottom_0'
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = 1.1
    variable = T_fluid
  []
  [energy_loss]
    type = FVBodyForce
    variable = T_fluid
    value = -0.1
  []

  [scalar_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
    boundaries_to_force = 'bottom_0'
  []
  [scalar_diffusion]
    type = FVDiffusion
    coeff = 1.0
    variable = scalar
  []
  [scalar_src]
    type = FVBodyForce
    variable = scalar
    value = 0.1
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1.0'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0.0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top_0'
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top_0'
    variable = vel_y
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'middle'
    variable = pressure
    function = 0
  []
  [inlet_t]
    type = FVDirichletBC
    boundary = 'left'
    variable = T_fluid
    value = 1
  []
  [outlet_scalar]
    type = FVDirichletBC
    boundary = 'middle'
    variable = scalar
    value = 1
  []
  [symmetry-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom_0'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom_0'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom_0'
    variable = pressure
  []
[]

[Executioner]
  type = SIMPLE
  momentum_l_abs_tol = 1e-12
  pressure_l_abs_tol = 1e-12
  energy_l_abs_tol = 1e-12
  passive_scalar_l_abs_tol = 1e-12
  momentum_l_tol = 0
  pressure_l_tol = 0
  energy_l_tol = 0
  passive_scalar_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  energy_system = 'energy_system'
  passive_scalar_systems = 'scalar_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  energy_equation_relaxation = 0.99
  passive_scalar_equation_relaxation = 0.99
  num_iterations = 100
  pressure_absolute_tolerance = 1e-9
  momentum_absolute_tolerance = 1e-9
  energy_absolute_tolerance = 1e-9
  passive_scalar_absolute_tolerance = 1e-9
  print_fields = false
[]

[FunctorMaterials]
  [const_functor]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '2'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
    block = ${restricted_blocks}
  []
[]

[Outputs]
  exodus = true
  csv = false
  perf_graph = false
  print_nonlinear_residuals = false
  print_linear_residuals = true
[]

Description
Example Input Syntax
Input Parameters
Input Files