- functorThe functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
C++ Type:MooseFunctorName
Unit:(no unit assumed)
Controllable:No
Description:The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
- variableThe name of the variable that this object applies to
C++ Type:AuxVariableName
Unit:(no unit assumed)
Controllable:No
Description:The name of the variable that this object applies to
FunctorAux
Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.
Overview
This object populates an elemental auxiliary variable by evaluating a functor with a cell-center/elemental or quadrature-point based argument. This functor may be a material property, a function or another variable. A cell-center/elemental argument should be used when a cell-averaged quantity (like for finite volume computations) is desired. Cell-center/elemental vs. quadrature-point based evaluations are controlled by the use_qp_arg boolean parameter. By default the parameter is false.
commentnote
The version of this auxiliary kernel for automatic differentiation (AD) functors (in particular AD material properties) is FunctorAux.
Example input syntax
In this example, we use FunctorAux to convert some material properties functors, defined by the fluid properties material, to auxiliary variables, to examine them in an Exodus output.
[AuxKernels<<<{"href": "../../syntax/AuxKernels/index.html"}>>>]
[speed]
type = VectorMagnitudeAux<<<{"description": "Creates a field representing the magnitude of three coupled variables using an Euclidean norm.", "href": "VectorMagnitudeAux.html"}>>>
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'velocity_norm'
x<<<{"description": "x-component of the vector"}>>> = u
y<<<{"description": "y-component of the vector"}>>> = v
[]
# To output the functor material properties
[rho_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'rho'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'rho_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[drho_dp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'drho/dpressure'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'drho_dp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[drho_dT_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'drho/dT_fluid'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'drho_dT_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[drho_dt_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'drho_dt'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'rho_dot_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[cp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'cp'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'cp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dcp_dp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dcp/dpressure'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dcp_dp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dcp_dT_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dcp/dT_fluid'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dcp_dT_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dcp_dt_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dcp_dt'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'cp_dot_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[cv_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'cv'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'cv_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[mu_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'mu'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'mu_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dmu_dp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dmu/dpressure'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dmu_dp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dmu_dT_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dmu/dT_fluid'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dmu_dT_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[k_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'k'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'k_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dk_dp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dk/dpressure'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dk_dp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dk_dT_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dk/dT_fluid'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dk_dT_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[Pr_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'Pr'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'Pr_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dPr_dp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dPr/dpressure'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dPr_dp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dPr_dT_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dPr/dT_fluid'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dPr_dT_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[Re_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'Re'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'Re_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dRe_dp_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dRe/dpressure'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dRe_dp_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[dRe_dT_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'dRe/dT_fluid'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'dRe_dT_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[Re_h_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'Re_h'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'Re_h_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[Re_i_out]
type = FunctorAux<<<{"description": "Evaluates a functor (variable, function or functor material property) on the current element, quadrature point, or node.", "href": "FunctorAux.html"}>>>
functor<<<{"description": "The functor to evaluate. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number."}>>> = 'Re_i'
variable<<<{"description": "The name of the variable that this object applies to"}>>> = 'Re_i_var'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'timestep_begin'
[]
[]Input Parameters
- blockThe list of blocks (ids or names) that this object will be applied
C++ Type:std::vector<SubdomainName>
Controllable:No
Description:The list of blocks (ids or names) that this object will be applied
- boundaryThe list of boundaries (ids or names) from the mesh where this object applies
C++ Type:std::vector<BoundaryName>
Controllable:No
Description:The list of boundaries (ids or names) from the mesh where this object applies
- check_boundary_restrictedTrueWhether to check for multiple element sides on the boundary in the case of a boundary restricted, element aux variable. Setting this to false will allow contribution to a single element's elemental value(s) from multiple boundary sides on the same element (example: when the restricted boundary exists on two or more sides of an element, such as at a corner of a mesh
Default:True
C++ Type:bool
Controllable:No
Description:Whether to check for multiple element sides on the boundary in the case of a boundary restricted, element aux variable. Setting this to false will allow contribution to a single element's elemental value(s) from multiple boundary sides on the same element (example: when the restricted boundary exists on two or more sides of an element, such as at a corner of a mesh
- execute_onLINEAR TIMESTEP_ENDThe list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
Default:LINEAR TIMESTEP_END
C++ Type:ExecFlagEnum
Options:XFEM_MARK, FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, LINEAR_CONVERGENCE, NONLINEAR, NONLINEAR_CONVERGENCE, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, MULTIAPP_FIXED_POINT_CONVERGENCE, FINAL, CUSTOM, PRE_DISPLACE
Controllable:No
Description:The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
- factor1A factor to apply on the functor. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
Default:1
C++ Type:MooseFunctorName
Unit:(no unit assumed)
Controllable:No
Description:A factor to apply on the functor. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.
Optional 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.
- seed0The seed for the master random number generator
Default:0
C++ Type:unsigned int
Controllable:No
Description:The seed for the master random number generator
- use_displaced_meshFalseWhether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Advanced Parameters
- prop_getter_suffixAn optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:An optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
- use_interpolated_stateFalseFor the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Default:False
C++ Type:bool
Controllable:No
Description:For the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Material Property Retrieval Parameters
Input Files
- (test/tests/variables/linearfv/diffusion-1d-aux.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux.i)
- (test/tests/functormaterials/smoother/test.i)
- (test/tests/vectorpostprocessors/extra_id_integral/functor_test.i)
- (test/tests/auxkernels/functor_coordinates_function_aux/test.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d-functor-material.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/solidification/pipe_solidification.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc-action.i)
- (test/tests/functors/matching-analytic-solution/test.i)
- (modules/navier_stokes/test/tests/finite_volume/materials/mixture_material/mixture.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-transient.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/multiapp-scalar-transport/fluid-flow.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected-action.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/lid-driven-two-phase.i)
- (modules/heat_transfer/test/tests/functormaterials/cylindrical_gap_heat_flux_functor_material/cylindrical_gap_heat_flux_functor_material.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d-parsed-function.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc.i)
- (test/tests/materials/functor_properties/vector-magnitude/test.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-advection-slip.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/pressure_driven_growth_transient.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/solidification/solidification_no_advection.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/pressure_driven_growth.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/wcnsfv.i)
- (modules/navier_stokes/test/tests/finite_volume/fvbcs/FVFunctorHeatFluxBC/wall_heat_transfer.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/turbulent_driven_growth.i)
- (modules/combined/test/tests/subchannel_thm_coupling/subchannel.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation-physics.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp.i)
- (modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/natural_convection/natural_circulation_pipe.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/materials/functorfluidprops.i)
- (modules/navier_stokes/test/tests/finite_volume/materials/ergun/ergun.i)
- (modules/navier_stokes/examples/laser-welding/2d-fv.i)
- (test/tests/materials/functor_properties/vector-magnitude/vector-test.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/rayleigh-bernard-two-phase.i)
- (test/tests/meshdivisions/block_division.i)
- (modules/navier_stokes/examples/solidification/gallium_melting.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-w-interface-area.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/lid-driven-two-phase-physics.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/lid-driven-two-phase-physics.i)
(modules/navier_stokes/test/tests/finite_volume/wcns/materials/functorfluidprops.i)
# Operating conditions
inlet_temp = 300
outlet_pressure = 1e5
inlet_v = 4
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 1
nx = 5
ny = 5
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = ${inlet_v}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 2
[]
[pressure]
type = INSFVPressureVariable
initial_condition = ${outlet_pressure}
[]
[T]
type = INSFVEnergyVariable
initial_condition = ${inlet_temp}
[]
[]
[FVKernels]
[u_time]
type = FVFunctorTimeKernel
variable = u
[]
[v_time]
type = FVFunctorTimeKernel
variable = v
[]
[p_time]
type = FVFunctorTimeKernel
variable = pressure
[]
[T_time]
type = FVFunctorTimeKernel
variable = T
[]
[]
[FluidProperties]
[fp]
type = FlibeFluidProperties
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = fp
pressure = 'pressure'
T_fluid = 'T'
speed = 'velocity_norm'
# For porous flow
characteristic_length = 2
porosity = 'porosity'
[]
[]
[AuxVariables]
[velocity_norm]
type = MooseVariableFVReal
[]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.4
[]
[rho_var]
type = MooseVariableFVReal
[]
[drho_dp_var]
type = MooseVariableFVReal
[]
[drho_dT_var]
type = MooseVariableFVReal
[]
[rho_dot_var]
type = MooseVariableFVReal
[]
[cp_var]
type = MooseVariableFVReal
[]
[dcp_dp_var]
type = MooseVariableFVReal
[]
[dcp_dT_var]
type = MooseVariableFVReal
[]
[cp_dot_var]
type = MooseVariableFVReal
[]
[cv_var]
type = MooseVariableFVReal
[]
[mu_var]
type = MooseVariableFVReal
[]
[dmu_dp_var]
type = MooseVariableFVReal
[]
[dmu_dT_var]
type = MooseVariableFVReal
[]
[k_var]
type = MooseVariableFVReal
[]
[dk_dp_var]
type = MooseVariableFVReal
[]
[dk_dT_var]
type = MooseVariableFVReal
[]
[Pr_var]
type = MooseVariableFVReal
[]
[dPr_dp_var]
type = MooseVariableFVReal
[]
[dPr_dT_var]
type = MooseVariableFVReal
[]
[Re_var]
type = MooseVariableFVReal
[]
[dRe_dp_var]
type = MooseVariableFVReal
[]
[dRe_dT_var]
type = MooseVariableFVReal
[]
[Re_h_var]
type = MooseVariableFVReal
[]
[Re_i_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[speed]
type = VectorMagnitudeAux
variable = 'velocity_norm'
x = u
y = v
[]
# To output the functor material properties
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'timestep_begin'
[]
[drho_dp_out]
type = FunctorAux
functor = 'drho/dpressure'
variable = 'drho_dp_var'
execute_on = 'timestep_begin'
[]
[drho_dT_out]
type = FunctorAux
functor = 'drho/dT_fluid'
variable = 'drho_dT_var'
execute_on = 'timestep_begin'
[]
[drho_dt_out]
type = FunctorAux
functor = 'drho_dt'
variable = 'rho_dot_var'
execute_on = 'timestep_begin'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'timestep_begin'
[]
[dcp_dp_out]
type = FunctorAux
functor = 'dcp/dpressure'
variable = 'dcp_dp_var'
execute_on = 'timestep_begin'
[]
[dcp_dT_out]
type = FunctorAux
functor = 'dcp/dT_fluid'
variable = 'dcp_dT_var'
execute_on = 'timestep_begin'
[]
[dcp_dt_out]
type = FunctorAux
functor = 'dcp_dt'
variable = 'cp_dot_var'
execute_on = 'timestep_begin'
[]
[cv_out]
type = FunctorAux
functor = 'cv'
variable = 'cv_var'
execute_on = 'timestep_begin'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'timestep_begin'
[]
[dmu_dp_out]
type = FunctorAux
functor = 'dmu/dpressure'
variable = 'dmu_dp_var'
execute_on = 'timestep_begin'
[]
[dmu_dT_out]
type = FunctorAux
functor = 'dmu/dT_fluid'
variable = 'dmu_dT_var'
execute_on = 'timestep_begin'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'timestep_begin'
[]
[dk_dp_out]
type = FunctorAux
functor = 'dk/dpressure'
variable = 'dk_dp_var'
execute_on = 'timestep_begin'
[]
[dk_dT_out]
type = FunctorAux
functor = 'dk/dT_fluid'
variable = 'dk_dT_var'
execute_on = 'timestep_begin'
[]
[Pr_out]
type = FunctorAux
functor = 'Pr'
variable = 'Pr_var'
execute_on = 'timestep_begin'
[]
[dPr_dp_out]
type = FunctorAux
functor = 'dPr/dpressure'
variable = 'dPr_dp_var'
execute_on = 'timestep_begin'
[]
[dPr_dT_out]
type = FunctorAux
functor = 'dPr/dT_fluid'
variable = 'dPr_dT_var'
execute_on = 'timestep_begin'
[]
[Re_out]
type = FunctorAux
functor = 'Re'
variable = 'Re_var'
execute_on = 'timestep_begin'
[]
[dRe_dp_out]
type = FunctorAux
functor = 'dRe/dpressure'
variable = 'dRe_dp_var'
execute_on = 'timestep_begin'
[]
[dRe_dT_out]
type = FunctorAux
functor = 'dRe/dT_fluid'
variable = 'dRe_dT_var'
execute_on = 'timestep_begin'
[]
[Re_h_out]
type = FunctorAux
functor = 'Re_h'
variable = 'Re_h_var'
execute_on = 'timestep_begin'
[]
[Re_i_out]
type = FunctorAux
functor = 'Re_i'
variable = 'Re_i_var'
execute_on = 'timestep_begin'
[]
[]
[Executioner]
type = Transient
end_time = 0.1
dt = 0.1
[]
[Outputs]
exodus = true
[]
(test/tests/variables/linearfv/diffusion-1d-aux.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 10
[]
[]
[Problem]
linear_sys_names = 'u_sys'
[]
[Variables]
[u]
type = MooseLinearVariableFVReal
solver_sys = 'u_sys'
initial_condition = 1.0
[]
[]
[AuxVariables]
[v_volume]
type = MooseLinearVariableFVReal
initial_condition = 50
[]
[v_functor]
type = MooseLinearVariableFVReal
initial_condition = 25
[]
[v_parsed]
type = MooseLinearVariableFVReal
initial_condition = 12.5
[]
[]
[AuxKernels]
[volume]
type = VolumeAux
variable = v_volume
[]
[functor]
type = FunctorAux
variable = v_functor
functor = u
[]
[parsed]
type = ParsedAux
variable = v_parsed
coupled_variables = 'v_volume v_functor'
expression = '0.5*v_volume+0.5*v_functor'
[]
[]
[LinearFVKernels]
[diffusion]
type = LinearFVDiffusion
variable = u
diffusion_coeff = coeff_func
[]
[source]
type = LinearFVSource
variable = u
source_density = source_func
[]
[]
[LinearFVBCs]
[dir]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = u
boundary = "left right"
functor = analytic_solution
[]
[]
[Functions]
[coeff_func]
type = ParsedFunction
expression = '0.5*x'
[]
[source_func]
type = ParsedFunction
expression = '2*x'
[]
[analytic_solution]
type = ParsedFunction
expression = '1-x*x'
[]
[]
[Executioner]
type = Steady
system_names = u_sys
l_tol = 1e-10
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
exodus = true
execute_on = TIMESTEP_END
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 5}'
ymin = '${fparse -l / 2}'
ymax = '${fparse l / 2}'
nx = 10
ny = 4
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_x
rho_d = ${rho_d}
fd = 'phase_2'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_friction]
type = PINSFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
is_porous_medium = false
momentum_component = x
mu = mu_mixture
rho = rho_mixture
variable = vel_x
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_y
rho_d = ${rho_d}
fd = 'phase_2'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_friction]
type = PINSFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
is_porous_medium = false
momentum_component = y
mu = mu_mixture
rho = rho_mixture
variable = vel_y
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FunctorMaterials]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
outputs = 'out'
output_properties = 'vel_slip_x'
ghost_layers = 5
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
outputs = 'out'
output_properties = 'vel_slip_y'
ghost_layers = 5
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
outputs = 'out'
output_properties = 'phase_1'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = '${rho_d} ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
print_linear_residuals = true
print_nonlinear_residuals = true
[out]
type = Exodus
hide = 'Re lin cum_lin'
[]
[perf]
type = PerfGraphOutput
[]
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
[]
[lin]
type = NumLinearIterations
[]
[cum_lin]
type = CumulativeValuePostprocessor
postprocessor = lin
[]
[]
(test/tests/functormaterials/smoother/test.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 100
ny = 1
xmax = 10
ymax = 1
[]
[]
[AuxVariables]
[checkerboard]
type = MooseVariableFVReal
[]
[smooth]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[checker]
type = ParsedAux
variable = checkerboard
# nonlinear growth to challenge the smoother a bit
expression = '2 + x * x * sin(PI * 10 * x)'
constant_names = 'PI'
constant_expressions = '3.14159265359'
use_xyzt = true
execute_on = 'TIMESTEP_BEGIN'
[]
[smooth]
type = FunctorAux
variable = smooth
functor = 'smoothed_functor'
execute_on = 'TIMESTEP_END'
[]
[]
[FunctorMaterials]
[smooth]
type = FunctorSmoother
functors_in = 'checkerboard'
functors_out = 'smoothed_functor'
# Using the face values will not smooth a checkerboard because the 'extreme' neighbor value are
# mixed with the element value
# Using the layered element average will smooth a checkerboard in 2D inside the volume, and fail to do so
# near the boundaries. In 1D it wont fix a checkboard as it does not average with the local value
# smoothing_technique = 'layered_elem_average'
smoothing_technique = 'remove_checkerboard'
# smoothing_technique = 'face_average'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[VectorPostprocessors]
[line]
type = LineValueSampler
variable = 'smooth'
num_points = 100
start_point = '0.05 0.5 0'
end_point = '9.95 0.5 0'
sort_by = 'x'
[]
[]
[Outputs]
exodus = true
[out]
type = CSV
execute_on = 'TIMESTEP_END'
[]
[]
(test/tests/vectorpostprocessors/extra_id_integral/functor_test.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
nx = 5
ny = 5
subdomain_ids = '0 0 0 0 0
0 0 0 0 0
1 1 1 1 1
1 1 1 1 1
1 1 1 1 1'
[]
[add_id]
type = ParsedExtraElementIDGenerator
input = gmg
extra_elem_integer_name = id
expression = 'if(x<0.2,1,2)'
[]
[]
[Variables]
[u]
order = FIRST
family = LAGRANGE
[]
[]
[Kernels]
[diff]
type = Diffusion
variable = u
[]
[bf]
type = BodyForce
variable = u
value = 1
[]
[]
[BCs]
[top]
type = DirichletBC
variable = u
boundary = top
value = 0
[]
[right]
type = DirichletBC
variable = u
boundary = right
value = 0
[]
[]
[VectorPostprocessors]
[eeid]
type = ExtraIDIntegralVectorPostprocessor
id_name = id
variable = u
force_preaux = true
#spatial_value_name = u
[]
[]
[AuxVariables]
[v]
family = MONOMIAL
order = CONSTANT
[AuxKernel]
type = FunctorAux
functor = eeid
execute_on = timestep_end
[]
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/auxkernels/functor_coordinates_function_aux/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -1
xmax = 1
ymin = -1
ymax = 1
nx = 3
ny = 3
elem_type = QUAD9
[]
[AuxVariables]
# These aux-variables are used as argument functors to the FunctorAbuseAux
[x_var]
initial_condition = 1
[]
[y_var]
type = MooseVariableFVReal
[]
[temperature]
initial_condition = 300
[]
# These are example output variables computed by the FunctorAbuseAux
[density]
[]
[multiple_dependency_test]
type = MooseVariableFVReal
[]
[higher_order_test]
family = MONOMIAL
order = SECOND
[]
[]
[Functions]
[density_correlation]
type = ParsedFunction
expression = '900 - t'
[]
[multi_dependency]
type = ParsedFunction
expression = 't*((x*x)+(y*y) + z)'
[]
[y_function]
type = ParsedFunction
expression = 'y'
[]
# Function used as a functor for the test
[time_function]
type = ParsedFunction
expression = '1 + 2 * t'
[]
[]
[Postprocessors]
# Postprocessor used as a functor for the test
[z_pp]
type = Receiver
default = 30
[]
[]
[AuxKernels]
[set_density]
type = FunctorCoordinatesFunctionAux
variable = density
function = density_correlation
t_functor = 'temperature'
x_functor = 0
y_functor = 0
z_functor = 0
[]
[set_y]
type = FunctorAux
functor = 'y_function'
variable = 'y_var'
# this auxkernel must execute before the y_var functor is used
# in the FunctorCoordinatesFunctionAux if we want y to be up to date!
execute_on = 'INITIAL'
[]
[set_complex_dependency_fv]
type = FunctorCoordinatesFunctionAux
variable = multiple_dependency_test
function = multi_dependency
t_functor = 'time_function'
x_functor = 'x_var'
y_functor = 'y_var'
z_functor = 'z_pp'
[]
[set_complex_dependency_higher_order]
type = FunctorCoordinatesFunctionAux
variable = higher_order_test
function = multi_dependency
t_functor = 'time_function'
x_functor = 'x_var'
y_functor = 'y_var'
z_functor = 'z_pp'
[]
[]
[Executioner]
type = Steady
[]
[Problem]
solve = false
[]
[Outputs]
exodus = true
hide = 'x_var y_var z_pp temperature'
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d-functor-material.i)
rho = 1.1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '3 3'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = BernoulliPressureVariable
u = u
porosity = porosity
rho = ${rho}
[]
[]
[AuxVariables]
[has_porosity_jump_face]
type = MooseVariableFVReal
[]
[porosity_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[has_porosity_jump_face]
type = HasPorosityJumpFace
porosity = porosity
execute_on = 'initial timestep_end'
variable = has_porosity_jump_face
[]
[porosity_out]
type = FunctorAux
variable = porosity_out
functor = porosity
execute_on = 'initial timestep_end'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 1
[]
[]
[FunctorMaterials]
[porosity]
type = ADPiecewiseByBlockFunctorMaterial
prop_name = 'porosity'
subdomain_to_prop_value = '1 1 2 0.5'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/solidification/pipe_solidification.i)
mu = 8.8871e-4
rho_solid = 997.561
rho_liquid = 997.561
k_solid = 0.6203
k_liquid = 0.6203
cp_solid = 4181.72
cp_liquid = 4181.72
L = 3e5
T_liquidus = 285
T_solidus = 280
advected_interp_method = 'average'
velocity_interp_method = 'rc'
U_inlet = '${fparse 0.5 * mu / rho_liquid / 0.5}'
T_inlet = 300.0
T_cold = 200.0
Nx = 30
Ny = 5
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
coord_type = 'RZ'
rz_coord_axis = 'X'
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = '${fparse 0.5 * 1.0}'
nx = ${Nx}
ny = ${Ny}
bias_y = '${fparse 1 / 1.2}'
[]
[rename1]
type = RenameBoundaryGenerator
input = gen
old_boundary = 'left'
new_boundary = 'inlet'
[]
[rename2]
type = RenameBoundaryGenerator
input = rename1
old_boundary = 'right'
new_boundary = 'outlet'
[]
[rename3]
type = RenameBoundaryGenerator
input = rename2
old_boundary = 'bottom'
new_boundary = 'symmetry'
[]
[rename4]
type = RenameBoundaryGenerator
input = rename3
old_boundary = 'top'
new_boundary = 'wall'
[]
[rename5]
type = ParsedGenerateSideset
input = rename4
normal = '0 1 0'
combinatorial_geometry = 'x>2.0 & x<8.0 & y>0.49999'
new_sideset_name = 'cooled_wall'
[]
[]
[AuxVariables]
[U]
type = MooseVariableFVReal
[]
[fl]
type = MooseVariableFVReal
initial_condition = 1.0
[]
[density]
type = MooseVariableFVReal
[]
[th_cond]
type = MooseVariableFVReal
[]
[cp_var]
type = MooseVariableFVReal
[]
[darcy_coef]
type = MooseVariableFVReal
[]
[fch_coef]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[compute_fl]
type = NSLiquidFractionAux
variable = fl
temperature = T
T_liquidus = '${T_liquidus}'
T_solidus = '${T_solidus}'
execute_on = 'TIMESTEP_END'
[]
[rho_out]
type = FunctorAux
functor = 'rho_mixture'
variable = 'density'
[]
[th_cond_out]
type = FunctorAux
functor = 'k_mixture'
variable = 'th_cond'
[]
[cp_out]
type = FunctorAux
functor = 'cp_mixture'
variable = 'cp_var'
[]
[darcy_out]
type = FunctorAux
functor = 'Darcy_coefficient'
variable = 'darcy_coef'
[]
[fch_out]
type = FunctorAux
functor = 'Forchheimer_coefficient'
variable = 'fch_coef'
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
[]
[pressure]
type = INSFVPressureVariable
[]
[T]
type = INSFVEnergyVariable
initial_condition = '${T_inlet}'
scaling = 1.0
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = rho_mixture
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = rho_mixture
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = rho_mixture
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
[]
[u_friction]
type = PINSFVMomentumFriction
variable = vel_x
momentum_component = 'x'
u = vel_x
v = vel_y
Darcy_name = 'Darcy_coeff'
Forchheimer_name = 'Forchheimer_coeff'
rho = ${rho_liquid}
mu = ${mu}
standard_friction_formulation = false
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = rho_mixture
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = rho_mixture
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
[]
[v_friction]
type = PINSFVMomentumFriction
variable = vel_y
momentum_component = 'y'
u = vel_x
v = vel_y
Darcy_name = 'Darcy_coeff'
Forchheimer_name = 'Forchheimer_coeff'
rho = ${rho_liquid}
mu = ${mu}
standard_friction_formulation = false
[]
[T_time]
type = INSFVEnergyTimeDerivative
variable = T
rho = rho_mixture
dh_dt = dh_dt
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = T
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = FVDiffusion
coeff = k_mixture
variable = T
[]
[energy_source]
type = NSFVPhaseChangeSource
variable = T
L = ${L}
liquid_fraction = fl
T_liquidus = ${T_liquidus}
T_solidus = ${T_solidus}
rho = 'rho_mixture'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'inlet'
variable = vel_x
function = '${U_inlet}'
[]
[sym_u]
type = INSFVSymmetryVelocityBC
boundary = 'symmetry'
variable = vel_x
u = vel_x
v = vel_y
mu = ${mu}
momentum_component = 'x'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'inlet'
variable = vel_y
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'wall'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'wall'
variable = vel_y
function = 0
[]
[sym_v]
type = INSFVSymmetryVelocityBC
boundary = 'symmetry'
variable = vel_y
u = vel_x
v = vel_y
mu = ${mu}
momentum_component = y
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'outlet'
variable = pressure
function = 0
[]
[sym_p]
type = INSFVSymmetryPressureBC
boundary = 'symmetry'
variable = pressure
[]
[sym_T]
type = INSFVSymmetryScalarBC
variable = T
boundary = 'symmetry'
[]
[cooled_wall]
type = FVFunctorDirichletBC
variable = T
functor = '${T_cold}'
boundary = 'cooled_wall'
[]
[]
[FunctorMaterials]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
rho = rho_mixture
cp = cp_mixture
temperature = 'T'
[]
[eff_cp]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${cp_solid} ${k_solid} ${rho_solid}'
phase_1_names = '${cp_liquid} ${k_liquid} ${rho_liquid}'
prop_names = 'cp_mixture k_mixture rho_mixture'
phase_1_fraction = fl
[]
[mushy_zone_resistance]
type = INSFVMushyPorousFrictionFunctorMaterial
liquid_fraction = 'fl'
mu = '${mu}'
rho_l = '${rho_liquid}'
[]
[friction]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coeff Forchheimer_coeff'
prop_values = 'darcy_coef darcy_coef darcy_coef fch_coef fch_coef fch_coef'
[]
[]
[Executioner]
type = Transient
dt = 5e3
end_time = 1e4
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_abs_tol = 1e-8
nl_max_its = 12
[]
[Postprocessors]
[average_T]
type = ElementAverageValue
variable = T
outputs = csv
execute_on = FINAL
[]
[]
[VectorPostprocessors]
[sat]
type = LineValueSampler
warn_discontinuous_face_values = false
start_point = '0.0 0 0'
end_point = '10.0 0 0'
num_points = '${Nx}'
sort_by = x
variable = 'T'
execute_on = FINAL
[]
[]
[Outputs]
exodus = true
[csv]
type = CSV
execute_on = 'FINAL'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc-action.i)
mu = 0.01
rho = 2000
u_inlet = 1
advected_interp_method = 'upwind'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 1
nx = 10
ny = 6
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[speed_output]
type = MooseVariableFVReal
[]
[vel_x_output]
type = MooseVariableFVReal
[]
[vel_y_output]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[speed]
type = FunctorAux
variable = 'speed_output'
functor = 'speed'
[]
[vel_x]
type = ADFunctorVectorElementalAux
variable = 'vel_x_output'
functor = 'velocity'
component = 0
[]
[vel_y]
type = ADFunctorVectorElementalAux
variable = 'vel_y_output'
functor = 'velocity'
component = 1
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'incompressible'
porous_medium_treatment = true
density = ${rho}
dynamic_viscosity = ${mu}
porosity = 'porosity'
initial_velocity = '${u_inlet} 1e-6 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_function = '${u_inlet} 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip symmetry'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '0.1'
momentum_advection_interpolation = ${advected_interp_method}
mass_advection_interpolation = ${advected_interp_method}
[]
[]
[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
nl_abs_tol = 1e-11
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/functors/matching-analytic-solution/test.i)
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 20
[]
[]
[Variables]
[u]
[]
[]
[AuxVariables]
[nodal]
[]
[elemental]
type = MooseVariableFVReal
[]
[elemental_grad]
type = MooseVariableFVReal
[]
[elemental_dot]
type = MooseVariableFVReal
[]
[elemental_grad_dot]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[nodal]
type = FunctorAux
functor = u
variable = nodal
[]
[elemental]
type = FunctorAux
functor = u
variable = elemental
[]
[elemental_dot]
type = FunctorAux
functor = dmat_dt
variable = elemental_dot
[]
[elemental_grad]
type = FunctorVectorElementalAux
functor = grad_mat
component = 0
variable = elemental_grad
[]
[elemental_grad_dot]
type = FunctorVectorElementalAux
functor = grad_dmat_dt
component = 0
variable = elemental_grad_dot
[]
[]
[Functions]
[analytic]
type = ParsedFunction
expression = 'x*t'
[]
[grad]
type = ParsedFunction
expression = 't'
[]
[dot]
type = ParsedFunction
expression = 'x'
[]
[grad_dot]
type = ParsedFunction
expression = '1'
[]
[]
[FunctorMaterials]
[val_dot_grad_dot]
type = ADGenericFunctorMaterial
prop_names = 'mat'
prop_values = 'u'
[]
[grad]
type = ADGenericFunctorGradientMaterial
prop_names = 'grad_mat'
prop_values = 'u'
[]
[]
[NodalKernels]
[rxn]
type = ReactionNodalKernel
variable = u
[]
[ffn]
type = UserForcingFunctorNodalKernel
variable = u
functor = analytic
[]
[]
[Executioner]
type = Transient
solve_type = NEWTON
num_steps = 1
dt = 1
[]
[Postprocessors]
[u_err]
type = ElementL2FunctorError
approximate = u
exact = analytic
[]
[nodal_err]
type = ElementL2FunctorError
approximate = nodal
exact = analytic
[]
[elemental_err]
type = ElementL2FunctorError
approximate = elemental
exact = analytic
[]
[dot_err]
type = ElementL2FunctorError
approximate = elemental_dot
exact = dot
[]
[grad_err]
type = ElementL2FunctorError
approximate = elemental_grad
exact = grad
[]
[grad_dot_err]
type = ElementL2FunctorError
approximate = elemental_grad_dot
exact = grad_dot
[]
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/materials/mixture_material/mixture.i)
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
nx = 5
[]
[]
[AuxVariables]
[fl]
type = MooseVariableFVReal
[]
[cp]
type = MooseVariableFVReal
[]
[k]
type = MooseVariableFVReal
[]
[]
[ICs]
[FunctionIC]
type = FunctionIC
variable = fl
function = 'x'
[]
[]
[AuxKernels]
[cp_aux]
type = FunctorAux
functor = cp_mixture
variable = cp
[]
[k_aux]
type = FunctorAux
functor = k_mixture
variable = k
[]
[]
[VectorPostprocessors]
[cp]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '0.9 0 0'
num_points = 5
variable = cp
sort_by = x
[]
[k]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '0.9 0 0'
num_points = 5
variable = k
sort_by = x
[]
[fl]
type = LineValueSampler
start_point = '0.1 0 0'
end_point = '0.9 0 0'
num_points = 5
variable = fl
sort_by = x
[]
[]
[Functions]
[cp_solid]
type = ADParsedFunction
expression = '1 - x'
[]
[cp_liquid]
type = ADParsedFunction
expression = 'x'
[]
[k_solid]
type = ADParsedFunction
expression = '2 - 3*x'
[]
[k_liquid]
type = ADParsedFunction
expression = '3*x'
[]
[]
[FunctorMaterials]
[eff_cp]
type = NSFVMixtureFunctorMaterial
phase_2_names = 'cp_solid k_solid'
phase_1_names = 'cp_liquid k_liquid'
prop_names = 'cp_mixture k_mixture'
phase_1_fraction = fl
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-transient.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 5}'
ymin = '${fparse -l / 2}'
ymax = '${fparse l / 2}'
nx = 10
ny = 4
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_x
rho_d = ${rho_d}
fd = 'phase_2'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_friction]
type = PINSFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
is_porous_medium = false
momentum_component = x
mu = mu_mixture
rho = rho_mixture
variable = vel_x
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_y
rho_d = ${rho_d}
fd = 'phase_2'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_friction]
type = PINSFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
is_porous_medium = false
momentum_component = y
mu = mu_mixture
rho = rho_mixture
variable = vel_y
[]
[phase_2_time]
type = FVFunctorTimeKernel
variable = phase_2
functor = phase_2
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[vel_slip_x_var]
type = MooseVariableFVReal
[]
[vel_slip_y_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[populate_vx_slip_var]
type = FunctorAux
variable = vel_slip_x_var
functor = 'vel_slip_x'
[]
[populate_vy_slip_var]
type = FunctorAux
variable = vel_slip_y_var
functor = 'vel_slip_y'
[]
[]
[FunctorMaterials]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = '${rho_d} ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
dt = 0.1
end_time = 1.0
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
exodus = false
[CSV]
type = CSV
execute_on = 'TIMESTEP_END'
[]
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[vslip_x]
type = SideExtremeValue
boundary = 'left'
variable = 'vel_slip_x_var'
[]
[vslip_y]
type = SideExtremeValue
boundary = 'left'
variable = 'vel_slip_y_var'
[]
[vslip_value]
type = ParsedPostprocessor
expression = 'sqrt(vslip_x*vslip_x + vslip_y*vslip_y)*vslip_x/abs(vslip_x)'
pp_names = 'vslip_x vslip_y'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/multiapp-scalar-transport/fluid-flow.i)
mu=1
rho=1
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method='average'
velocity_interp_method='rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = -1
ymax = 1
nx = 100
ny = 20
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[ax_out]
type = MooseVariableFVReal
[]
[ay_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[ax_out]
type = FunctorAux
functor = ax
variable = ax_out
execute_on = timestep_end
[]
[ay_out]
type = FunctorAux
functor = ay
variable = ay_out
execute_on = timestep_end
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = ${rho}
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
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
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
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
function = 0
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0
[]
[]
[MultiApps]
[scalar]
type = FullSolveMultiApp
execute_on = 'timestep_end'
input_files = 'scalar-transport.i'
[]
[]
[Transfers]
[ax]
type = MultiAppCopyTransfer
source_variable = ax_out
variable = ax
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[ay]
type = MultiAppCopyTransfer
source_variable = ay_out
variable = ay
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[u]
type = MultiAppCopyTransfer
source_variable = u
variable = u
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[v]
type = MultiAppCopyTransfer
source_variable = v
variable = v
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[pressure]
type = MultiAppCopyTransfer
source_variable = pressure
variable = pressure
execute_on = 'timestep_end'
to_multi_app = 'scalar'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
nl_rel_tol = 1e-12
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h.i)
L = 30
nx = 600
bulk_u = 0.01
q_source = 50000.
A_cp = 976.78
B_cp = 1.0634
T_in = 860.
p_ref = 101325.0
rho = 2000.
advected_interp_method = 'upwind'
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = ${L}
nx = ${nx}
[]
allow_renumbering = false
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
u = vel_x
[]
[Problem]
linear_sys_names = 'u_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = ${bulk_u}
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${p_ref}
[]
[h]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = ${fparse 860.*1900.}
[]
[]
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[alpha_var]
type = MooseLinearVariableFVReal
[]
[T]
type = MooseLinearVariableFVReal
initial_condition = 860.
[]
[h_aux]
type = MooseLinearVariableFVReal
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu'
momentum_component = 'x'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[temp_advection]
type = LinearFVEnergyAdvection
variable = h
[]
[source]
type = LinearFVSource
variable = h
source_density = source_func
[]
[]
[LinearFVBCs]
[inlet_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u} #${bulk_u} #'fully_developed_velocity'
[]
[inlet_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'left'
functor = 'h_from_p_T'
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'left'
functor = ${T_in}
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = ${p_ref}
[]
[outlet_h]
type = LinearFVAdvectionDiffusionOutflowBC
variable = h
use_two_term_expansion = false
boundary = 'right'
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = 'right'
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = ${q_source}
[]
[T_analytical]
type = ParsedFunction
expression = ${fparse (-A_cp+sqrt(A_cp^2-2*B_cp*(-q_source/rho/bulk_u*L-A_cp*T_in-B_cp/2*T_in*T_in)))/B_cp}
[]
[]
[FunctorMaterials]
[enthalpy_material]
type = LinearFVEnthalpyFunctorMaterial
pressure = ${p_ref}
T_fluid = T
h = h
h_from_p_T_functor = h_from_p_T_functor
T_from_p_h_functor = T_from_p_h_functor
[]
[h_from_p_T_functor]
type = ParsedFunctorMaterial
property_name = 'h_from_p_T_functor'
functor_names = 'T'
expression = '${A_cp}*T+${B_cp}/2*(T^2)'
[]
[T_from_p_h_functor]
type = ParsedFunctorMaterial
property_name = 'T_from_p_h_functor'
functor_names = 'h'
expression = '(-${A_cp}+sqrt(${A_cp}^2+2*h*${B_cp}))/${B_cp}'
[]
[rho]
type = ADParsedFunctorMaterial
property_name = 'rho'
functor_names = 'T'
expression = ${rho}
[]
[cp]
type = ADParsedFunctorMaterial
property_name = 'cp'
functor_names = 'T'
expression = '${A_cp}+${B_cp}*T'
[]
[mu]
type = ADParsedFunctorMaterial
property_name = 'mu'
functor_names = 'T'
expression = '4.5e-3'
[]
[k]
type = ADParsedFunctorMaterial
property_name = 'k'
functor_names = 'T'
expression = 0.7
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[T_from_h_functor_aux]
type = FunctorAux
functor = 'T_from_p_h'
variable = 'T'
execute_on = 'NONLINEAR'
[]
[h_from_T_functor_aux]
type = FunctorAux
functor = 'h_from_p_T'
variable = 'h_aux'
execute_on = 'NONLINEAR'
[]
[]
[Postprocessors]
[T_out_sim]
type = ElementalVariableValue
variable = T
elementid = ${fparse nx-1}
[]
[T_out_analytic]
type = FunctionValuePostprocessor
function = T_analytical
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-12
pressure_l_abs_tol = 1e-12
energy_l_abs_tol = 1e-12
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.95
num_iterations = 100
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 200
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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
[out]
type = CSV
[]
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected-action.i)
mu = 1.1
rho = 1.1
darcy = 1.1
forch = 1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[AuxVariables]
[eps_out]
type = MooseVariableFVReal
[]
[eps_smoothed_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[eps_out]
type = FunctorAux
variable = eps_out
functor = porosity
execute_on = 'timestep_end'
[]
[eps_smoothed_out]
type = FunctorAux
variable = eps_smoothed_out
functor = smoothed_porosity
[]
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'incompressible'
porous_medium_treatment = true
porosity = porosity
porosity_smoothing_layers = 2
friction_types = 'darcy forchheimer'
friction_coeffs = 'Darcy_coefficient Forchheimer_coefficient'
use_friction_correction = true
consistent_scaling = 1.0
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '1 1 0'
initial_pressure = 0.0
inlet_boundaries = 'left top bottom'
momentum_inlet_types = 'fixed-velocity fixed-velocity fixed-velocity'
momentum_inlet_functors = 'exact_u exact_v; exact_u exact_v; exact_u exact_v'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_functors = 'exact_p'
mass_advection_interpolation = 'average'
momentum_advection_interpolation = 'average'
[]
[]
[]
[]
[FVKernels]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_forcing]
type = INSFVBodyForce
variable = superficial_vel_x
functor = forcing_u
momentum_component = 'x'
rhie_chow_user_object = 'pins_rhie_chow_interpolator'
[]
[v_forcing]
type = INSFVBodyForce
variable = superficial_vel_y
functor = forcing_v
momentum_component = 'y'
rhie_chow_user_object = 'pins_rhie_chow_interpolator'
[]
[]
[FunctorMaterials]
[darcy]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '${darcy} ${darcy} ${darcy} ${forch} ${forch} ${forch}'
[]
[constants]
type = ADGenericFunctorMaterial
prop_names = 'rho mu'
prop_values = '${rho} ${mu}'
[]
[]
[Functions]
[porosity]
type = ParsedFunction
expression = '.5 + .1 * sin(pi * x / 4) * cos(pi * y / 4)'
[]
[exact_u]
type = ParsedFunction
expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[forcing_u]
type = ParsedFunction
expression = 'darcy*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) + (1/2)*forch*rho*sqrt(sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2 + sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.1*pi^2*sin((1/4)*x*pi)*sin((1/4)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.025*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.025*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.1*pi^2*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/2)*y*pi)*cos((1/4)*x*pi)^2*cos((1/2)*x*pi)*cos((1/4)*y*pi)^2/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) + 0.025*pi*mu*(0.1*pi*sin((1/4)*x*pi)*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + (1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*(-0.1*pi*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.1*pi*rho*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.1*pi*rho*sin((1/2)*y*pi)^2*cos((1/4)*x*pi)*cos((1/2)*x*pi)^2*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/4*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
symbol_names = 'mu rho darcy forch'
symbol_values = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_v]
type = ParsedFunction
expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_v]
type = ParsedFunction
expression = 'darcy*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) + (1/2)*forch*rho*sqrt(sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2 + sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-0.1*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.025*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.025*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.05*pi^2*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) + 0.025*pi*mu*(0.1*pi*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*(-0.1*pi*sin((1/4)*x*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + (1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.1*pi*rho*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)*cos((1/2)*y*pi)^2/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.1*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (3/2)*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
symbol_names = 'mu rho darcy forch'
symbol_values = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_p]
type = ParsedFunction
expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
symbol_names = 'rho'
symbol_values = '${rho}'
[]
[]
[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
[]
[Outputs]
exodus = false
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2FunctorError
approximate = superficial_vel_x
exact = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2FunctorError
approximate = superficial_vel_y
exact = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
type = ElementL2FunctorError
approximate = pressure
exact = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/lid-driven-two-phase.i)
mu = 1.0
rho = 1.0e3
mu_d = 0.3
rho_d = 1.0
dp = 0.01
U_lid = 0.1
g = -9.81
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 5
ny = 5
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
[]
[vel_y]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = 'rho_mixture'
[]
[mean_zero_pressure]
type = FVPointValueConstraint
variable = pressure
lambda = lambda
point = '0 0 0'
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_buoyant]
type = INSFVMomentumGravity
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
gravity = '0 ${g} 0'
[]
# NOTE: the friction terms for u and v are missing
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_buoyant]
type = INSFVMomentumGravity
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
gravity = '0 ${g} 0'
[]
[phase_2_time]
type = FVFunctorTimeKernel
variable = phase_2
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
[]
[phase_2_diffusion]
type = FVDiffusion
variable = phase_2
coeff = 1e-3
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${U_lid}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[bottom_phase_2]
type = FVDirichletBC
variable = phase_2
boundary = 'bottom'
value = 1.0
[]
[top_phase_2]
type = FVDirichletBC
variable = phase_2
boundary = 'top'
value = 0.0
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FunctorMaterials]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
gravity = '0 ${g} 0'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
gravity = '0 ${g} 0'
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_1_names = '${rho_d} ${mu_d}'
phase_2_names = '${rho} ${mu}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient]
type = ElementExtremeFunctorValue
functor = 'drag_coefficient'
value_type = max
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 7
iteration_window = 2
growth_factor = 2.0
cutback_factor = 0.5
dt = 1e-3
[]
nl_max_its = 20
nl_rel_tol = 1e-03
nl_abs_tol = 1e-9
l_max_its = 5
end_time = 1e8
line_search=none
[]
[Outputs]
exodus = false
[CSV]
type = CSV
execute_on = 'FINAL'
execute_scalars_on = NONE
[]
[]
(modules/heat_transfer/test/tests/functormaterials/cylindrical_gap_heat_flux_functor_material/cylindrical_gap_heat_flux_functor_material.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 10
ny = 10
nz = 10
[]
[AuxVariables]
[q_cond]
family = MONOMIAL
order = CONSTANT
[]
[q_rad]
family = MONOMIAL
order = CONSTANT
[]
[q_total]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[q_cond_kern]
type = FunctorAux
variable = q_cond
functor = conduction_heat_flux
execute_on = 'INITIAL'
[]
[q_rad_kern]
type = FunctorAux
variable = q_rad
functor = radiation_heat_flux
execute_on = 'INITIAL'
[]
[q_total_kern]
type = FunctorAux
variable = q_total
functor = total_heat_flux
execute_on = 'INITIAL'
[]
[]
[Functions]
[r_outer_fn]
type = ParsedFunction
# vary gap distance from 1 um to 1 mm in (0,1)
expression = '1.0 + 10^(-6 + 3*z)'
[]
[T_inner_fn]
type = ParsedFunction
expression = '300 + 1000 * x'
[]
[T_outer_fn]
type = ParsedFunction
expression = '300 + 1000 * y'
[]
[]
[Materials]
[heat_flux_fmat]
type = CylindricalGapHeatFluxFunctorMaterial
r_inner = 1.0
r_outer = r_outer_fn
emissivity_inner = 0.25
emissivity_outer = 0.75
k_gap = 0.15
T_inner = T_inner_fn
T_outer = T_outer_fn
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d-parsed-function.i)
rho = 1.1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 1
dx = '1 1'
ix = '3 3'
subdomain_id = '1 2'
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = BernoulliPressureVariable
u = u
porosity = porosity
rho = ${rho}
[]
[]
[Functions]
[porosity]
type = ParsedFunction
expression = 'if(x > 1, 0.5, 1)'
[]
[]
[AuxVariables]
[has_porosity_jump_face]
type = MooseVariableFVReal
[]
[porosity_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[has_porosity_jump_face]
type = HasPorosityJumpFace
porosity = porosity
execute_on = 'initial timestep_end'
variable = has_porosity_jump_face
[]
[porosity_out]
type = FunctorAux
variable = porosity_out
functor = porosity
execute_on = 'initial timestep_end'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
function = '1'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 1
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
[]
[Postprocessors]
[inlet_p]
type = SideAverageValue
variable = 'pressure'
boundary = 'left'
[]
[outlet-u]
type = SideIntegralVariablePostprocessor
variable = u
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc.i)
mu = 0.01
rho = 2000
u_inlet = 1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 1
nx = 10
ny = 6
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[Variables]
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${u_inlet}
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1e-6
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[porosity]
family = MONOMIAL
order = CONSTANT
fv = true
initial_condition = 0.5
[]
[speed_output]
type = MooseVariableFVReal
[]
[vel_x_output]
type = MooseVariableFVReal
[]
[vel_y_output]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[speed]
type = FunctorAux
variable = 'speed_output'
functor = 'speed'
[]
[vel_x]
type = ADFunctorVectorElementalAux
variable = 'vel_x_output'
functor = 'velocity'
component = 0
[]
[vel_y]
type = ADFunctorVectorElementalAux
variable = 'vel_y_output'
functor = 'velocity'
component = 1
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_x
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_x
momentum_component = 'x'
pressure = pressure
porosity = porosity
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = superficial_vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
porosity = porosity
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = superficial_vel_y
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = superficial_vel_y
momentum_component = 'y'
pressure = pressure
porosity = porosity
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_x
function = ${u_inlet}
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = superficial_vel_y
function = 0
[]
[no-slip-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_x
function = 0
[]
[no-slip-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = superficial_vel_y
function = 0
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = ${mu}
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[outlet-p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 0.1
[]
[]
[FunctorMaterials]
# Testing this object
[var_mat]
type = PINSFVSpeedFunctorMaterial
superficial_vel_x = 'superficial_vel_x'
superficial_vel_y = 'superficial_vel_y'
porosity = porosity
[]
[]
[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
nl_abs_tol = 1e-11
[]
# Some basic Postprocessors to examine the solution
[Postprocessors]
[inlet-p]
type = SideAverageValue
variable = pressure
boundary = 'left'
[]
[outlet-u]
type = SideAverageValue
variable = superficial_vel_x
boundary = 'right'
[]
[]
[Outputs]
exodus = true
csv = false
[]
(test/tests/materials/functor_properties/vector-magnitude/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[u]
type = MooseVariableFVReal
[]
[v]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[mag]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = FunctorAux
variable = mag
functor = mat_mag
[]
[]
[FVKernels]
[v_diff]
type = FVDiffusion
variable = v
coeff = 1
[]
[u_diff]
type = FVDiffusion
variable = u
coeff = 1
[]
[]
[FVBCs]
[v_left]
type = FVDirichletBC
variable = v
boundary = 'left'
value = 0
[]
[v_right]
type = FVDirichletBC
variable = v
boundary = 'right'
value = 1
[]
[u_bottom]
type = FVDirichletBC
variable = u
boundary = 'bottom'
value = 0
[]
[u_top]
type = FVDirichletBC
variable = u
boundary = 'top'
value = 1
[]
[]
[Materials]
[functor]
type = ADVectorMagnitudeFunctorMaterial
x_functor = u
y_functor = v
vector_magnitude_name = mat_mag
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-advection-slip.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
mu_interp_method = 'average'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 5}'
ymin = '${fparse -l / 2}'
ymax = '${fparse l / 2}'
nx = 10
ny = 6
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_advection_slip]
type = WCNSFV2PMomentumAdvectionSlip
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
rho_d = ${rho_d}
fd = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_friction]
type = PINSFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
is_porous_medium = false
momentum_component = x
mu = mu_mixture
rho = rho_mixture
variable = vel_x
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_advection_slip]
type = WCNSFV2PMomentumAdvectionSlip
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
rho_d = ${rho_d}
fd = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_friction]
type = PINSFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
is_porous_medium = false
momentum_component = y
mu = mu_mixture
rho = rho_mixture
variable = vel_y
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = 0.1
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FunctorMaterials]
[phase_1]
property_name = 'phase_1'
type = ADParsedFunctorMaterial
functor_names = 'phase_2'
expression = '1 - phase_2'
outputs = 'out'
output_properties = 'phase_1'
[]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
outputs = 'out'
output_properties = 'vel_slip_x'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
outputs = 'out'
output_properties = 'vel_slip_y'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = '${rho_d} ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
[out]
type = Exodus
hide = 'Re lin cum_lin'
[]
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
[]
[lin]
type = NumLinearIterations
[]
[cum_lin]
type = CumulativeValuePostprocessor
postprocessor = lin
[]
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/pressure_driven_growth_transient.i)
###############################################################################
# Validation test based on Hibiki and Ishii experiment [1] reported in Figure 3
# [1] Hibiki, T., & Ishii, M. (2000). One-group interfacial area transport of bubbly flows in vertical round tubes.
# International Journal of Heat and Mass Transfer, 43(15), 2711-2726.
###############################################################################
mu = 1.0
rho = 1000.0
mu_d = 1.0
rho_d = 1.0
l = ${fparse 50.8/1000.0}
U = 0.491230114
dp = 0.001
inlet_phase_2 = 0.049
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
mass_exchange_coeff = 0.0
inlet_interface_area = ${fparse 6.0*inlet_phase_2/dp}
outlet_pressure = 1e6
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[Problem]
identify_variable_groups_in_nl = false
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
coord_type = 'RZ'
rz_coord_axis = 'X'
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 60}'
ymin = 0
ymax = '${fparse l / 2}'
nx = 20
ny = 5
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
initial_condition = ${inlet_phase_2}
[]
[interface_area]
type = INSFVScalarFieldVariable
initial_condition = ${inlet_interface_area}
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_x
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_y
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[phase_2_time]
type = FVFunctorTimeKernel
variable = phase_2
functor = phase_2
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_x'
v_slip = 'vel_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_diffusion]
type = FVDiffusion
variable = phase_2
coeff = 1.0
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = ${mass_exchange_coeff}
[]
[interface_area_time]
type = FVFunctorTimeKernel
variable = interface_area
functor = interface_area
[]
[interface_area_advection]
type = INSFVScalarFieldAdvection
variable = interface_area
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[interface_area_diffusion]
type = FVDiffusion
variable = interface_area
coeff = 0.1
[]
[interface_area_source_sink]
type = WCNSFV2PInterfaceAreaSourceSink
variable = interface_area
u = 'vel_x'
v = 'vel_y'
L = ${fparse l/2}
rho = 'rho_mixture'
rho_d = 'rho'
pressure = 'pressure'
k_c = '${fparse mass_exchange_coeff}'
fd = 'phase_2'
sigma = 1e-3
cutoff_fraction = 0.0
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '${outlet_pressure}'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[inlet_interface_area]
type = FVDirichletBC
boundary = 'left'
variable = interface_area
value = ${inlet_interface_area}
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_x
u = vel_x
v = vel_y
mu = 'mu_mixture'
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_y
u = vel_x
v = vel_y
mu = 'mu_mixture'
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[symmetry-phase-2]
type = INSFVSymmetryScalarBC
boundary = 'bottom'
variable = phase_2
[]
[symmetry-interface-area]
type = INSFVSymmetryScalarBC
boundary = 'bottom'
variable = interface_area
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[FunctorMaterials]
[bubble_properties]
type = GeneralFunctorFluidProps
fp = 'fp'
pressure = 'pressure'
T_fluid = 300.0
speed = 1.0
characteristic_length = 1.0
porosity = 1.0
output_properties = 'rho'
outputs = 'out'
[]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = 'rho ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
nl_abs_tol = 1e-7
dt = 0.1
end_time = 1.0
nl_max_its = 10
line_search = 'none'
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
[out]
type = Exodus
[]
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/solidification/solidification_no_advection.i)
rho_solid = 1.0
rho_liquid = 1.0
k_solid = 0.03
k_liquid = 0.1
cp_solid = 1.0
cp_liquid = 1.0
T_liquidus = 260
T_solidus = 240
L = 1.0
T_hot = 300.0
T_cold = 200.0
N = 10
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
nx = ${N}
ny = ${N}
[]
[]
[AuxVariables]
[fl]
type = MooseVariableFVReal
initial_condition = 1.0
[]
[density]
type = MooseVariableFVReal
[]
[th_cond]
type = MooseVariableFVReal
[]
[cp_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[compute_fl]
type = NSLiquidFractionAux
variable = fl
temperature = T
T_liquidus = '${T_liquidus}'
T_solidus = '${T_solidus}'
execute_on = 'TIMESTEP_END'
[]
[rho_out]
type = FunctorAux
functor = 'rho_mixture'
variable = 'density'
[]
[th_cond_out]
type = FunctorAux
functor = 'k_mixture'
variable = 'th_cond'
[]
[cp_out]
type = FunctorAux
functor = 'cp_mixture'
variable = 'cp_var'
[]
[]
[Variables]
[T]
type = INSFVEnergyVariable
initial_condition = '${T_hot}'
[]
[]
[FVKernels]
[T_time]
type = INSFVEnergyTimeDerivative
variable = T
rho = ${rho_liquid}
[]
[energy_diffusion]
type = FVDiffusion
coeff = 'k_mixture'
variable = T
[]
[energy_source]
type = NSFVPhaseChangeSource
variable = T
L = ${L}
liquid_fraction = fl
T_liquidus = ${T_liquidus}
T_solidus = ${T_solidus}
rho = 'rho_mixture'
[]
[]
[FVBCs]
[heated_wall]
type = FVDirichletBC
variable = T
value = '${T_hot}'
boundary = 'top'
[]
[cooled_wall]
type = FVDirichletBC
variable = T
value = '${T_cold}'
boundary = 'bottom'
[]
[]
[FunctorMaterials]
[eff_cp]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${cp_solid} ${k_solid} ${rho_solid}'
phase_1_names = '${cp_liquid} ${k_liquid} ${rho_liquid}'
prop_names = 'cp_mixture k_mixture rho_mixture'
phase_1_fraction = fl
[]
[h]
type = INSFVEnthalpyFunctorMaterial
cp = ${cp_liquid}
temperature = T
rho = ${rho_liquid}
[]
[]
[Executioner]
type = Transient
dt = 0.5
end_time = 50.0
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_abs_tol = 1e-12
nl_max_its = 50
steady_state_detection = true
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation.i)
H = 0.015 #halfwidth of the channel, 10 cm of channel height
L = 1
bulk_u = 0.01
p_ref = 101325.0
advected_interp_method = 'upwind'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = -${H}
ymax = ${H}
nx = 30
ny = 15
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = ${bulk_u}
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${p_ref}
[]
[h]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 44000 # 1900 is an approx of cp(T)
[]
[]
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[T]
type = MooseLinearVariableFVReal
initial_condition = 777.
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu'
momentum_component = 'x'
use_nonorthogonal_correction = false
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
u = vel_x
v = vel_y
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
mu = 'mu'
momentum_component = 'y'
use_nonorthogonal_correction = false
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
u = vel_x
v = vel_y
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[temp_conduction]
type = LinearFVDiffusion
diffusion_coeff = 'alpha'
variable = h
[]
[temp_advection]
type = LinearFVEnergyAdvection
variable = h
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[]
[LinearFVBCs]
[inlet_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u} #${bulk_u} #'fully_developed_velocity'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = 0
[]
[inlet_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'left'
functor = h_from_p_T # ${fparse 1900.*860.}
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'left'
functor = 860.
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = 'top bottom'
functor = 0.
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = 'top bottom'
functor = 0.
[]
[walls_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'top bottom'
functor = h_from_p_T # ${fparse 1900. * 950}
[]
[walls_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'top bottom'
functor = 950.
[]
[walls_p]
type = LinearFVExtrapolatedPressureBC
boundary = 'top bottom'
variable = pressure
use_two_term_expansion = false
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = ${p_ref}
[]
[outlet_h]
type = LinearFVAdvectionDiffusionOutflowBC
variable = h
use_two_term_expansion = false
boundary = 'right'
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = right
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_y
use_two_term_expansion = false
boundary = right
[]
[]
[FluidProperties]
[lead]
type = LeadFluidProperties
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = lead
pressure = ${p_ref}
T_fluid = 'T'
speed = 1
porosity = 1
characteristic_length = 1
[]
[alpha]
type = ADParsedFunctorMaterial
property_name = 'alpha'
functor_names = 'k cp'
expression = 'k/cp'
[]
[enthalpy_material]
type = LinearFVEnthalpyFunctorMaterial
pressure = ${p_ref}
T_fluid = T
h = h
fp = lead
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[T_from_h_functor]
type = FunctorAux
functor = 'T_from_p_h'
variable = 'T'
execute_on = 'NONLINEAR'
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-6
pressure_l_abs_tol = 1e-6
energy_l_abs_tol = 1e-8
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.9
num_iterations = 200
pressure_absolute_tolerance = 1e-6
momentum_absolute_tolerance = 1e-6
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 1000
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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = 'TIMESTEP_BEGIN FINAL'
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/pressure_driven_growth.i)
###############################################################################
# Validation test based on Hibiki and Ishii experiment [1] reported in Figure 3
# [1] Hibiki, T., & Ishii, M. (2000). One-group interfacial area transport of bubbly flows in vertical round tubes.
# International Journal of Heat and Mass Transfer, 43(15), 2711-2726.
###############################################################################
mu = 1.0
rho = 1000.0
mu_d = 1.0
rho_d = 1.0
l = ${fparse 50.8/1000.0}
U = 0.491230114
dp = 0.001
inlet_phase_2 = 0.049
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
mass_exchange_coeff = 0.0
inlet_interface_area = ${fparse 6.0*inlet_phase_2/dp}
outlet_pressure = 1e5
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[Problem]
identify_variable_groups_in_nl = false
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
coord_type = 'RZ'
rz_coord_axis = 'X'
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 60}'
ymin = 0
ymax = '${fparse l / 2}'
nx = 20
ny = 5
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
initial_condition = ${inlet_phase_2}
[]
[interface_area]
type = INSFVScalarFieldVariable
initial_condition = ${inlet_interface_area}
[]
[]
[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 = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_x
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_y
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_x'
v_slip = 'vel_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_diffusion]
type = FVDiffusion
variable = phase_2
coeff = 1.0
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = ${mass_exchange_coeff}
[]
[interface_area_advection]
type = INSFVScalarFieldAdvection
variable = interface_area
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[interface_area_diffusion]
type = FVDiffusion
variable = interface_area
coeff = 0.1
[]
[interface_area_source_sink]
type = WCNSFV2PInterfaceAreaSourceSink
variable = interface_area
u = 'vel_x'
v = 'vel_y'
L = ${fparse l/2}
rho = 'rho_mixture'
rho_d = 'rho'
pressure = 'pressure'
k_c = '${fparse mass_exchange_coeff}'
fd = 'phase_2'
sigma = 1e-3
cutoff_fraction = 0.0
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '${outlet_pressure}'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[inlet_interface_area]
type = FVDirichletBC
boundary = 'left'
variable = interface_area
value = ${inlet_interface_area}
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_x
u = vel_x
v = vel_y
mu = 'mu_mixture'
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_y
u = vel_x
v = vel_y
mu = 'mu_mixture'
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[symmetry-phase-2]
type = INSFVSymmetryScalarBC
boundary = 'bottom'
variable = phase_2
[]
[symmetry-interface-area]
type = INSFVSymmetryScalarBC
boundary = 'bottom'
variable = interface_area
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[FunctorMaterials]
[bubble_properties]
type = GeneralFunctorFluidProps
fp = 'fp'
pressure = 'pressure'
T_fluid = 300.0
speed = 1.0
characteristic_length = 1.0
porosity = 1.0
output_properties = 'rho'
outputs = 'out'
[]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = 'rho ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
line_search = 'none'
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
[out]
type = Exodus
[]
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/boussinesq/wcnsfv.i)
mu = 1
rho = 'rho'
k = 1
cp = 1
alpha = 1
velocity_interp_method = 'rc'
advected_interp_method = 'average'
# rayleigh=1e3
cold_temp=300
hot_temp=310
[GlobalParams]
two_term_boundary_expansion = true
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 10
ymin = 0
ymax = 10
nx = 64
ny = 64
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[v]
type = INSFVVelocityVariable
initial_condition = 1e-15
[]
[pressure]
type = INSFVPressureVariable
initial_condition = 1e5
[]
[T]
type = INSFVEnergyVariable
scaling = 1e-4
initial_condition = ${cold_temp}
[]
[lambda]
family = SCALAR
order = FIRST
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[vel_x]
order = FIRST
family = MONOMIAL
[]
[vel_y]
order = FIRST
family = MONOMIAL
[]
[viz_T]
order = FIRST
family = MONOMIAL
[]
[rho_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = u
y = v
execute_on = 'initial timestep_end'
[]
[vel_x]
type = ParsedAux
variable = vel_x
expression = 'u'
execute_on = 'initial timestep_end'
coupled_variables = 'u'
[]
[vel_y]
type = ParsedAux
variable = vel_y
expression = 'v'
execute_on = 'initial timestep_end'
coupled_variables = 'v'
[]
[viz_T]
type = ParsedAux
variable = viz_T
expression = 'T'
execute_on = 'initial timestep_end'
coupled_variables = 'T'
[]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_out'
execute_on = 'initial timestep_end'
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mean_zero_pressure]
type = FVIntegralValueConstraint
variable = pressure
lambda = lambda
phi0 = 1e5
[]
[u_advection]
type = INSFVMomentumAdvection
variable = u
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_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
[]
[u_gravity]
type = INSFVMomentumGravity
variable = u
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'x'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = v
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_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
[]
[v_gravity]
type = INSFVMomentumGravity
variable = v
gravity = '0 -1 0'
rho = ${rho}
momentum_component = 'y'
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[]
[FVBCs]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'left right top bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'left right top bottom'
function = 0
[]
[T_hot]
type = FVDirichletBC
variable = T
boundary = left
value = ${hot_temp}
[]
[T_cold]
type = FVDirichletBC
variable = T
boundary = right
value = ${cold_temp}
[]
[]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[Materials]
[const]
type = ADGenericConstantMaterial
prop_names = 'alpha'
prop_values = '${alpha}'
[]
[]
[FunctorMaterials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[rho]
type = RhoFromPTFunctorMaterial
fp = fp
temperature = T
pressure = pressure
[]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T'
rho = ${rho}
[]
[]
[Functions]
[lid_function]
type = ParsedFunction
expression = '4*x*(1-x)'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/fvbcs/FVFunctorHeatFluxBC/wall_heat_transfer.i)
flux=10
[GlobalParams]
porosity = 'porosity'
splitting = 'porosity'
locality = 'global'
average_porosity = 'average_eps'
average_k_fluid='average_k_fluid'
average_k_solid='average_k_solid'
average_kappa='average_k_fluid' # because of vector matprop, should be kappa
average_kappa_solid='average_kappa_solid'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 20
xmin = 0.0
xmax = 1.0
ymin = 0.0
ymax = 1.0
[]
[Variables]
[Tf]
type = MooseVariableFVReal
[]
[Ts]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[k]
type = MooseVariableFVReal
[]
[kappa]
type = MooseVariableFVReal
[]
[k_s]
type = MooseVariableFVReal
[]
[kappa_s]
type = MooseVariableFVReal
[]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.2
[]
[]
[Functions]
[k_function]
type = ParsedFunction
expression = 0.1*(100*y+1)
[]
[kappa_function]
type = ParsedFunction
expression = 0.2*(200*y+1)
[]
[kappa_s_function]
type = ParsedFunction
expression = 0.4*(200*y+1)
[]
[k_s_function]
type = ParsedFunction
expression = 0.2*(200*y+1)+2*x
[]
[]
[FVKernels]
[Tf_diffusion]
type = FVDiffusion
variable = Tf
coeff = 1
[]
[Ts_diffusion]
type = FVDiffusion
variable = Ts
coeff = 1
[]
[]
[FVBCs]
[left_Ts]
type = NSFVFunctorHeatFluxBC
variable = Ts
boundary = 'left'
phase = 'solid'
value = ${flux}
k = 'k_mat'
k_s = 'k_s_mat'
kappa = 'kappa_mat'
kappa_s = 'kappa_s_mat'
[]
[right_Ts]
type = FVDirichletBC
variable = Ts
boundary = 'right'
value = 1000.0
[]
[left_Tf]
type = NSFVFunctorHeatFluxBC
variable = Tf
boundary = 'left'
phase = 'fluid'
value = ${flux}
k = 'k_mat'
k_s = 'k_s_mat'
kappa = 'kappa_mat'
kappa_s = 'kappa_s_mat'
[]
[right_Tf]
type = FVDirichletBC
variable = Tf
boundary = 'right'
value = 1000.0
[]
[]
[AuxKernels]
[k]
type = FunctorAux
variable = k
functor = 'k_mat'
[]
[k_s]
type = FunctorAux
variable = k_s
functor = 'k_s_mat'
[]
[kappa_s]
type = FunctorAux
variable = kappa_s
functor = 'kappa_s_mat'
[]
[]
[FunctorMaterials]
[thermal_conductivities_k]
type = ADGenericFunctorMaterial
prop_names = 'k_mat'
prop_values = 'k_function'
[]
[thermal_conductivities_k_s]
type = ADGenericFunctorMaterial
prop_names = 'k_s_mat'
prop_values = 'k_s_function'
[]
[thermal_conductivities_kappa]
type = ADGenericVectorFunctorMaterial
prop_names = 'kappa_mat'
prop_values = '0.1 0.2 .03'
[]
[thermal_conductivities_kappa_s]
type = ADGenericFunctorMaterial
prop_names = 'kappa_s_mat'
prop_values = 'kappa_s_function'
[]
[]
[Postprocessors]
[average_eps]
type = ElementAverageValue
variable = porosity
# because porosity is constant in time, we evaluate this only once
execute_on = 'initial'
[]
[average_k_fluid]
type = ElementAverageValue
variable = k
[]
[average_k_solid]
type = ElementAverageValue
variable = k_s
[]
[average_kappa_solid]
type = ElementAverageValue
variable = kappa_s
[]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
hide = 'porosity average_eps'
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/turbulent_driven_growth.i)
###############################################################################
# Validation test based on Hibiki and Ishii experiment [1] reported in Figure 5
# [1] Hibiki, T., & Ishii, M. (2000). One-group interfacial area transport of
# bubbly flows in vertical round tubes.
# International Journal of Heat and Mass Transfer, 43(15), 2711-2726.
###############################################################################
mu = 1.0
rho = 1000.0
mu_d = 1.0
rho_d = 1.0
l = ${fparse 50.8/1000.0}
U = 5.031429
dp = 0.005
inlet_phase_2 = 0.442
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
mass_exchange_coeff = 0.0
inlet_interface_area = ${fparse 6.0*inlet_phase_2/dp}
outlet_pressure = 1e5
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[Problem]
identify_variable_groups_in_nl = false
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
coord_type = 'RZ'
rz_coord_axis = 'X'
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 60}'
ymin = 0
ymax = '${fparse l / 2}'
nx = 20
ny = 5
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
initial_condition = ${inlet_phase_2}
[]
[interface_area]
type = INSFVScalarFieldVariable
initial_condition = ${inlet_interface_area}
[]
[]
[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 = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_x
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_y
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_x'
v_slip = 'vel_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_diffusion]
type = FVDiffusion
variable = phase_2
coeff = 1.0
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = ${mass_exchange_coeff}
[]
[interface_area_advection]
type = INSFVScalarFieldAdvection
variable = interface_area
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[interface_area_diffusion]
type = FVDiffusion
variable = interface_area
coeff = 0.1
[]
[interface_area_source_sink]
type = WCNSFV2PInterfaceAreaSourceSink
variable = interface_area
u = 'vel_x'
v = 'vel_y'
L = ${fparse l/2}
rho = 'rho_mixture'
rho_d = 'rho'
pressure = 'pressure'
k_c = '${fparse mass_exchange_coeff}'
fd = 'phase_2'
sigma = 1e-3
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '${outlet_pressure}'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[inlet_interface_area]
type = FVDirichletBC
boundary = 'left'
variable = interface_area
value = ${inlet_interface_area}
[]
[symmetry-u]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_x
u = vel_x
v = vel_y
mu = 'mu_mixture'
momentum_component = 'x'
[]
[symmetry-v]
type = PINSFVSymmetryVelocityBC
boundary = 'bottom'
variable = vel_y
u = vel_x
v = vel_y
mu = 'mu_mixture'
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'bottom'
variable = pressure
[]
[symmetry-phase-2]
type = INSFVSymmetryScalarBC
boundary = 'bottom'
variable = phase_2
[]
[symmetry-interface-area]
type = INSFVSymmetryScalarBC
boundary = 'bottom'
variable = interface_area
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
[]
[]
[FunctorMaterials]
[bubble_properties]
type = GeneralFunctorFluidProps
fp = 'fp'
pressure = 'pressure'
T_fluid = 300.0
speed = 1.0
characteristic_length = 1.0
porosity = 1.0
output_properties = 'rho'
outputs = 'out'
[]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = 'rho ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
line_search = 'none'
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
[out]
type = Exodus
[]
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(modules/combined/test/tests/subchannel_thm_coupling/subchannel.i)
# Based on M. Fontana, et al. this arbitrary subassembly is used for THM-SC coupling
T_in = 583.0 #K
flow_area = 0.0004980799633447909 #m2
mass_flux_in = '${fparse 1.0/flow_area}'
P_out = 2e5 # Pa
###################################################
# Geometric parameters
###################################################
n_cells = 25
n_rings = 3
fuel_pin_pitch = 7.26e-3
fuel_pin_diameter = 5.84e-3
wire_z_spacing = 0.3048
wire_diameter = 1.42e-3
inner_duct_in = 3.41e-2
heated_length = 1.0
###################################################
[TriSubChannelMesh]
[subchannel]
type = SCMTriSubChannelMeshGenerator
nrings = ${n_rings}
n_cells = ${n_cells}
flat_to_flat = ${inner_duct_in}
heated_length = ${heated_length}
pin_diameter = ${fuel_pin_diameter}
pitch = ${fuel_pin_pitch}
dwire = ${wire_diameter}
hwire = ${wire_z_spacing}
spacer_z = '0.0'
spacer_k = '0.0'
[]
[fuel_pins]
type = SCMTriPinMeshGenerator
input = subchannel
nrings = ${n_rings}
n_cells = ${n_cells}
heated_length = ${heated_length}
pitch = ${fuel_pin_pitch}
[]
[]
[AuxVariables]
[mdot]
block = subchannel
[]
[SumWij]
block = subchannel
[]
[P]
block = subchannel
[]
[DP]
block = subchannel
[]
[h]
block = subchannel
[]
[T]
block = subchannel
[]
[rho]
block = subchannel
[]
[S]
block = subchannel
[]
[w_perim]
block = subchannel
[]
[mu]
block = subchannel
[]
[displacement]
block = subchannel
[]
[q_prime]
block = fuel_pins
[]
[Tpin]
block = fuel_pins
[]
[Dpin]
block = fuel_pins
[]
[]
[FluidProperties]
[Sodium]
type = PBSodiumFluidProperties
[]
[]
[Problem]
type = TriSubChannel1PhaseProblem
fp = Sodium
n_blocks = 1
P_out = report_pressure_outlet
CT = 2.6
compute_density = true
compute_viscosity = true
compute_power = true
P_tol = 1.0e-3
T_tol = 1.0e-3
implicit = true
segregated = false
staggered_pressure = false
monolithic_thermal = false
verbose_multiapps = true
verbose_subchannel = false
interpolation_scheme = 'upwind'
[]
[ICs]
[S_IC]
type = SCMTriFlowAreaIC
variable = S
[]
[w_perim_IC]
type = SCMTriWettedPerimIC
variable = w_perim
[]
[q_prime_IC]
type = SCMTriPowerIC
variable = q_prime
power = 10000 #W
filename = "pin_power_profile19.txt"
[]
[T_ic]
type = ConstantIC
variable = T
value = ${T_in}
[]
[Dpin_ic]
type = ConstantIC
variable = Dpin
value = ${fuel_pin_diameter}
[]
[P_ic]
type = ConstantIC
variable = P
value = 0.0
[]
[DP_ic]
type = ConstantIC
variable = DP
value = 0.0
[]
[Viscosity_ic]
type = ViscosityIC
variable = mu
p = ${P_out}
T = T
fp = Sodium
[]
[rho_ic]
type = RhoFromPressureTemperatureIC
variable = rho
p = ${P_out}
T = T
fp = Sodium
[]
[h_ic]
type = SpecificEnthalpyFromPressureTemperatureIC
variable = h
p = ${P_out}
T = T
fp = Sodium
[]
[mdot_ic]
type = ConstantIC
variable = mdot
value = 0.0
[]
[]
[AuxKernels]
[T_in_bc]
type = FunctorAux
functor = report_temperature_inlet
variable = T
boundary = inlet
execute_on = 'timestep_begin'
block = subchannel
[]
[mdot_in_bc]
type = SCMMassFlowRateAux
variable = mdot
boundary = inlet
area = S
mass_flux = report_mass_flux_inlet
execute_on = 'timestep_begin'
block = subchannel
[]
[]
[Outputs]
csv = true
[]
[Executioner]
type = Steady
[]
[Postprocessors]
[total_pressure_drop_SC]
type = SubChannelDelta
variable = P
execute_on = "timestep_end"
[]
[total_pressure_drop_SC_limited]
type = ParsedPostprocessor
pp_names = 'total_pressure_drop_SC'
function = 'min(total_pressure_drop_SC, 1e6)'
execute_on = "timestep_end"
[]
[Total_power]
type = ElementIntegralVariablePostprocessor
variable = q_prime
block = fuel_pins
[]
[report_mass_flux_inlet]
type = Receiver
default = ${mass_flux_in}
[]
[report_temperature_inlet]
type = Receiver
default = ${T_in}
force_preaux = true
[]
[report_pressure_outlet]
type = Receiver
default = ${P_out}
[]
[]
################################################################################
# A multiapp that projects data to a detailed mesh
################################################################################
[MultiApps]
[viz]
type = FullSolveMultiApp
input_files = '3D.i'
execute_on = 'FINAL'
[]
[]
[Transfers]
[subchannel_transfer]
type = SCMSolutionTransfer
to_multi_app = viz
variable = 'mdot SumWij P DP h T rho mu S'
[]
[pin_transfer]
type = SCMPinSolutionTransfer
to_multi_app = viz
variable = 'Dpin Tpin q_prime'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation-physics.i)
H = 0.015
L = 1
bulk_u = 0.01
p_ref = 101325.0
advected_interp_method = 'upwind'
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = -${H}
ymax = ${H}
nx = 30
ny = 15
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
[]
[Physics]
[NavierStokes]
[FlowSegregated]
[flow]
compressibility = 'weakly-compressible'
velocity_variable = 'vel_x vel_y'
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '${bulk_u} 0 0'
initial_pressure = '${p_ref}'
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_functors = '${bulk_u} 0'
wall_boundaries = 'top bottom'
momentum_wall_types = 'noslip noslip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_functors = '${p_ref}'
orthogonality_correction = false
momentum_advection_interpolation = ${advected_interp_method}
pressure_two_term_bc_expansion = false
momentum_two_term_bc_expansion = false
[]
[]
[FluidHeatTransferSegregated]
[energy]
coupled_flow_physics = flow
solve_for_enthalpy = true
fluid_temperature_variable = 'T'
fp = 'lead'
thermal_conductivity = 'k'
specific_heat = 'cp'
initial_temperature = '777'
initial_enthalpy = '44000'
energy_inlet_types = 'fixed-temperature'
energy_inlet_functors = '860'
energy_wall_types = 'fixed-temperature fixed-temperature'
energy_wall_functors = '950 950'
energy_advection_interpolation = ${advected_interp_method}
energy_two_term_bc_expansion = false
use_nonorthogonal_correction = false
[]
[]
[]
[]
[FluidProperties]
[lead]
type = LeadFluidProperties
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = lead
pressure = ${p_ref}
T_fluid = 'T'
speed = 1
porosity = 1
characteristic_length = 1
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-6
pressure_l_abs_tol = 1e-6
energy_l_abs_tol = 1e-8
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.9
num_iterations = 200
pressure_absolute_tolerance = 1e-6
momentum_absolute_tolerance = 1e-6
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 1000
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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = 'TIMESTEP_BEGIN FINAL'
[]
# To match the gold file
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp.i)
L = 30
nx = 600
bulk_u = 0.01
p_ref = 101325.0
T_in = 860.
q_source = 20000.
advected_interp_method = 'upwind'
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = ${L}
nx = ${nx}
[]
allow_renumbering = false
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
u = vel_x
[]
[Problem]
linear_sys_names = 'u_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = RhieChowMassFlux
u = vel_x
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = ${bulk_u}
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${p_ref}
[]
[h]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = ${fparse 860.*240.}
[]
[]
[AuxVariables]
[rho_var]
type = MooseLinearVariableFVReal
[]
[cp_var]
type = MooseLinearVariableFVReal
[]
[mu_var]
type = MooseLinearVariableFVReal
[]
[k_var]
type = MooseLinearVariableFVReal
[]
[alpha_var]
type = MooseLinearVariableFVReal
[]
[T]
type = MooseLinearVariableFVReal
initial_condition = ${T_in}
[]
[h_aux]
type = MooseLinearVariableFVReal
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
mu = 'mu'
momentum_component = 'x'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[temp_advection]
type = LinearFVEnergyAdvection
variable = h
[]
[source]
type = LinearFVSource
variable = h
source_density = source_func
[]
[]
[LinearFVBCs]
[inlet_u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u}
[]
[inlet_h]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = h
boundary = 'left'
functor = 'h_from_p_T'
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T
boundary = 'left'
functor = ${T_in}
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = ${p_ref}
[]
[outlet_h]
type = LinearFVAdvectionDiffusionOutflowBC
variable = h
use_two_term_expansion = false
boundary = 'right'
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
variable = vel_x
use_two_term_expansion = false
boundary = 'right'
[]
[]
[FluidProperties]
[lead]
type = LeadFluidProperties
[]
[]
[FunctorMaterials]
[enthalpy_material]
type = LinearFVEnthalpyFunctorMaterial
pressure = ${p_ref}
T_fluid = T
h = h
fp = lead
[]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = lead
pressure = ${p_ref}
T_fluid = 'T'
speed = 1
porosity = 1
characteristic_length = 1
[]
[source_func]
type = ADParsedFunctorMaterial
property_name = source_func
functor_names = 'rho'
expression = ${q_source}
[]
[]
[AuxKernels]
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'NONLINEAR'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'NONLINEAR'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'NONLINEAR'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'NONLINEAR'
[]
[T_from_h_functor_aux]
type = FunctorAux
functor = 'T_from_p_h'
variable = 'T'
execute_on = 'NONLINEAR'
[]
[h_from_T_functor_aux]
type = FunctorAux
functor = 'h_from_p_T'
variable = 'h_aux'
execute_on = 'NONLINEAR'
[]
[]
[Postprocessors]
[T_out_sim]
type = ElementalVariableValue
variable = T
elementid = ${fparse nx-1}
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-12
pressure_l_abs_tol = 1e-12
energy_l_abs_tol = 1e-12
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
momentum_equation_relaxation = 0.7
pressure_variable_relaxation = 0.3
energy_equation_relaxation = 0.95
num_iterations = 100
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
energy_absolute_tolerance = 1e-6
print_fields = false
momentum_l_max_its = 200
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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
continue_on_max_its = true
[]
[Outputs]
[out]
type = CSV
[]
[]
(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected.i)
mu = 1.1
rho = 1.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
darcy = 1.1
forch = 1.1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = -1
ymax = 1
nx = 2
ny = 2
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
porosity = porosity
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = u
v = v
porosity = porosity
pressure = pressure
smoothing_layers = 2
[]
[]
[Variables]
[u]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[v]
type = PINSFVSuperficialVelocityVariable
initial_condition = 1
[]
[pressure]
type = INSFVPressureVariable
[]
[]
[AuxVariables]
[eps_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[eps_out]
type = FunctorAux
variable = eps_out
functor = porosity
execute_on = 'timestep_end'
[]
[]
[FVKernels]
[mass]
type = PINSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[mass_forcing]
type = FVBodyForce
variable = pressure
function = forcing_p
[]
[u_advection]
type = PINSFVMomentumAdvection
variable = u
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = PINSFVMomentumDiffusion
variable = u
mu = ${mu}
porosity = porosity
momentum_component = 'x'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = u
pressure = pressure
porosity = porosity
momentum_component = 'x'
[]
[u_drag]
type = PINSFVMomentumFriction
variable = u
momentum_component = 'x'
rho = ${rho}
speed = speed
mu = ${mu}
[]
[u_correction]
type = PINSFVMomentumFrictionCorrection
variable = u
momentum_component = 'x'
rho = ${rho}
speed = speed
mu = ${mu}
[]
[u_forcing]
type = INSFVBodyForce
variable = u
functor = forcing_u
momentum_component = 'x'
[]
[v_advection]
type = PINSFVMomentumAdvection
variable = v
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = PINSFVMomentumDiffusion
variable = v
mu = ${mu}
porosity = porosity
momentum_component = 'y'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = v
pressure = pressure
porosity = porosity
momentum_component = 'y'
[]
[v_drag]
type = PINSFVMomentumFriction
variable = v
momentum_component = 'y'
rho = ${rho}
speed = speed
mu = ${mu}
[]
[v_correction]
type = PINSFVMomentumFrictionCorrection
variable = v
momentum_component = 'y'
rho = ${rho}
speed = speed
mu = ${mu}
[]
[v_forcing]
type = INSFVBodyForce
variable = v
functor = forcing_v
momentum_component = 'y'
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = u
functor = 'exact_u'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = v
functor = 'exact_v'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = u
function = 'exact_u'
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = v
function = 'exact_v'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = 'exact_p'
[]
[]
[FunctorMaterials]
[darcy]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coefficient Forchheimer_coefficient'
prop_values = '${darcy} ${darcy} ${darcy} ${forch} ${forch} ${forch}'
[]
[speed]
type = PINSFVSpeedFunctorMaterial
superficial_vel_x = u
superficial_vel_y = v
porosity = porosity
[]
[]
[Functions]
[porosity]
type = ParsedFunction
expression = '.5 + .1 * sin(pi * x / 4) * cos(pi * y / 4)'
[]
[exact_u]
type = ParsedFunction
expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
[]
[forcing_u]
type = ParsedFunction
expression = 'darcy*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) + (1/2)*forch*rho*sqrt(sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2 + sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.1*pi^2*sin((1/4)*x*pi)*sin((1/4)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.025*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.025*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.1*pi^2*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/2)*y*pi)*cos((1/4)*x*pi)^2*cos((1/2)*x*pi)*cos((1/4)*y*pi)^2/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) + 0.025*pi*mu*(0.1*pi*sin((1/4)*x*pi)*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + (1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*(-0.1*pi*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.1*pi*rho*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.1*pi*rho*sin((1/2)*y*pi)^2*cos((1/4)*x*pi)*cos((1/2)*x*pi)^2*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/4*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
symbol_names = 'mu rho darcy forch'
symbol_values = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_v]
type = ParsedFunction
expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
[]
[forcing_v]
type = ParsedFunction
expression = 'darcy*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) + (1/2)*forch*rho*sqrt(sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2 + sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-0.1*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.025*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.025*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.05*pi^2*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) + 0.025*pi*mu*(0.1*pi*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*(-0.1*pi*sin((1/4)*x*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + (1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.1*pi*rho*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)*cos((1/2)*y*pi)^2/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.1*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (3/2)*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
symbol_names = 'mu rho darcy forch'
symbol_values = '${mu} ${rho} ${darcy} ${forch}'
[]
[exact_p]
type = ParsedFunction
expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
[]
[forcing_p]
type = ParsedFunction
expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
symbol_names = 'rho'
symbol_values = '${rho}'
[]
[]
[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
[]
[Outputs]
exodus = false
csv = true
[]
[Postprocessors]
[h]
type = AverageElementSize
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2u]
type = ElementL2FunctorError
approximate = u
exact = exact_u
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2v]
type = ElementL2FunctorError
approximate = v
exact = exact_v
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[L2p]
type = ElementL2FunctorError
approximate = pressure
exact = exact_p
outputs = 'console csv'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/natural_convection/natural_circulation_pipe.i)
# natural convection through a pipe
# Reference solution in "reference_pipe_natural_convection.py"
# Reference mdot: 0.0792 kg/s
# this input
# iy mdot
# 10 8.302364e-02
# 20 8.111192e-02
# 40 8.007924e-02
# 80 7.954403e-02
# 160 7.927201e-02
# Convergence to the analytical result is observed
height = 10.0
gravity = 9.81
p0 = 1e5
molar_mass = 29.0e-3
T0 = 328
Ru = 8.3145
Ri = '${fparse Ru / molar_mass}'
density = '${fparse p0 / (Ri * T0)}'
head = '${fparse height * density * gravity}'
k = 25.68e-3
gamma = 1.4
[Mesh]
[mesh]
type = CartesianMeshGenerator
dim = 2
dx = '0.1'
ix = '2'
dy = '${height}'
iy = '5'
[]
[]
[GlobalParams]
rhie_chow_user_object = pins_rhie_chow_interpolator
[]
[FluidProperties]
[air]
type = IdealGasFluidProperties
molar_mass = ${molar_mass}
k = ${k}
gamma = ${gamma}
[]
[]
[Modules]
[NavierStokesFV]
compressibility = 'weakly-compressible'
add_energy_equation = true
gravity = '0 -${gravity} 0'
density = rho
dynamic_viscosity = mu
specific_heat = cp
thermal_conductivity = k
initial_velocity = '0 1e-6 0'
initial_pressure = ${p0}
initial_temperature = ${T0}
inlet_boundaries = 'bottom'
momentum_inlet_types = 'fixed-pressure'
momentum_inlet_function = '${fparse p0 + head}'
energy_inlet_types = 'fixed-temperature'
energy_inlet_function = '${T0}'
energy_scaling = 1e-5
wall_boundaries = 'left right'
momentum_wall_types = 'slip slip'
energy_wall_types = 'heatflux heatflux'
energy_wall_function = '300 300'
outlet_boundaries = 'top'
momentum_outlet_types = 'fixed-pressure'
pressure_function = '${fparse p0}'
momentum_advection_interpolation = 'upwind'
mass_advection_interpolation = 'upwind'
porous_medium_treatment = true
porosity = porosity
energy_advection_interpolation = 'average'
[]
[]
[FVKernels]
[u_friction]
type = PINSFVMomentumFriction
variable = superficial_vel_x
Darcy_name = linear_friction_coeff
momentum_component = 'x'
standard_friction_formulation = false
rho = rho
[]
[v_friction]
type = PINSFVMomentumFriction
variable = superficial_vel_y
Darcy_name = linear_friction_coeff
momentum_component = 'y'
standard_friction_formulation = false
rho = rho
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6
end_time = 1e4
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.1
growth_factor = 2
iteration_window = 2
optimal_iterations = 6
[]
[]
[Functions]
[mu_rampdown_fn]
type = PiecewiseLinear
x = '0 0.5 1 5 10 100 1000 2000'
y = '1000 1000 100 10 1 1 1 0'
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = air
pressure = pressure
T_fluid = T_fluid
speed = speed
force_define_density = true
neglect_derivatives_of_density_time_derivative = false
mu_rampdown = 'mu_rampdown_fn'
characteristic_length = 1
porosity = porosity
[]
[scalar_props]
type = ADGenericFunctorMaterial
prop_names = 'porosity loss_coeff'
prop_values = '1 1.3'
[]
[linear_friction]
type = ADParsedFunctorMaterial
property_name = 'linear_friction'
expression = 'loss_coeff * rho'
functor_names = 'loss_coeff rho'
[]
[linear_friction_coeff]
type = ADGenericVectorFunctorMaterial
prop_names = 'linear_friction_coeff'
prop_values = 'linear_friction linear_friction linear_friction'
[]
[]
[AuxVariables]
[rho_var]
type = MooseVariableFVReal
[]
[cp_var]
type = MooseVariableFVReal
[]
[rho_cp_T_fluid_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[rho_var_aux]
type = FunctorAux
variable = rho_var
functor = rho
[]
[cp_var_aux]
type = FunctorAux
variable = cp_var
functor = cp
[]
[rho_cp_T_fluid_var_aux]
type = ParsedAux
variable = rho_cp_T_fluid_var
coupled_variables = 'rho_var cp_var T_fluid'
expression = 'rho_var * cp_var * T_fluid'
[]
[]
[Postprocessors]
[inlet_mfr]
type = VolumetricFlowRate
vel_x = superficial_vel_x
vel_y = superficial_vel_y
advected_quantity = rho
boundary = bottom
advected_interp_method = average
[]
[outlet_mfr]
type = VolumetricFlowRate
vel_x = superficial_vel_x
vel_y = superficial_vel_y
advected_quantity = rho
boundary = top
advected_interp_method = average
[]
[inlet_energy]
type = VolumetricFlowRate
vel_x = superficial_vel_x
vel_y = superficial_vel_y
advected_quantity = rho_cp_T_fluid_var
boundary = bottom
advected_interp_method = average
[]
[outlet_energy]
type = VolumetricFlowRate
vel_x = superficial_vel_x
vel_y = superficial_vel_y
advected_quantity = rho_cp_T_fluid_var
boundary = top
advected_interp_method = average
[]
[]
[Debug]
show_var_residual_norms = true
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/materials/functorfluidprops.i)
# Operating conditions
inlet_temp = 300
outlet_pressure = 1e5
inlet_v = 4
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 2
ymin = 0
ymax = 1
nx = 5
ny = 5
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = ${inlet_v}
[]
[v]
type = INSFVVelocityVariable
initial_condition = 2
[]
[pressure]
type = INSFVPressureVariable
initial_condition = ${outlet_pressure}
[]
[T]
type = INSFVEnergyVariable
initial_condition = ${inlet_temp}
[]
[]
[FVKernels]
[u_time]
type = FVFunctorTimeKernel
variable = u
[]
[v_time]
type = FVFunctorTimeKernel
variable = v
[]
[p_time]
type = FVFunctorTimeKernel
variable = pressure
[]
[T_time]
type = FVFunctorTimeKernel
variable = T
[]
[]
[FluidProperties]
[fp]
type = FlibeFluidProperties
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = fp
pressure = 'pressure'
T_fluid = 'T'
speed = 'velocity_norm'
# For porous flow
characteristic_length = 2
porosity = 'porosity'
[]
[]
[AuxVariables]
[velocity_norm]
type = MooseVariableFVReal
[]
[porosity]
type = MooseVariableFVReal
initial_condition = 0.4
[]
[rho_var]
type = MooseVariableFVReal
[]
[drho_dp_var]
type = MooseVariableFVReal
[]
[drho_dT_var]
type = MooseVariableFVReal
[]
[rho_dot_var]
type = MooseVariableFVReal
[]
[cp_var]
type = MooseVariableFVReal
[]
[dcp_dp_var]
type = MooseVariableFVReal
[]
[dcp_dT_var]
type = MooseVariableFVReal
[]
[cp_dot_var]
type = MooseVariableFVReal
[]
[cv_var]
type = MooseVariableFVReal
[]
[mu_var]
type = MooseVariableFVReal
[]
[dmu_dp_var]
type = MooseVariableFVReal
[]
[dmu_dT_var]
type = MooseVariableFVReal
[]
[k_var]
type = MooseVariableFVReal
[]
[dk_dp_var]
type = MooseVariableFVReal
[]
[dk_dT_var]
type = MooseVariableFVReal
[]
[Pr_var]
type = MooseVariableFVReal
[]
[dPr_dp_var]
type = MooseVariableFVReal
[]
[dPr_dT_var]
type = MooseVariableFVReal
[]
[Re_var]
type = MooseVariableFVReal
[]
[dRe_dp_var]
type = MooseVariableFVReal
[]
[dRe_dT_var]
type = MooseVariableFVReal
[]
[Re_h_var]
type = MooseVariableFVReal
[]
[Re_i_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[speed]
type = VectorMagnitudeAux
variable = 'velocity_norm'
x = u
y = v
[]
# To output the functor material properties
[rho_out]
type = FunctorAux
functor = 'rho'
variable = 'rho_var'
execute_on = 'timestep_begin'
[]
[drho_dp_out]
type = FunctorAux
functor = 'drho/dpressure'
variable = 'drho_dp_var'
execute_on = 'timestep_begin'
[]
[drho_dT_out]
type = FunctorAux
functor = 'drho/dT_fluid'
variable = 'drho_dT_var'
execute_on = 'timestep_begin'
[]
[drho_dt_out]
type = FunctorAux
functor = 'drho_dt'
variable = 'rho_dot_var'
execute_on = 'timestep_begin'
[]
[cp_out]
type = FunctorAux
functor = 'cp'
variable = 'cp_var'
execute_on = 'timestep_begin'
[]
[dcp_dp_out]
type = FunctorAux
functor = 'dcp/dpressure'
variable = 'dcp_dp_var'
execute_on = 'timestep_begin'
[]
[dcp_dT_out]
type = FunctorAux
functor = 'dcp/dT_fluid'
variable = 'dcp_dT_var'
execute_on = 'timestep_begin'
[]
[dcp_dt_out]
type = FunctorAux
functor = 'dcp_dt'
variable = 'cp_dot_var'
execute_on = 'timestep_begin'
[]
[cv_out]
type = FunctorAux
functor = 'cv'
variable = 'cv_var'
execute_on = 'timestep_begin'
[]
[mu_out]
type = FunctorAux
functor = 'mu'
variable = 'mu_var'
execute_on = 'timestep_begin'
[]
[dmu_dp_out]
type = FunctorAux
functor = 'dmu/dpressure'
variable = 'dmu_dp_var'
execute_on = 'timestep_begin'
[]
[dmu_dT_out]
type = FunctorAux
functor = 'dmu/dT_fluid'
variable = 'dmu_dT_var'
execute_on = 'timestep_begin'
[]
[k_out]
type = FunctorAux
functor = 'k'
variable = 'k_var'
execute_on = 'timestep_begin'
[]
[dk_dp_out]
type = FunctorAux
functor = 'dk/dpressure'
variable = 'dk_dp_var'
execute_on = 'timestep_begin'
[]
[dk_dT_out]
type = FunctorAux
functor = 'dk/dT_fluid'
variable = 'dk_dT_var'
execute_on = 'timestep_begin'
[]
[Pr_out]
type = FunctorAux
functor = 'Pr'
variable = 'Pr_var'
execute_on = 'timestep_begin'
[]
[dPr_dp_out]
type = FunctorAux
functor = 'dPr/dpressure'
variable = 'dPr_dp_var'
execute_on = 'timestep_begin'
[]
[dPr_dT_out]
type = FunctorAux
functor = 'dPr/dT_fluid'
variable = 'dPr_dT_var'
execute_on = 'timestep_begin'
[]
[Re_out]
type = FunctorAux
functor = 'Re'
variable = 'Re_var'
execute_on = 'timestep_begin'
[]
[dRe_dp_out]
type = FunctorAux
functor = 'dRe/dpressure'
variable = 'dRe_dp_var'
execute_on = 'timestep_begin'
[]
[dRe_dT_out]
type = FunctorAux
functor = 'dRe/dT_fluid'
variable = 'dRe_dT_var'
execute_on = 'timestep_begin'
[]
[Re_h_out]
type = FunctorAux
functor = 'Re_h'
variable = 'Re_h_var'
execute_on = 'timestep_begin'
[]
[Re_i_out]
type = FunctorAux
functor = 'Re_i'
variable = 'Re_i_var'
execute_on = 'timestep_begin'
[]
[]
[Executioner]
type = Transient
end_time = 0.1
dt = 0.1
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/materials/ergun/ergun.i)
# This file simulates flow of fluid in a porous elbow for the purpose of verifying
# correct implementation of the various different solution variable sets. This input
# tests correct implementation of the primitive superficial variable set. Flow enters on the top
# and exits on the right. Because the purpose is only to test the equivalence of
# different equation sets, no solid energy equation is included.
porosity_left = 0.4
porosity_right = 0.6
pebble_diameter = 0.06
mu = 1.81e-5 # This has been increased to avoid refining the mesh
M = 28.97e-3
R = 8.3144598
# inlet mass flowrate, kg/s
mdot = -10.0
# inlet mass flux (superficial)
mflux_in_superficial = ${fparse mdot / (pi * 0.5 * 0.5)}
# inlet mass flux (interstitial)
mflux_in_interstitial = ${fparse mflux_in_superficial / porosity_left}
p_initial = 201325.0
T_initial = 300.0
rho_initial = ${fparse p_initial / T_initial * M / R}
vel_y_initial = ${fparse mflux_in_interstitial / rho_initial}
vel_x_initial = 0.0
superficial_vel_y_initial = ${fparse mflux_in_superficial / rho_initial}
superficial_vel_x_initial = 1e-12
# Computation parameters
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
# ==============================================================================
# GEOMETRY AND MESH
# ==============================================================================
[Mesh]
[fmg]
type = FileMeshGenerator
file = 'ergun_in.e'
[]
coord_type = RZ
[]
[UserObjects]
[rc]
type = PINSFVRhieChowInterpolator
u = superficial_vel_x
v = superficial_vel_y
pressure = pressure
porosity = porosity
[]
[]
[GlobalParams]
porosity = porosity
pebble_diameter = ${pebble_diameter}
fp = fp
# rho for the kernels. Must match fluid property!
rho = ${rho_initial}
fv = true
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
# behavior at time of test creation
two_term_boundary_expansion = false
rhie_chow_user_object = 'rc'
[]
# ==============================================================================
# VARIABLES AND KERNELS
# ==============================================================================
[Variables]
[pressure]
type = INSFVPressureVariable
initial_condition = ${p_initial}
[]
[superficial_vel_x]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${superficial_vel_x_initial}
[]
[superficial_vel_y]
type = PINSFVSuperficialVelocityVariable
initial_condition = ${superficial_vel_y_initial}
[]
[]
[FVKernels]
# Mass Equation.
[mass]
type = PINSFVMassAdvection
variable = 'pressure'
[]
# Momentum x component equation.
[vel_x_time]
type = PINSFVMomentumTimeDerivative
variable = 'superficial_vel_x'
momentum_component = 'x'
[]
[vel_x_advection]
type = PINSFVMomentumAdvection
variable = 'superficial_vel_x'
momentum_component = 'x'
[]
[vel_x_viscosity]
type = PINSFVMomentumDiffusion
variable = 'superficial_vel_x'
momentum_component = 'x'
mu = 'mu'
[]
[u_pressure]
type = PINSFVMomentumPressure
variable = 'superficial_vel_x'
pressure = pressure
momentum_component = 'x'
[]
[u_friction]
type = PINSFVMomentumFriction
variable = 'superficial_vel_x'
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
momentum_component = 'x'
speed = speed
mu = 'mu'
[]
# Momentum y component equation.
[vel_y_time]
type = PINSFVMomentumTimeDerivative
variable = 'superficial_vel_y'
momentum_component = 'y'
[]
[vel_y_advection]
type = PINSFVMomentumAdvection
variable = 'superficial_vel_y'
momentum_component = 'y'
[]
[vel_y_viscosity]
type = PINSFVMomentumDiffusion
variable = 'superficial_vel_y'
momentum_component = 'y'
mu = 'mu'
[]
[v_pressure]
type = PINSFVMomentumPressure
variable = 'superficial_vel_y'
pressure = pressure
momentum_component = 'y'
[]
[v_friction]
type = PINSFVMomentumFriction
variable = 'superficial_vel_y'
Darcy_name = 'Darcy_coefficient'
Forchheimer_name = 'Forchheimer_coefficient'
momentum_component = 'y'
mu = 'mu'
speed = speed
[]
[gravity]
type = PINSFVMomentumGravity
variable = 'superficial_vel_y'
gravity = '0 -9.81 0'
momentum_component = 'y'
[]
[]
# ==============================================================================
# AUXVARIABLES AND AUXKERNELS
# ==============================================================================
[AuxVariables]
[T_fluid]
initial_condition = ${T_initial}
order = CONSTANT
family = MONOMIAL
[]
[vel_x]
initial_condition = ${fparse vel_x_initial}
order = CONSTANT
family = MONOMIAL
[]
[vel_y]
initial_condition = ${fparse vel_y_initial}
order = CONSTANT
family = MONOMIAL
[]
[porosity_out]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[vel_x]
type = FunctorAux
variable = vel_x
functor = vel_x_mat
[]
[vel_y]
type = FunctorAux
variable = vel_y
functor = vel_y_mat
[]
[porosity_out]
type = FunctorAux
variable = porosity_out
functor = porosity
[]
[]
# ==============================================================================
# FLUID PROPERTIES, MATERIALS AND USER OBJECTS
# ==============================================================================
[FluidProperties]
[fp]
type = IdealGasFluidProperties
k = 0.0
mu = ${mu}
gamma = 1.4
molar_mass = ${M}
[]
[]
[FunctorMaterials]
[enthalpy]
type = INSFVEnthalpyMaterial
temperature = 'T_fluid'
[]
[speed]
type = PINSFVSpeedFunctorMaterial
superficial_vel_x = 'superficial_vel_x'
superficial_vel_y = 'superficial_vel_y'
porosity = porosity
vel_x = vel_x_mat
vel_y = vel_y_mat
[]
[kappa]
type = FunctorKappaFluid
[]
[const_Fdrags_mat]
type = FunctorErgunDragCoefficients
porosity = porosity
[]
[fluidprops]
type = GeneralFunctorFluidProps
mu_rampdown = mu_func
porosity = porosity
characteristic_length = ${pebble_diameter}
T_fluid = 'T_fluid'
pressure = 'pressure'
speed = 'speed'
[]
[]
d = 0.05
[Functions]
[mu_func]
type = PiecewiseLinear
x = '1 3 5 10 15 20'
y = '1e5 1e4 1e3 1e2 1e1 1'
[]
[real_porosity_function]
type = ParsedFunction
expression = 'if (x < 0.6 - ${d}, ${porosity_left}, if (x > 0.6 + ${d}, ${porosity_right},
(x-(0.6-${d}))/(2*${d})*(${porosity_right}-${porosity_left}) + ${porosity_left}))'
[]
[porosity]
type = ParsedFunction
expression = 'if (x < 0.6 - ${d}, ${porosity_left}, if (x > 0.6 + ${d}, ${porosity_right},
(x-(0.6-${d}))/(2*${d})*(${porosity_right}-${porosity_left}) + ${porosity_left}))'
[]
[]
# ==============================================================================
# BOUNDARY CONDITIONS
# ==============================================================================
[FVBCs]
[outlet_p]
type = INSFVOutletPressureBC
variable = 'pressure'
function = ${p_initial}
boundary = 'right'
[]
## No or Free slip BC
[free-slip-wall-x]
type = INSFVNaturalFreeSlipBC
boundary = 'bottom wall_1 wall_2 left'
variable = superficial_vel_x
momentum_component = 'x'
[]
[free-slip-wall-y]
type = INSFVNaturalFreeSlipBC
boundary = 'bottom wall_1 wall_2 left'
variable = superficial_vel_y
momentum_component = 'y'
[]
## Symmetry
[symmetry-x]
type = PINSFVSymmetryVelocityBC
boundary = 'left'
variable = superficial_vel_x
u = superficial_vel_x
v = superficial_vel_y
mu = 'mu'
momentum_component = 'x'
[]
[symmetry-y]
type = PINSFVSymmetryVelocityBC
boundary = 'left'
variable = superficial_vel_y
u = superficial_vel_x
v = superficial_vel_y
mu = 'mu'
momentum_component = 'y'
[]
[symmetry-p]
type = INSFVSymmetryPressureBC
boundary = 'left'
variable = 'pressure'
[]
## inlet
[inlet_vel_x]
type = INSFVInletVelocityBC
variable = 'superficial_vel_x'
function = ${superficial_vel_x_initial}
boundary = 'top'
[]
[inlet_vel_y]
type = INSFVInletVelocityBC
variable = 'superficial_vel_y'
function = ${superficial_vel_y_initial}
boundary = 'top'
[]
[]
# ==============================================================================
# EXECUTION PARAMETERS
# ==============================================================================
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
petsc_options_value = 'asm lu NONZERO 200'
line_search = 'none'
# Problem time parameters
dtmin = 0.01
dtmax = 2000
end_time = 3000
# must be the same as the fluid
# Iterations parameters
l_max_its = 50
l_tol = 1e-8
nl_max_its = 25
# nl_rel_tol = 5e-7
nl_abs_tol = 2e-7
# Automatic scaling
automatic_scaling = true
verbose = true
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.025
cutback_factor = 0.5
growth_factor = 2.0
[]
# Steady state detection.
steady_state_detection = true
steady_state_tolerance = 1e-7
steady_state_start_time = 400
[]
# ==============================================================================
# POSTPROCESSORS DEBUG AND OUTPUTS
# ==============================================================================
[Postprocessors]
[mass_flow_in]
type = VolumetricFlowRate
boundary = 'top'
vel_x = 'superficial_vel_x'
vel_y = 'superficial_vel_y'
advected_quantity = ${rho_initial}
execute_on = 'INITIAL TIMESTEP_END'
[]
[mass_flow_out]
type = VolumetricFlowRate
boundary = 'right'
vel_x = 'superficial_vel_x'
vel_y = 'superficial_vel_y'
advected_quantity = ${rho_initial}
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_in]
type = SideAverageValue
variable = pressure
boundary = 'top'
[]
[dP]
type = LinearCombinationPostprocessor
pp_names = 'p_in'
pp_coefs = '1.0'
b = ${fparse -p_initial}
[]
[]
[Outputs]
exodus = true
print_linear_residuals = false
[]
(modules/navier_stokes/examples/laser-welding/2d-fv.i)
period=.2e-4 # s
endtime=${fparse 3 * period} # s
timestep=${fparse period / 100} # s
surfacetemp=2700 # K
bottomtemp=2700 # K
sb=5.67e-8 # W/(m^2 K^4)
advected_interp_method='upwind'
velocity_interp_method='rc'
rho='rho'
mu='mu'
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[Mesh]
type = GeneratedMesh
dim = 2
xmin = -.7e-3 # m
xmax = 0.7e-3 # m
ymin = -.35e-3 # m
ymax = 0
nx = 75
ny = 20
displacements = 'disp_x disp_y'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
use_displaced_mesh = true
disp_x = disp_x
disp_y = disp_y
[]
[]
[Problem]
extra_tag_vectors = 'e_time e_advection e_conduction e_laser e_radiation e_mesh_advection'
[]
[AuxVariables]
[mu_out]
type = MooseVariableFVReal
[]
[e_time]
type = MooseVariableFVReal
[]
[e_advection]
type = MooseVariableFVReal
[]
[e_mesh_advection]
type = MooseVariableFVReal
[]
[e_conduction]
type = MooseVariableFVReal
[]
[e_laser]
type = MooseVariableFVReal
[]
[e_radiation]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mu_out]
type = FunctorAux
functor = mu
variable = mu_out
execute_on = timestep_end
[]
[e_time]
type = TagVectorAux
variable = e_time
vector_tag = e_time
v = T
[]
[e_advection]
type = TagVectorAux
variable = e_advection
vector_tag = e_advection
v = T
[]
[e_mesh_advection]
type = TagVectorAux
variable = e_mesh_advection
vector_tag = e_mesh_advection
v = T
[]
[e_conduction]
type = TagVectorAux
variable = e_conduction
vector_tag = e_conduction
v = T
[]
[e_laser]
type = TagVectorAux
variable = e_laser
vector_tag = e_laser
v = T
[]
[e_radiation]
type = TagVectorAux
variable = e_radiation
vector_tag = e_radiation
v = T
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
[]
[vel_y]
type = INSFVVelocityVariable
[]
[T]
type = INSFVEnergyVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[disp_x]
[]
[disp_y]
[]
[]
[ICs]
[T]
type = FunctionIC
variable = T
function = '${surfacetemp} + ((${surfacetemp} - ${bottomtemp}) / .35e-3) * y'
[]
[]
[Kernels]
[disp_x]
type = MatDiffusion
variable = disp_x
diffusivity = 1e6
[]
[disp_y]
type = MatDiffusion
variable = disp_y
diffusivity = 1e6
[]
[]
[FVKernels]
# pressure equation
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
use_displaced_mesh = true
boundaries_to_force = top
[]
# momentum equations
# u equation
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = ${rho}
momentum_component = 'x'
use_displaced_mesh = true
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'x'
use_displaced_mesh = true
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
use_displaced_mesh = true
[]
[u_pressure]
type = INSFVMomentumPressureFlux
variable = vel_x
momentum_component = 'x'
pressure = pressure
use_displaced_mesh = true
[]
[u_mesh_advection_volumetric]
type = INSFVMomentumMeshAdvection
variable = vel_x
momentum_component = 'x'
rho = ${rho}
disp_x = disp_x
disp_y = disp_y
add_to_a = false
use_displaced_mesh = true
[]
# v equation
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = ${rho}
momentum_component = 'y'
use_displaced_mesh = true
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
momentum_component = 'y'
use_displaced_mesh = true
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
use_displaced_mesh = true
[]
[v_pressure]
type = INSFVMomentumPressureFlux
variable = vel_y
momentum_component = 'y'
pressure = pressure
use_displaced_mesh = true
[]
[v_mesh_advection_volumetric]
type = INSFVMomentumMeshAdvection
variable = vel_y
momentum_component = 'y'
rho = ${rho}
disp_x = disp_x
disp_y = disp_y
add_to_a = false
use_displaced_mesh = true
[]
# energy equation
[temperature_time]
type = INSFVEnergyTimeDerivative
variable = T
rho = ${rho}
dh_dt = dh_dt
use_displaced_mesh = true
extra_vector_tags = 'e_time'
[]
[temperature_advection]
type = INSFVEnergyAdvection
variable = T
use_displaced_mesh = true
extra_vector_tags = 'e_advection'
[]
[temperature_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
use_displaced_mesh = true
extra_vector_tags = 'e_conduction'
[]
[temperature_mesh_advection_volumetric]
type = INSFVMeshAdvection
variable = T
rho = ${rho}
disp_x = disp_x
disp_y = disp_y
advected_quantity = 'h'
use_displaced_mesh = true
extra_vector_tags = 'e_mesh_advection'
[]
[]
[FVBCs]
# momentum boundary conditions
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'bottom right left'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'bottom right left'
function = 0
[]
[vapor_recoil_x]
type = INSFVVaporRecoilPressureMomentumFluxBC
variable = vel_x
boundary = 'top'
momentum_component = 'x'
rc_pressure = rc_pressure
use_displaced_mesh = true
[]
[vapor_recoil_y]
type = INSFVVaporRecoilPressureMomentumFluxBC
variable = vel_y
boundary = 'top'
momentum_component = 'y'
rc_pressure = rc_pressure
use_displaced_mesh = true
[]
# energy boundary conditions
[T_cold]
type = FVDirichletBC
variable = T
boundary = 'bottom'
value = '${bottomtemp}'
[]
[radiation_flux]
type = FVFunctorRadiativeBC
variable = T
boundary = 'top'
emissivity = '1'
Tinfinity = 300
stefan_boltzmann_constant = ${sb}
use_displaced_mesh = true
extra_vector_tags = 'e_radiation'
[]
[weld_flux]
type = FVGaussianEnergyFluxBC
variable = T
boundary = 'top'
P0 = 159.96989792079225
R = 1.25e-4
x_beam_coord = '2e-4 * sin(t * 2 * pi / ${period})'
y_beam_coord = 0
z_beam_coord = 0
use_displaced_mesh = true
extra_vector_tags = 'e_laser'
[]
[]
[BCs]
# displacement boundary conditions
[x_no_disp]
type = DirichletBC
variable = disp_x
boundary = 'bottom'
value = 0
[]
[y_no_disp]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[]
[displace_x_top]
type = INSADDisplaceBoundaryBC
boundary = 'top'
variable = 'disp_x'
velocity = 'vel'
component = 0
associated_subdomain = 0
[]
[displace_y_top]
type = INSADDisplaceBoundaryBC
boundary = 'top'
variable = 'disp_y'
velocity = 'vel'
component = 1
associated_subdomain = 0
[]
[displace_x_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'top'
variable = 'disp_x'
velocity = 'vel'
component = 0
[]
[displace_y_top_dummy]
type = INSADDummyDisplaceBoundaryIntegratedBC
boundary = 'top'
variable = 'disp_y'
velocity = 'vel'
component = 1
[]
[]
[FunctorMaterials]
[steel]
type = AriaLaserWeld304LStainlessSteelFunctorMaterial
temperature = T
beta = 1e7
[]
[disp_vec_value_and_dot]
type = ADGenericVectorFunctorMaterial
prop_names = 'disp_vec'
prop_values = 'disp_x disp_y 0'
[]
[vel]
type = ADGenericVectorFunctorMaterial
prop_names = 'vel'
prop_values = 'vel_x vel_y 0'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type -mat_mffd_err'
petsc_options_value = 'lu NONZERO strumpack 1e-6'
[]
[]
[Executioner]
type = Transient
end_time = ${endtime}
dtmin = 1e-8
dtmax = ${timestep}
petsc_options = '-snes_converged_reason -ksp_converged_reason -options_left'
solve_type = 'PJFNK'
line_search = 'none'
nl_max_its = 12
l_max_its = 100
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 7
dt = ${timestep}
linear_iteration_ratio = 1e6
growth_factor = 1.1
[]
[]
[Outputs]
exodus = true
csv = true
[]
[Debug]
show_var_residual_norms = true
[]
[Postprocessors]
[laser_flux]
type = TagVectorSum
vector = 'e_laser'
[]
[volume_rho_cp_dT]
type = TagVectorSum
vector = 'e_time'
[]
[conduction]
type = TagVectorSum
vector = 'e_conduction'
[]
[advection]
type = TagVectorSum
vector = 'e_advection'
[]
[mesh_advection]
type = TagVectorSum
vector = 'e_mesh_advection'
[]
[radiation]
type = TagVectorSum
vector = 'e_radiation'
[]
[total_sum]
type = ParsedPostprocessor
expression = 'laser_flux + volume_rho_cp_dT + advection + mesh_advection + conduction + radiation'
pp_names = 'laser_flux volume_rho_cp_dT advection mesh_advection conduction radiation'
[]
[]
(test/tests/materials/functor_properties/vector-magnitude/vector-test.i)
# This example reproduces the libmesh vector_fe example 1 results
[Mesh]
type = GeneratedMesh
dim = 2
nx = 15
ny = 15
xmin = -1
ymin = -1
[]
[Variables]
[u]
family = LAGRANGE_VEC
[]
[]
[AuxVariables]
[mag]
order = FIRST
family = MONOMIAL
[]
[]
[AuxKernels]
[mag]
type = FunctorAux
variable = mag
functor = mat_mag
[]
[]
[Kernels]
[diff]
type = VectorDiffusion
variable = u
[]
[body_force]
type = VectorBodyForce
variable = u
function_x = 'ffx'
function_y = 'ffy'
[]
[]
[BCs]
[bnd]
type = VectorFunctionDirichletBC
variable = u
function_x = 'x_exact_sln'
function_y = 'y_exact_sln'
function_z = '0'
boundary = 'left right top bottom'
[]
[]
[Functions]
[x_exact_sln]
type = ParsedFunction
expression = 'cos(.5*pi*x)*sin(.5*pi*y)'
[]
[y_exact_sln]
type = ParsedFunction
expression = 'sin(.5*pi*x)*cos(.5*pi*y)'
[]
[ffx]
type = ParsedFunction
expression = '.5*pi*pi*cos(.5*pi*x)*sin(.5*pi*y)'
[]
[ffy]
type = ParsedFunction
expression = '.5*pi*pi*sin(.5*pi*x)*cos(.5*pi*y)'
[]
[]
[Materials]
[functor]
type = ADVectorMagnitudeFunctorMaterial
vector_functor = u
vector_magnitude_name = mat_mag
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/rayleigh-bernard-two-phase.i)
mu = 1.0
rho = 1e3
mu_d = 0.3
rho_d = 1.0
dp = 0.01
U_lid = 0.0
g = -9.81
[GlobalParams]
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
rhie_chow_user_object = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 11
ny = 11
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
[]
[vel_y]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
[]
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Correctors]
[pin_pressure]
type = NSPressurePin
variable = pressure
pin_type = point-value
point = '0 0 0'
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
rho = 'rho_mixture'
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[u_buoyant]
type = INSFVMomentumGravity
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
gravity = '0 ${g} 0'
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[v_buoyant]
type = INSFVMomentumGravity
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
gravity = '0 ${g} 0'
[]
[phase_2_time]
type = FVFunctorTimeKernel
variable = phase_2
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
[]
[phase_2_diffusion]
type = FVDiffusion
variable = phase_2
coeff = 1e-3
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${U_lid}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[bottom_phase_2]
type = FVDirichletBC
variable = phase_2
boundary = 'bottom'
value = 1.0
[]
[top_phase_2]
type = FVDirichletBC
variable = phase_2
boundary = 'top'
value = 0.0
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[phase_1]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[compute_phase_1]
type = ParsedAux
variable = phase_1
coupled_variables = 'phase_2'
expression = '1 - phase_2'
[]
[]
[FunctorMaterials]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_1_names = '${rho_d} ${mu_d}'
phase_2_names = '${rho} ${mu}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient]
type = ElementExtremeFunctorValue
functor = 'drag_coefficient'
value_type = max
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 10
iteration_window = 2
growth_factor = 2
cutback_factor = 0.5
dt = 1e-3
[]
nl_max_its = 20
nl_rel_tol = 1e-03
nl_abs_tol = 1e-9
l_max_its = 5
end_time = 1e8
[]
[Outputs]
exodus = false
[CSV]
type = CSV
execute_on = 'FINAL'
[]
[]
(test/tests/meshdivisions/block_division.i)
[Mesh]
[cmg]
type = CartesianMeshGenerator
dim = 3
dx = '1.5 2.4 0.1'
dy = '1.3 0.9'
dz = '0.4 0.5 0.6 0.7'
ix = '2 1 1'
iy = '2 3'
iz = '1 1 1 1'
subdomain_id = '0 1 1
2 2 2
3 4 4
5 5 5
0 1 1
2 2 2
3 4 4
5 5 5
'
[]
[]
[MeshDivisions]
[block_div]
type = SubdomainsDivision
[]
[]
[AuxVariables]
[blocks]
family = MONOMIAL
order = CONSTANT
[]
[div]
family = MONOMIAL
order = CONSTANT
[]
[diff]
family = MONOMIAL
order = CONSTANT
[]
[]
[AuxKernels]
[mesh_div]
type = MeshDivisionAux
variable = div
mesh_division = 'block_div'
[]
[subdomains]
type = FunctorAux
functor = 'blocks_fmat'
variable = 'blocks'
[]
[difference]
type = ParsedAux
variable = diff
expression = 'blocks - div'
coupled_variables = 'blocks div'
[]
[]
[FunctorMaterials]
[fmat]
type = PiecewiseByBlockFunctorMaterial
prop_name = 'blocks_fmat'
subdomain_to_prop_value = '0 0 1 1 2 2 3 3 4 4 5 5'
[]
[]
[Postprocessors]
[min_diff]
type = ElementExtremeValue
variable = diff
value_type = 'min'
[]
[max_diff]
type = ElementExtremeValue
variable = diff
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/examples/solidification/gallium_melting.i)
##########################################################
# Simulation of Gallium Melting Experiment
# Ref: Gau, C., & Viskanta, R. (1986). Melting and solidification of a pure metal on a vertical wall.
# Key physics: melting/solidification, convective heat transfer, natural convection
##########################################################
mu = 1.81e-3
rho_solid = 6093
rho_liquid = 6093
k_solid = 32
k_liquid = 32
cp_solid = 381.5
cp_liquid = 381.5
L = 80160
alpha_b = 1.2e-4
T_solidus = 302.93
T_liquidus = '${fparse T_solidus + 0.1}'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
T_cold = 301.15
T_hot = 311.15
Nx = 100
Ny = 50
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = 88.9e-3
ymin = 0
ymax = 63.5e-3
nx = ${Nx}
ny = ${Ny}
[]
[]
[AuxVariables]
[U]
type = MooseVariableFVReal
[]
[fl]
type = MooseVariableFVReal
initial_condition = 0.0
[]
[density]
type = MooseVariableFVReal
[]
[th_cond]
type = MooseVariableFVReal
[]
[cp_var]
type = MooseVariableFVReal
[]
[darcy_coef]
type = MooseVariableFVReal
[]
[fch_coef]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[mag]
type = VectorMagnitudeAux
variable = U
x = vel_x
y = vel_y
[]
[compute_fl]
type = NSLiquidFractionAux
variable = fl
temperature = T
T_liquidus = '${T_liquidus}'
T_solidus = '${T_solidus}'
execute_on = 'TIMESTEP_END'
[]
[rho_out]
type = FunctorAux
functor = 'rho_mixture'
variable = 'density'
[]
[th_cond_out]
type = FunctorAux
functor = 'k_mixture'
variable = 'th_cond'
[]
[cp_out]
type = FunctorAux
functor = 'cp_mixture'
variable = 'cp_var'
[]
[darcy_out]
type = FunctorAux
functor = 'Darcy_coefficient'
variable = 'darcy_coef'
[]
[fch_out]
type = FunctorAux
functor = 'Forchheimer_coefficient'
variable = 'fch_coef'
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
[]
[pressure]
type = INSFVPressureVariable
[]
[lambda]
family = SCALAR
order = FIRST
[]
[T]
type = INSFVEnergyVariable
initial_condition = '${T_cold}'
scaling = 1e-4
[]
[]
[FVKernels]
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = rho_mixture
[]
[mean_zero_pressure]
type = FVIntegralValueConstraint
variable = pressure
lambda = lambda
phi0 = 0.0
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = rho_mixture
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = rho_mixture
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
[]
[u_friction]
type = PINSFVMomentumFriction
variable = vel_x
momentum_component = 'x'
u = vel_x
v = vel_y
Darcy_name = 'Darcy_coeff'
Forchheimer_name = 'Forchheimer_coeff'
rho = ${rho_liquid}
mu = ${mu}
standard_friction_formulation = false
[]
[u_buoyancy]
type = INSFVMomentumBoussinesq
variable = vel_x
T_fluid = T
gravity = '0 -9.81 0'
rho = '${rho_liquid}'
ref_temperature = ${T_cold}
momentum_component = 'x'
[]
[u_gravity]
type = INSFVMomentumGravity
variable = vel_x
gravity = '0 -9.81 0'
rho = '${rho_liquid}'
momentum_component = 'x'
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = rho_mixture
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = rho_mixture
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
[]
[v_friction]
type = PINSFVMomentumFriction
variable = vel_y
momentum_component = 'y'
u = vel_x
v = vel_y
Darcy_name = 'Darcy_coeff'
Forchheimer_name = 'Forchheimer_coeff'
rho = ${rho_liquid}
mu = ${mu}
standard_friction_formulation = false
[]
[v_buoyancy]
type = INSFVMomentumBoussinesq
variable = vel_y
T_fluid = T
gravity = '0 -9.81 0'
rho = '${rho_liquid}'
ref_temperature = ${T_cold}
momentum_component = 'y'
[]
[v_gravity]
type = INSFVMomentumGravity
variable = vel_y
gravity = '0 -9.81 0'
rho = '${rho_liquid}'
momentum_component = 'y'
[]
[T_time]
type = INSFVEnergyTimeDerivative
variable = T
rho = rho_mixture
dh_dt = dh_dt
[]
[energy_advection]
type = INSFVEnergyAdvection
variable = T
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = ${advected_interp_method}
[]
[energy_diffusion]
type = FVDiffusion
coeff = k_mixture
variable = T
[]
[energy_source]
type = NSFVPhaseChangeSource
variable = T
L = ${L}
liquid_fraction = fl
T_liquidus = ${T_liquidus}
T_solidus = ${T_solidus}
rho = 'rho_mixture'
[]
[]
[FVBCs]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'left right top bottom'
variable = vel_y
function = 0
[]
[hot_wall]
type = FVDirichletBC
variable = T
value = '${T_hot}'
boundary = 'left'
[]
[cold_wall]
type = FVDirichletBC
variable = T
value = '${T_cold}'
boundary = 'right'
[]
[]
[FunctorMaterials]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
rho = rho_mixture
cp = cp_mixture
temperature = 'T'
[]
[eff_cp]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${cp_solid} ${k_solid} ${rho_solid}'
phase_1_names = '${cp_liquid} ${k_liquid} ${rho_liquid}'
prop_names = 'cp_mixture k_mixture rho_mixture'
phase_1_fraction = fl
[]
[mushy_zone_resistance]
type = INSFVMushyPorousFrictionFunctorMaterial
liquid_fraction = 'fl'
mu = '${mu}'
rho_l = '${rho_liquid}'
dendrite_spacing_scaling = 1e-1
[]
[friction]
type = ADGenericVectorFunctorMaterial
prop_names = 'Darcy_coeff Forchheimer_coeff'
prop_values = 'darcy_coef darcy_coef darcy_coef fch_coef fch_coef fch_coef'
[]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'alpha_b'
prop_values = '${alpha_b}'
[]
[]
[Executioner]
type = Transient
# Time-stepping parameters
start_time = 0.0
end_time = 200.0
num_steps = 2
[TimeStepper]
type = IterationAdaptiveDT
# Raise time step often but not by as much
# There's a rough spot for convergence near 10% fluid fraction
optimal_iterations = 15
growth_factor = 1.5
dt = 0.1
[]
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_rel_tol = 1e-6
nl_max_its = 30
line_search = 'none'
[]
[Postprocessors]
[ave_p]
type = ElementAverageValue
variable = 'pressure'
execute_on = 'INITIAL TIMESTEP_END'
[]
[ave_fl]
type = ElementAverageValue
variable = 'fl'
execute_on = 'INITIAL TIMESTEP_END'
[]
[ave_T]
type = ElementAverageValue
variable = 'T'
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[VectorPostprocessors]
[vel_x]
type = ElementValueSampler
variable = 'vel_x fl'
sort_by = 'x'
[]
[]
[Outputs]
exodus = true
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-w-interface-area.i)
mu = 10.0
rho = 100.0
mu_d = 1.0
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.0
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
mass_exchange_coeff = 0.01
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[Problem]
identify_variable_groups_in_nl = false
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 5}'
ymin = '${fparse -l / 2}'
ymax = '${fparse l / 2}'
nx = 20
ny = 5
[]
uniform_refine = 0
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
[]
[pressure]
type = INSFVPressureVariable
[]
[phase_2]
type = INSFVScalarFieldVariable
[]
[interface_area]
type = INSFVScalarFieldVariable
[]
[]
[FVKernels]
inactive = 'u_time v_time phase_2_time interface_area_time'
[mass]
type = INSFVMassAdvection
variable = pressure
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = ${rho}
[]
[u_time]
type = INSFVMomentumTimeDerivative
variable = vel_x
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'x'
[]
[u_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_x
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_time]
type = INSFVMomentumTimeDerivative
variable = vel_y
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
advected_interp_method = ${advected_interp_method}
velocity_interp_method = ${velocity_interp_method}
rho = 'rho_mixture'
momentum_component = 'y'
[]
[v_drift]
type = WCNSFV2PMomentumDriftFlux
variable = vel_y
rho_d = ${rho_d}
fd = 'rho_mixture_var'
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_mixture'
limit_interpolation = true
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[phase_2_time]
type = FVFunctorTimeKernel
variable = phase_2
functor = phase_2
[]
[phase_2_advection]
type = INSFVScalarFieldAdvection
variable = phase_2
u_slip = 'vel_slip_x'
v_slip = 'vel_slip_y'
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[phase_2_diffusion]
type = FVDiffusion
variable = phase_2
coeff = 1.0
[]
[phase_2_src]
type = NSFVMixturePhaseInterface
variable = phase_2
phase_coupled = phase_1
alpha = ${mass_exchange_coeff}
[]
[interface_area_time]
type = FVFunctorTimeKernel
variable = interface_area
functor = interface_area
[]
[interface_area_advection]
type = INSFVScalarFieldAdvection
variable = interface_area
velocity_interp_method = ${velocity_interp_method}
advected_interp_method = 'upwind'
[]
[interface_area_diffusion]
type = FVDiffusion
variable = interface_area
coeff = 0.1
[]
[interface_area_source_sink]
type = WCNSFV2PInterfaceAreaSourceSink
variable = interface_area
u = 'vel_x'
v = 'vel_y'
L = 1.0
rho = 'rho_mixture'
rho_d = ${rho_d}
pressure = 'pressure'
k_c = ${fparse mass_exchange_coeff * 100.0}
fd = 'phase_2'
sigma = 1e-3
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = '${U}'
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = '0'
[]
[walls-u]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_x
function = 0
[]
[walls-v]
type = INSFVNoSlipWallBC
boundary = 'top bottom'
variable = vel_y
function = 0
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = '0'
[]
[inlet_phase_2]
type = FVDirichletBC
boundary = 'left'
variable = phase_2
value = ${inlet_phase_2}
[]
[inlet_interface_area]
type = FVDirichletBC
boundary = 'left'
variable = interface_area
value = 0.0
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[rho_mixture_var]
type = MooseVariableFVReal
[]
[mu_mixture_var]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
[]
[populate_rho_mixture_var]
type = FunctorAux
variable = rho_mixture_var
functor = 'rho_mixture'
[]
[populate_mu_mixture_var]
type = FunctorAux
variable = mu_mixture_var
functor = 'mu_mixture'
[]
[]
[FunctorMaterials]
[populate_u_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_x'
momentum_component = 'x'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[populate_v_slip]
type = WCNSFV2PSlipVelocityFunctorMaterial
slip_velocity_name = 'vel_slip_y'
momentum_component = 'y'
u = 'vel_x'
v = 'vel_y'
rho = ${rho}
mu = 'mu_mixture'
rho_d = ${rho_d}
particle_diameter = ${dp}
linear_coef_name = 'Darcy_coefficient'
[]
[compute_phase_1]
type = ADParsedFunctorMaterial
property_name = phase_1
functor_names = 'phase_2'
expression = '1 - phase_2'
[]
[CD]
type = NSFVDispersePhaseDragFunctorMaterial
rho = 'rho_mixture'
mu = mu_mixture
u = 'vel_x'
v = 'vel_y'
particle_diameter = ${dp}
[]
[mixing_material]
type = NSFVMixtureFunctorMaterial
phase_2_names = '${rho} ${mu}'
phase_1_names = '${rho_d} ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
# dt = 0.1
# end_time = 1.0
# nl_max_its = 10
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
function = '${rho} * ${l} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/lid-driven-two-phase-physics.i)
mu = 1.0
rho = 1.0e3
mu_d = 0.3
rho_d = 1.0
dp = 0.01
U_lid = 0.1
g = -9.81
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
k = 1
k_d = 1
cp = 1
cp_d = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 5
ny = 5
[]
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'incompressible'
density = 'rho_mixture'
dynamic_viscosity = 'mu_mixture'
# Initial conditions
initial_velocity = '0 0 0'
initial_pressure = 0
# Pressure pin
pin_pressure = true
pinned_pressure_type = 'point-value'
pinned_pressure_point = '0 0 0'
pinned_pressure_value = '0'
# Gravity
gravity = '0 ${g} 0'
# Boundary conditions are defined outside of the Physics
# Moving walls are not that common of a problem
mass_advection_interpolation = '${advected_interp_method}'
momentum_advection_interpolation = '${advected_interp_method}'
velocity_interpolation = '${velocity_interp_method}'
[]
[]
[TwoPhaseMixture]
[mixture]
phase_1_fraction_name = 'phase_1'
phase_2_fraction_name = 'phase_2'
add_phase_transport_equation = true
phase_advection_interpolation = '${advected_interp_method}'
phase_fraction_diffusivity = 1e-3
# We could consider adding fixed-value-yet-not-an-inlet
# boundary conditions to the TwoPhaseMixture physics
# Base phase material properties
phase_1_density_name = ${rho}
phase_1_viscosity_name = ${mu}
phase_1_specific_heat_name = ${cp}
phase_1_thermal_conductivity_name = ${k}
# Other phase material properties
phase_2_density_name = ${rho_d}
phase_2_viscosity_name = ${mu_d}
phase_2_specific_heat_name = ${cp_d}
phase_2_thermal_conductivity_name = ${k_d}
output_all_properties = true
# Friction model, not actually used!
use_dispersed_phase_drag_model = true
particle_diameter = ${dp}
[]
[]
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${U_lid}
[]
[no_slip_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'left right bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = vel_y
boundary = 'left right top bottom'
function = 0
[]
[bottom_phase_2]
type = FVDirichletBC
variable = phase_2
boundary = 'bottom'
value = 1.0
[]
[top_phase_2]
type = FVDirichletBC
variable = phase_2
boundary = 'top'
value = 0.0
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
execute_on = 'TIMESTEP_END'
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient]
type = ElementExtremeFunctorValue
functor = 'drag_coefficient'
value_type = max
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 7
iteration_window = 2
growth_factor = 2.0
cutback_factor = 0.5
dt = 1e-3
[]
nl_max_its = 20
nl_rel_tol = 1e-03
nl_abs_tol = 1e-9
l_max_its = 5
end_time = 1e8
line_search=none
[]
[Outputs]
exodus = false
[CSV]
type = CSV
execute_on = 'FINAL'
execute_scalars_on = NONE
[]
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/lid-driven-two-phase-physics.i)
mu = 1.0
rho = 1.0e3
mu_d = 0.3
rho_d = 5e2
dp = 0.01
U_lid = 0.1
advected_interp_method = 'upwind'
k = 1
k_d = 1
cp = 1
cp_d = 1
[Mesh]
inactive = 'make_skew'
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 10
ny = 10
[]
[make_skew]
type = MoveNodeGenerator
input = 'gen'
node_id = 0
shift_position = '0.007 0.0021 0'
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system phi_system'
[]
[Physics]
[NavierStokes]
[FlowSegregated]
[flow]
compressibility = 'incompressible'
density = 'rho_mixture'
dynamic_viscosity = 'mu_mixture'
# Initial conditions
initial_velocity = '1e-12 1e-12 0'
initial_pressure = 0.2
wall_boundaries = 'top left right bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '${U_lid} 0; 0 0; 0 0; 0 0'
orthogonality_correction = false
pressure_two_term_bc_expansion = true
momentum_advection_interpolation = ${advected_interp_method}
[]
[]
[TwoPhaseMixtureSegregated]
[mixture]
system_names = 'phi_system'
phase_1_fraction_name = 'phase_1'
phase_2_fraction_name = 'phase_2'
add_phase_transport_equation = true
phase_advection_interpolation = '${advected_interp_method}'
phase_fraction_diffusivity = 1e-3
# We could consider adding fixed-value-yet-not-an-inlet
# boundary conditions to the TwoPhaseMixture physics
# Base phase material properties
phase_1_density_name = ${rho}
phase_1_viscosity_name = ${mu}
phase_1_specific_heat_name = ${cp}
phase_1_thermal_conductivity_name = ${k}
# Other phase material properties
phase_2_density_name = ${rho_d}
phase_2_viscosity_name = ${mu_d}
phase_2_specific_heat_name = ${cp_d}
phase_2_thermal_conductivity_name = ${k_d}
output_all_properties = true
# Friction model, not actually used!
use_dispersed_phase_drag_model = true
particle_diameter = ${dp}
add_advection_slip_term = false
[]
[]
[]
[]
[LinearFVBCs]
[botttom-phase-2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'bottom'
variable = phase_2
functor = '0'
[]
[top-phase-2]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top'
variable = phase_2
functor = '1'
[]
[]
[Executioner]
type = PIMPLE
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
dt = 1
end_time = 10
# Systems
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
active_scalar_systems = 'phi_system'
momentum_equation_relaxation = 0.8
active_scalar_equation_relaxation = '0.7'
pressure_variable_relaxation = 0.3
# We need to converge the problem to show conservation
num_iterations = 200
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
active_scalar_absolute_tolerance = '1e-10'
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'
active_scalar_petsc_options_iname = '-pc_type -pc_factor_shift_type' # -pc_hypre_type'
active_scalar_petsc_options_value = 'lu NONZERO'
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
active_scalar_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
active_scalar_l_tol = 0
# print_fields = true
continue_on_max_its = true
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.05 0.05 0.0'
[]
[Outputs]
exodus = true
[out]
type = CSV
execute_on = 'FINAL'
[]
[]
[AuxVariables]
[drag_coefficient]
type = MooseVariableFVReal
[]
[]
[AuxKernels]
[populate_cd]
type = FunctorAux
variable = drag_coefficient
functor = 'Darcy_coefficient'
execute_on = 'TIMESTEP_END'
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient]
type = ElementExtremeFunctorValue
functor = 'drag_coefficient'
value_type = max
[]
[]