- expressionExpression to parse for the new functor material
C++ Type:FunctionExpression
Unit:(no unit assumed)
Controllable:No
Description:Expression to parse for the new functor material
- property_nameName to give the new functor material property
C++ Type:std::string
Controllable:No
Description:Name to give the new functor material property
ParsedFunctorMaterial
This functor material computes a functor material property using a mathematical expression provided by a string. The expression may operate on any of the following values:
the spatial point, provided by
x,y, andz,the time, provided by
t, andany functor.
Usage
This functor material creates a functor material property with the name given by "property_name".
The mathematical expression is provided via "expression".
Functors used in this expression are provided via "functor_names". These functors can optionally be assigned alternate (usually simpler) names for use in the expression by providing "functor_symbols". Otherwise their names are used directly in the expression.
For more information on the mathematical operators that can be used in the expression, see the function parser site.
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
- declare_suffixAn optional suffix parameter that can be appended to any declared 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 declared properties. The suffix will be prepended with a '_' character.
- epsilon0Fuzzy comparison tolerance
Default:0
C++ Type:double
Unit:(no unit assumed)
Controllable:No
Description:Fuzzy comparison tolerance
- execute_onALWAYSThe 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:ALWAYS
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, ALWAYS
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.
- functor_namesFunctors to use in the parsed expression
C++ Type:std::vector<std::string>
Controllable:No
Description:Functors to use in the parsed expression
- functor_symbolsSymbolic name to use for each functor in 'functor_names' in the parsed expression. If not provided, then the actual functor names must be used in the parsed expression.
C++ Type:std::vector<std::string>
Controllable:No
Description:Symbolic name to use for each functor in 'functor_names' in the parsed expression. If not provided, then the actual functor names must be used in the parsed expression.
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.
- implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Controllable:No
Description:Determines whether this object is calculated using an implicit or explicit form
- search_methodnearest_node_connected_sidesChoice of search algorithm. All options begin by finding the nearest node in the primary boundary to a query point in the secondary boundary. In the default nearest_node_connected_sides algorithm, primary boundary elements are searched iff that nearest node is one of their nodes. This is fast to determine via a pregenerated node-to-elem map and is robust on conforming meshes. In the optional all_proximate_sides algorithm, primary boundary elements are searched iff they touch that nearest node, even if they are not topologically connected to it. This is more CPU-intensive but is necessary for robustness on any boundary surfaces which has disconnections (such as Flex IGA meshes) or non-conformity (such as hanging nodes in adaptively h-refined meshes).
Default:nearest_node_connected_sides
C++ Type:MooseEnum
Options:nearest_node_connected_sides, all_proximate_sides
Controllable:No
Description:Choice of search algorithm. All options begin by finding the nearest node in the primary boundary to a query point in the secondary boundary. In the default nearest_node_connected_sides algorithm, primary boundary elements are searched iff that nearest node is one of their nodes. This is fast to determine via a pregenerated node-to-elem map and is robust on conforming meshes. In the optional all_proximate_sides algorithm, primary boundary elements are searched iff they touch that nearest node, even if they are not topologically connected to it. This is more CPU-intensive but is necessary for robustness on any boundary surfaces which has disconnections (such as Flex IGA meshes) or non-conformity (such as hanging nodes in adaptively h-refined meshes).
- 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
Advanced Parameters
- disable_fpoptimizerFalseDisable the function parser algebraic optimizer
Default:False
C++ Type:bool
Controllable:No
Description:Disable the function parser algebraic optimizer
- enable_ad_cacheTrueEnable caching of function derivatives for faster startup time
Default:True
C++ Type:bool
Controllable:No
Description:Enable caching of function derivatives for faster startup time
- enable_auto_optimizeTrueEnable automatic immediate optimization of derivatives
Default:True
C++ Type:bool
Controllable:No
Description:Enable automatic immediate optimization of derivatives
- enable_jitTrueEnable just-in-time compilation of function expressions for faster evaluation
Default:True
C++ Type:bool
Controllable:No
Description:Enable just-in-time compilation of function expressions for faster evaluation
- evalerror_behaviornanWhat to do if evaluation error occurs. Options are to pass a nan, pass a nan with a warning, throw a error, or throw an exception
Default:nan
C++ Type:MooseEnum
Options:nan, nan_warning, error, exception
Controllable:No
Description:What to do if evaluation error occurs. Options are to pass a nan, pass a nan with a warning, throw a error, or throw an exception
Parsed Expression Advanced Parameters
- output_propertiesList of material properties, from this material, to output (outputs must also be defined to an output type)
C++ Type:std::vector<std::string>
Controllable:No
Description:List of material properties, from this material, to output (outputs must also be defined to an output type)
- outputsnone Vector of output names where you would like to restrict the output of variables(s) associated with this object
Default:none
C++ Type:std::vector<OutputName>
Controllable:No
Description:Vector of output names where you would like to restrict the output of variables(s) associated with this object
Outputs Parameters
Input Files
- (modules/navier_stokes/test/tests/finite_volume/ins/dittus-boelter/channel.i)
- (test/tests/functormaterials/functor_change/fp_child.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/materials/2d-steady-wall-balance.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp.i)
- (test/tests/functormaterials/functor_change/nonlinear.i)
- (test/tests/postprocessors/discrete_variable_residual_norm/part_fe.i)
- (test/tests/functors/scalar_variable/test.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/conjugate_heat_transfer/cht_neu-dir.i)
- (test/tests/executioners/nl_forced_its/nl_forced_its.i)
- (test/tests/outputs/csv/all_columns_parent.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/bulk_heat_transfer/flow-around-square-linear.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/lid-driven-two-phase.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/natural_convection/natural_circulation_pipe.i)
- (test/tests/kernels/functor_kernel/functor_kernel.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp-nonlinearFV.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/bulk_heat_transfer/flow-around-square-linear-fluidonly-physics.i)
- (test/tests/convergence/parent.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/turbulent_driven_growth.i)
- (test/tests/functormaterials/output/output.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/rayleigh-bernard-two-phase-physics_heated.i)
- (test/tests/outputs/csv/all_columns_child.i)
- (test/tests/functormaterials/output/output_ad.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/bulk_heat_transfer/flow-around-square-linear-fluidonly.i)
- (test/tests/functormaterials/functor_change/fp_parent.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/wcns/materials/1d_test_cpT.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/pressure_driven_growth.i)
- (test/tests/functormaterials/parsed_functor_material/parsed_functor_material.i)
- (test/tests/executioners/nl_divergence_tolerance/nl_divergence_tolerance.i)
- (test/tests/postprocessors/discrete_variable_residual_norm/part_fv.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h.i)
- (test/tests/postprocessors/side_integral/side_integral_functor_fe.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-energy.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/natural_convection/linear_segregated/2d/diff_heated_cavity_linear_buoyancy.i)
- (modules/navier_stokes/test/tests/finite_volume/ins/cht/conjugate_heat_transfer/cht_rob-rob.i)
- (modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-transient.i)
- (test/tests/executioners/nl_divergence_tolerance/nl_abs_divergence_tolerance.i)
- (modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/enthalpy_equation.i)
- (test/tests/convergence/default_steady_state_convergence/base.i)
- (test/tests/convergence/child.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/two_phase/mixture_model/segregated/channel-drift-flux.i)
property_name
C++ Type:std::string
Controllable:No
Description:Name to give the new functor material property
expression
C++ Type:FunctionExpression
Unit:(no unit assumed)
Controllable:No
Description:Expression to parse for the new functor material
functor_names
C++ Type:std::vector<std::string>
Controllable:No
Description:Functors to use in the parsed expression
functor_symbols
C++ Type:std::vector<std::string>
Controllable:No
Description:Symbolic name to use for each functor in 'functor_names' in the parsed expression. If not provided, then the actual functor names must be used in the parsed expression.
(modules/navier_stokes/test/tests/finite_volume/ins/dittus-boelter/channel.i)
# Waterish Fluid properties
mu = 1.79e-3
rho = 1e3
cp = 4.186e3
k = .561
D_h = .05
num_axial_elements = 50
num_radial_elements = 10
h = '${fparse D_h/2/num_radial_elements}'
# Operating conditions
u_inlet = 1
T_inlet = 300
T_wall = 350
p_outlet = 0
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse h * num_axial_elements}'
ymin = 0
ymax = '${fparse h * num_radial_elements}'
nx = ${num_axial_elements}
ny = ${num_radial_elements}
[]
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'incompressible'
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '${u_inlet} 0 0'
initial_pressure = 0.0
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_functors = '${u_inlet} 0'
wall_boundaries = 'bottom top'
momentum_wall_types = 'symmetry slip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure-zero-gradient'
pressure_functors = '${p_outlet}'
mass_advection_interpolation = 'average'
momentum_advection_interpolation = 'average'
[]
[]
[FluidHeatTransfer]
[heat]
thermal_conductivity = 'k'
specific_heat = 'cp'
fluid_temperature_variable = 'T_fluid'
initial_temperature = '${T_inlet}'
energy_inlet_types = 'FIXED-TEMPERATURE'
energy_inlet_functors = '${T_inlet}'
energy_wall_types = 'heatflux heatflux'
energy_wall_functors = '0 q'
energy_advection_interpolation = 'average'
[]
[]
[]
[]
[FluidProperties]
[simple]
type = SimpleFluidProperties
thermal_conductivity = ${k}
cp = ${cp}
viscosity = ${mu}
density0 = ${rho}
[]
[]
[UserObjects]
[layered_speed]
execute_on = 'linear nonlinear'
type = LayeredAverageFunctor
direction = 'x'
functor = 'speed'
num_layers = ${num_axial_elements}
[]
[layered_T_fluid]
execute_on = 'linear nonlinear'
type = LayeredAverageFunctor
direction = 'x'
num_layers = ${num_axial_elements}
functor = 'T_fluid'
[]
[]
[FunctorMaterials]
[converter]
type = FunctorADConverter
ad_props_in = 'pressure'
reg_props_out = 'nonad_pressure'
[]
[functor_props]
type = NonADGeneralFunctorFluidProps
T_fluid = layered_T_fluid
characteristic_length = ${D_h}
fp = simple
porosity = 1
pressure = nonad_pressure
speed = layered_speed
[]
[dittus]
type = DittusBoelterFunctorMaterial
D_h = ${D_h}
Hw = Hw
Pr = Pr
Re = Re
T_fluid = layered_T_fluid
T_wall = ${T_wall}
k = k
[]
[q]
type = ParsedFunctorMaterial
expression = 'Hw * (T_wall - T_fluid)'
functor_symbols = 'Hw T_fluid T_wall'
functor_names = 'Hw layered_T_fluid ${T_wall}'
property_name = 'q'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
line_search = 'none'
[]
[Outputs]
exodus = true
[]
(test/tests/functormaterials/functor_change/fp_child.i)
# Solves the nonlinear equation
# S(T) = B - A * (T - T_inf)^2
# on each node.
T_ambient = 300.0
source_coef_A = 0.1
source_coef_B = 1e4
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[S]
[]
[]
[AuxVariables]
[T_child]
[]
[]
[FunctorMaterials]
[equation_mat]
type = ADParsedFunctorMaterial
expression = 'B - A * (T - T_inf)^2 - S'
functor_symbols = 'T T_inf A B S'
functor_names = 'T_child ${T_ambient} ${source_coef_A} ${source_coef_B} S'
property_name = 'equation'
[]
[]
[Kernels]
[equation_kernel]
type = FunctorKernel
variable = S
functor = equation
functor_on_rhs = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_max_its = 10
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
l_tol = 1e-3
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/materials/2d-steady-wall-balance.i)
L = 30
bulk_u = 0.01
p_ref = 101325.0
T_in = 860
q_source = 50000
q2_wall = 10000
A_cp = 976.78
B_cp = 1.0634
rho = 2000
advected_interp_method = 'upwind'
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${L}
ymin = 1
ymax = 2.5
nx = 10
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = ${bulk_u}
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
initial_condition = ${p_ref}
two_term_boundary_expansion = false
[]
[T]
type = INSFVEnergyVariable
two_term_boundary_expansion = false
initial_condition = ${T_in}
[]
[]
[FVKernels]
[mass]
type = WCNSFVMassAdvection
variable = pressure
rho = 'rho'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = 'rho'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = 'rho'
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu'
momentum_component = 'y'
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
[]
[source]
type = FVBodyForce
variable = T
function = source_func
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u}
[]
[inlet-v]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_y
functor = 0
[]
[inlet_T]
type = FVDirichletBC
variable = T
boundary = 'left'
value = ${T_in}
[]
[incoming_heat]
type = FVNeumannBC
variable = T
value = ${q2_wall}
boundary = 'top'
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = ${p_ref}
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = '${q_source}'
[]
[]
[FunctorMaterials]
[converter_to_regular_T]
type = FunctorADConverter
ad_props_in = 'T'
reg_props_out = 'T_nAD'
[]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T'
rho = 'rho'
cp = 'cp'
assumed_constant_cp = false
h_in = 'h'
# fp = 'fp'
# pressure = 'pressure'
[]
[rho]
type = ADParsedFunctorMaterial
property_name = 'rho'
expression = '${rho}'
[]
[mu]
type = ADParsedFunctorMaterial
property_name = 'mu'
expression = '4.5e-3'
[]
[k]
type = ADParsedFunctorMaterial
property_name = 'k'
expression = '0.7'
[]
[h]
type = ADParsedFunctorMaterial
property_name = 'h'
functor_names = 'T ${A_cp} ${B_cp}'
functor_symbols = 'T A_cp B_cp'
expression = 'A_cp * T + B_cp * T * T / 2'
[]
[cp]
type = ADParsedFunctorMaterial
property_name = 'cp'
functor_names = 'T ${A_cp} ${B_cp}'
functor_symbols = 'T A_cp B_cp'
expression = 'A_cp+B_cp*T'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_abs_tol = 1e-9
nl_max_its = 50
line_search = 'none'
automatic_scaling = true
off_diagonals_in_auto_scaling = true
[]
[Postprocessors]
[H_in]
type = VolumetricFlowRate
vel_x = 'vel_x'
advected_quantity = 'rho_h'
boundary = 'left'
[]
[H_out]
type = VolumetricFlowRate
vel_x = 'vel_x'
advected_quantity = 'rho_h'
boundary = 'right'
[]
[Q]
type = FunctionElementIntegral
function = 'source_func'
execute_on = 'initial'
[]
[Q_wall]
type = FunctionSideIntegral
function = ${q2_wall}
boundary = 'top'
[]
[balance_in_percent]
type = ParsedPostprocessor
expression = '(H_out + H_in - Q - Q_wall) / H_in * 100'
pp_names = 'H_in H_out Q Q_wall'
[]
[]
[Outputs]
csv = true
[]
(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
[]
[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
[]
[]
(test/tests/functormaterials/functor_change/nonlinear.i)
# Solves the equation
#
# U^2 = C
# U(0) = U0
C = 25.0
U0 = 1.0
[Mesh]
type = GeneratedMesh
dim = 1
nx = 1
[]
[Variables]
[U]
initial_condition = ${U0}
[]
[]
[FunctorMaterials]
[residual_fmat]
type = ADParsedFunctorMaterial
expression = 'U^2 - C'
functor_symbols = 'U C'
functor_names = 'U ${C}'
property_name = residual_prop
[]
[]
[Kernels]
[residual]
type = FunctorKernel
variable = U
functor = residual_prop
functor_on_rhs = false
[]
[]
[FunctorMaterials]
[mat]
type = ADFunctorChangeFunctorMaterial
functor = U
change_over = nonlinear
take_absolute_value = false
prop_name = U_change
[]
[]
[Postprocessors]
[U_avg]
type = AverageNodalVariableValue
variable = U
execute_on = 'NONLINEAR_CONVERGENCE'
[]
[U_max_change]
type = ElementExtremeFunctorValue
functor = U_change
value_type = max
execute_on = 'NONLINEAR_CONVERGENCE'
[]
[]
[Convergence]
[nl_conv]
type = IterationCountConvergence
max_iterations = 2
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
line_search = none
nonlinear_convergence = nl_conv
[]
[Outputs]
[console]
type = Console
execute_postprocessors_on = 'NONLINEAR'
[]
[csv]
type = CSV
file_base = nonlinear
execute_on = 'NONLINEAR'
[]
[]
(test/tests/postprocessors/discrete_variable_residual_norm/part_fe.i)
[Variables]
[T_fe]
[]
[]
[FunctorMaterials]
[heat_flux_mat_nodal]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T_fe ${T_ambient} ${htc}'
property_name = 'heat_flux_nodal'
[]
[source_mat_nodal]
type = ADParsedFunctorMaterial
expression = 'B - A * (T - T_inf)^2'
functor_symbols = 'A B T T_inf'
functor_names = '${source_coef_A} ${source_coef_B} T_fe ${T_ambient}'
property_name = 'source_nodal'
[]
[]
[Kernels]
[T_fe_diff]
type = FunctionDiffusion
variable = T_fe
function = ${k}
[]
[T_fe_source]
type = FunctorKernel
variable = T_fe
functor = source_nodal
functor_on_rhs = true
[]
[]
[BCs]
[left_bc_nodal]
type = DirichletBC
variable = T_fe
boundary = left
value = ${T_ambient}
[]
[right_bc_nodal]
type = FunctorNeumannBC
variable = T_fe
boundary = right
functor = heat_flux_nodal
flux_is_inward = false
[]
[]
[Postprocessors]
# l-1
[fe_A_l1]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockA'
norm_type = l_1
execute_on = 'FINAL'
[]
[fe_A_l1_nobias]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockA'
norm_type = l_1
correct_mesh_bias = true
execute_on = 'FINAL'
[]
[fe_B_l1]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockB'
norm_type = l_1
execute_on = 'FINAL'
[]
# l-2
[fe_A_l2]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockA'
norm_type = l_2
execute_on = 'FINAL'
[]
[fe_A_l2_nobias]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockA'
norm_type = l_2
correct_mesh_bias = true
execute_on = 'FINAL'
[]
[fe_B_l2]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockB'
norm_type = l_2
execute_on = 'FINAL'
[]
# l-infinity
[fe_A_linf]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockA'
norm_type = l_inf
execute_on = 'FINAL'
[]
[fe_A_linf_nobias]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockA'
norm_type = l_inf
correct_mesh_bias = true
execute_on = 'FINAL'
[]
[fe_B_linf]
type = DiscreteVariableResidualNorm
variable = T_fe
block = 'blockB'
norm_type = l_inf
execute_on = 'FINAL'
[]
[]
(test/tests/functors/scalar_variable/test.i)
# Domain on (0,1) with 1 element
#
# du/dt = v, u(0) = 0
# dv/dt = 1, v(0) = 0
#
# Taking 3 time steps of 1 second each. Values should be the following:
#
# t = 0: u = 0, v = 0
# t = 1: u = 1, v = 1
# t = 2: u = 3, v = 2
# t = 3: u = 6, v = 3
u0 = 0
v0 = 0
v_source = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 1
nx = 1
xmin = 0
xmax = 1
[]
[]
[Variables]
[u]
family = LAGRANGE
order = FIRST
initial_condition = ${u0}
[]
[v]
family = SCALAR
order = FIRST
initial_condition = ${v0}
[]
[]
[Kernels]
[time_deriv_u]
type = ADTimeDerivative
variable = u
[]
[source_u]
type = FunctorKernel
variable = u
functor = source_u
functor_on_rhs = true
[]
[]
[FunctorMaterials]
[u_source_mat]
type = ADParsedFunctorMaterial
expression = 'v'
functor_names = 'v'
property_name = source_u
[]
[]
[ScalarKernels]
[time_deriv_v]
type = ADScalarTimeDerivative
variable = v
[]
[source_v]
type = ParsedODEKernel
variable = v
expression = '-${v_source}'
[]
[]
[Postprocessors]
[u_avg]
type = ElementAverageValue
variable = u
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Executioner]
type = Transient
dt = 1
num_steps = 3
solve_type = NEWTON
[]
[Outputs]
csv = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/conjugate_heat_transfer/cht_neu-dir.i)
### benchmark sources:
### https://doi.org/10.1016/j.compfluid.2018.06.016
### https://doi.org/10.1016/0017-9310(74)90087-8
b = 0.01 # plate thickness
l = 0.2 # plate length
nxi = 24 # nx in the inlet/entrance region
nyf = 18 # ny in fluid
nxf = 24 # nx in the main fluid region
nys = 8 # ny in the solid domain
fx1_bias = 1.00 # bdry layer bias - fluid
fx2_bias = '${fparse 1.0/1.00}' # bdry layer bias - solid
fy_bias = 1.20 # bdry layer bias - fluid
sy_bias = '${fparse 1.0/1.05}' # bdry layer bias - solid
k_s = 0.2876
rho = 0.3525
mu = 3.95e-5
k = 0.06808
cp = 1142.6
vin = 12.0
Tin = 1000.0
T_s_bottom = 600.0
P_out = 1.03e5
h_s = 0.0
advected_interp_method = 'upwind'
[Mesh]
[fluid_channel]
type = GeneratedMeshGenerator
dim = 2
nx = ${nxf}
ny = ${nyf}
xmin = 0
xmax = ${l}
ymin = 0
ymax = '${fparse 10.0*b}'
subdomain_ids = '1'
subdomain_name = 'fluid'
bias_x = '${fx1_bias}'
bias_y = '${fparse fy_bias}'
boundary_name_prefix = 'fluid'
[]
[solid_base]
type = GeneratedMeshGenerator
dim = 2
nx = ${nxf}
ny = ${nys}
xmin = 0
xmax = ${l}
ymin = '${fparse -b}'
ymax = 0
subdomain_ids = '2'
subdomain_name = 'solid'
bias_x = ${fx1_bias}
bias_y = '${fparse sy_bias}'
boundary_id_offset = 10
boundary_name_prefix = 'solid'
[]
[entrance]
type = GeneratedMeshGenerator
dim = 2
nx = '${fparse 2.0*nxi}'
ny = ${nyf}
xmin = '${fparse -2.0*l}'
xmax = 0
ymin = 0
ymax = '${fparse 10.0*b}'
subdomain_ids = '0'
subdomain_name = 'entrance'
bias_x = ${fx2_bias}
bias_y = '${fparse fy_bias}'
boundary_id_offset = 20
boundary_name_prefix = 'ent'
[]
[smg]
type = StitchedMeshGenerator
inputs = 'entrance fluid_channel solid_base'
stitch_boundaries_pairs = 'ent_right fluid_left;
fluid_bottom solid_top'
prevent_boundary_ids_overlap = false
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = 'smg'
primary_block = 'fluid'
paired_block = 'solid'
new_boundary = interface
[]
[symmetry_transform]
type = SymmetryTransformGenerator
input = interface
mirror_point = '0 0 0'
mirror_normal_vector = '0 1 0'
[]
inactive = 'symmetry_transform'
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system solid_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
block = '0 1'
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = ${vin}
solver_sys = u_system
block = '0 1'
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
block = '0 1'
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${P_out}
block = '0 1'
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = ${Tin}
block = '0 1'
[]
[T_solid]
type = MooseLinearVariableFVReal
solver_sys = solid_energy_system
initial_condition = ${T_s_bottom}
block = 2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[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
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = false
[]
[solid-conduction]
type = LinearFVDiffusion
variable = T_solid
diffusion_coeff = ${k_s}
use_nonorthogonal_correction = false
[]
[]
[LinearFVBCs]
# velocity BCs
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_left'
variable = vel_x
functor = ${vin}
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_left'
variable = vel_y
functor = '0.000'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_bottom interface'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_bottom interface'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'fluid_right'
variable = pressure
functor = ${P_out}
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_right'
variable = vel_x
use_two_term_expansion = false
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_right'
variable = vel_y
use_two_term_expansion = false
[]
# freestream BCs for top of fluid domain
[freestream_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_top ent_top'
variable = vel_x
use_two_term_expansion = false
[]
[freestream_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_top ent_top'
variable = vel_y
use_two_term_expansion = false
[]
[freestream_p]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
boundary = 'fluid_top ent_top'
variable = pressure
functor = 0
[]
# temperature BCs
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = ${Tin}
boundary = 'ent_left'
[]
[heated_wall_solid]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_solid
functor = ${T_s_bottom}
boundary = 'solid_bottom'
[]
[insulated_fluid]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
functor = 0
boundary = 'ent_bottom ent_top fluid_top'
[]
[insulated_solid]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_solid
functor = 0
boundary = 'solid_left solid_right'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = 'fluid_right'
[]
[fluid_solid]
type = LinearFVDirichletCHTBC
variable = T_fluid
boundary = interface
functor = interface_temperature_solid_interface
[]
[solid_fluid]
type = LinearFVRobinCHTBC
variable = T_solid
boundary = interface
h = ${h_s}
thermal_conductivity = ${k_s}
incoming_flux = heat_flux_to_solid_interface
surface_temperature = interface_temperature_fluid_interface
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[]
[Postprocessors]
[h_in]
type = VolumetricFlowRate
boundary = 'ent_left'
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
subtract_mesh_velocity = false
[]
[h_out]
type = VolumetricFlowRate
boundary = 'fluid_right fluid_top ent_top interface'
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
advected_interp_method = upwind
subtract_mesh_velocity = false
[]
[]
[VectorPostprocessors]
[y_vs_ts]
type = LineValueSampler
variable = 'T_solid'
start_point = '0.05 -1e-9 0' # making sure we are always in the domain
end_point = '0.05 ${fparse -b+1e-9} 0'
num_points = 8
sort_by = id
warn_discontinuous_face_values = false
[]
[y_vs_tf]
type = LineValueSampler
variable = 'T_fluid'
start_point = '0.05 1e-9 0' # making sure we are always in the domain
end_point = '0.05 ${fparse b-1e-9} 0'
num_points = 12
sort_by = id
warn_discontinuous_face_values = false
[]
[]
[Executioner]
type = SIMPLE
num_iterations = 1000
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
rhie_chow_user_object = 'rc'
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
momentum_equation_relaxation = 0.9
pressure_variable_relaxation = 0.3
momentum_absolute_tolerance = 1e-7
pressure_absolute_tolerance = 1e-7
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_system = 'energy_system'
solid_energy_system = 'solid_energy_system'
energy_l_abs_tol = 1e-10
solid_energy_l_abs_tol = 1e-10
energy_l_tol = 0
solid_energy_l_tol = 0
energy_equation_relaxation = 1.0
energy_absolute_tolerance = 1e-7
solid_energy_absolute_tolerance = 1e-7
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
solid_energy_petsc_options_iname = '-pc_type -pc_hypre_type'
solid_energy_petsc_options_value = 'hypre boomeramg'
cht_interfaces = 'interface'
cht_solid_flux_relaxation = 0.4
cht_fluid_flux_relaxation = 0.4
cht_solid_temperature_relaxation = 0.4
cht_fluid_temperature_relaxation = 0.4
max_cht_fpi = 3
print_fields = false
[]
[Outputs]
csv = true
execute_on = timestep_end
[]
(test/tests/executioners/nl_forced_its/nl_forced_its.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[./u]
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[force]
type = FVCoupledForce
v = v
variable = u
[]
[]
[FunctorMaterials]
[parsed]
type = ADParsedFunctorMaterial
property_name = 'v'
functor_names = 'u'
expression = 'if(u>0.1,1e6,0)'
[]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
line_search = 'none'
solve_type = NEWTON
nl_max_its = 5
nl_forced_its = 3
nl_abs_div_tol = 1e+3
petsc_options = '-snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(test/tests/outputs/csv/all_columns_parent.i)
# Heat conduction with fixed temperature on left and convection BC on right:
#
# d/dx(-k dT/dx) = S'''(T) (0,1)X(0,1)
# T = T_inf x = 0
# -k dT/dx = htc (T - T_inf) x = 1
#
# Source is temperature-dependent and is calculated in the child app:
# S(T) = B - A * (T - T_inf)^2
k = 15.0
htc = 100.0
T_ambient = 300.0
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[T]
[]
[]
[AuxVariables]
[S_parent]
[]
[Tavg_scalar]
family = SCALAR
order = FIRST
[]
[]
[Functions]
[Tavg_scalar_fn]
type = PostprocessorFunction
pp = Tavg_pp
[]
[]
[AuxScalarKernels]
[Tavg_scalar_kernel]
type = FunctionScalarAux
variable = Tavg_scalar
function = Tavg_scalar_fn
execute_on = 'TIMESTEP_END'
[]
[]
[FunctorMaterials]
[heat_flux_mat]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T ${T_ambient} ${htc}'
property_name = 'heat_flux'
[]
[]
[Kernels]
[diff]
type = FunctionDiffusion
variable = T
function = ${k}
[]
[source]
type = CoupledForce
variable = T
v = S_parent
[]
[]
[BCs]
[left_bc]
type = DirichletBC
variable = T
boundary = left
value = ${T_ambient}
[]
[right_bc]
type = FunctorNeumannBC
variable = T
boundary = right
functor = heat_flux
flux_is_inward = false
[]
[]
[Convergence]
[fp_conv]
type = IterationCountConvergence
max_iterations = 3
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
multiapp_fixed_point_convergence = fp_conv
[]
[MultiApps]
[source_app]
type = FullSolveMultiApp
positions = '0 0 0'
input_files = all_columns_child.i
execute_on = 'TIMESTEP_END'
[]
[]
[Transfers]
[T_to_child]
type = MultiAppCopyTransfer
to_multi_app = source_app
source_variable = T
variable = T_child
execute_on = 'SAME_AS_MULTIAPP'
[]
[S_from_child]
type = MultiAppCopyTransfer
from_multi_app = source_app
source_variable = S
variable = S_parent
execute_on = 'SAME_AS_MULTIAPP'
[]
[]
[Postprocessors]
[Tavg_pp]
type = AverageNodalVariableValue
variable = T
execute_on = 'TIMESTEP_END'
[]
[fp_it]
type = NumFixedPointIterations
get_index_instead_of_count = true
execute_on = 'TIMESTEP_END'
[]
[]
[Outputs]
[console]
type = Console
new_row_detection_columns = ALL
execute_postprocessors_on = 'MULTIAPP_FIXED_POINT_ITERATION_END'
execute_scalars_on = 'MULTIAPP_FIXED_POINT_ITERATION_END'
execute_on = 'MULTIAPP_FIXED_POINT_ITERATION_END'
[]
[out]
type = CSV
new_row_detection_columns = ALL
execute_postprocessors_on = 'MULTIAPP_FIXED_POINT_ITERATION_END'
execute_scalars_on = 'MULTIAPP_FIXED_POINT_ITERATION_END'
execute_on = 'MULTIAPP_FIXED_POINT_ITERATION_END'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/bulk_heat_transfer/flow-around-square-linear.i)
mu = 0.01
rho = 1.1
k = 0.0005
cp = 10
k_s = 3.0
h_conv = 5
power_density = 10000
advected_interp_method = 'upwind'
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmin = 0
ymin = 0
ymax = 0.1
xmax = 0.1
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = generated_mesh
block_name = subdomain1
bottom_left = '0.04 0.04 0'
block_id = 1
top_right = '0.06 0.06 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = 0
paired_block = 1
new_boundary = interface
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system solid_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
block = 0
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.1
solver_sys = u_system
block = 0
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.01
block = 0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
block = 0
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
block = 0
[]
[T_solid]
type = MooseLinearVariableFVReal
solver_sys = solid_energy_system
initial_condition = 500
block = 1
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = true
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = true
[]
[solid-conduction]
type = LinearFVDiffusion
variable = T_solid
diffusion_coeff = ${k_s}
use_nonorthogonal_correction = true
[]
[solid-source]
type = LinearFVSource
variable = T_solid
source_density = ${power_density}
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '0.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[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
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = 300
boundary = 'left'
[]
[walls_T]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
functor = 0.0
boundary = 'top bottom'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = right
[]
[fluid_solid]
type = LinearFVConvectiveHeatTransferBC
variable = T_fluid
T_solid = T_solid
T_fluid = T_fluid
boundary = interface
h = ${h_conv}
[]
[solid_fluid]
type = LinearFVConvectiveHeatTransferBC
variable = T_solid
T_solid = T_solid
T_fluid = T_fluid
boundary = interface
h = ${h_conv}
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[]
[Postprocessors]
[h_in]
type = VolumetricFlowRate
boundary = left
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
subtract_mesh_velocity = false
[]
[h_out]
type = VolumetricFlowRate
boundary = right
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
advected_interp_method = upwind
subtract_mesh_velocity = false
[]
[power]
type = ElementIntegralFunctorPostprocessor
functor = ${power_density}
block = 1
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
energy_l_abs_tol = 1e-13
solid_energy_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
energy_l_tol = 0
solid_energy_l_tol = 0
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
solid_energy_system = 'solid_energy_system'
momentum_equation_relaxation = 0.8
energy_equation_relaxation = 1.0
pressure_variable_relaxation = 0.3
num_iterations = 1000
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_absolute_tolerance = 1e-10
solid_energy_absolute_tolerance = 1e-10
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
solid_energy_petsc_options_iname = '-pc_type -pc_hypre_type'
solid_energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${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
[]
[]
(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} ${mu}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Postprocessors]
[average_void]
type = ElementAverageValue
variable = 'phase_2'
[]
[max_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = max
[]
[min_y_velocity]
type = ElementExtremeValue
variable = 'vel_y'
value_type = min
[]
[max_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = max
[]
[min_x_velocity]
type = ElementExtremeValue
variable = 'vel_x'
value_type = min
[]
[max_x_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_x'
value_type = max
[]
[max_y_slip_velocity]
type = ElementExtremeFunctorValue
functor = 'vel_slip_y'
value_type = max
[]
[max_drag_coefficient]
type = ElementExtremeFunctorValue
functor = 'drag_coefficient'
value_type = max
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 7
iteration_window = 2
growth_factor = 2.0
cutback_factor = 0.5
dt = 1e-3
[]
nl_max_its = 20
nl_rel_tol = 1e-03
nl_abs_tol = 1e-9
l_max_its = 5
end_time = 1e8
line_search=none
[]
[Outputs]
exodus = false
[CSV]
type = CSV
execute_on = 'FINAL'
execute_scalars_on = NONE
[]
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/natural_convection/natural_circulation_pipe.i)
# natural convection through a pipe
# Reference solution in "reference_pipe_natural_convection.py"
# Reference mdot: 0.0792 kg/s
# this input
# iy mdot
# 10 8.302364e-02
# 20 8.111192e-02
# 40 8.007924e-02
# 80 7.954403e-02
# 160 7.927201e-02
# Convergence to the analytical result is observed
height = 10.0
gravity = 9.81
p0 = 1e5
molar_mass = 29.0e-3
T0 = 328
Ru = 8.3145
Ri = '${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 = ${T0}
inlet_boundaries = 'bottom'
momentum_inlet_types = 'fixed-pressure'
momentum_inlet_functors = '${fparse p0 + head}'
energy_inlet_types = 'fixed-temperature'
energy_inlet_functors = '${T0}'
energy_scaling = 1e-5
wall_boundaries = 'left right'
momentum_wall_types = 'slip slip'
energy_wall_types = 'heatflux heatflux'
energy_wall_functors = '300 300'
outlet_boundaries = 'top'
momentum_outlet_types = 'fixed-pressure'
pressure_functors = '${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
[]
(test/tests/kernels/functor_kernel/functor_kernel.i)
# Heat conduction with fixed temperature on left and convection BC on right.
# Source is temperature-dependent:
# S(T) = B - A * (T - T_inf)^2 [W]
# S'''(T) = B/V - A/V * (T - T_inf)^2 [W/m^3]
# Assume volume V = 1 m^3, so
# S'''(T) = B - A * (T - T_inf)^2 [W/m^3]
k = 15.0
htc = 100.0
T_ambient = 300.0
source_coef_A = 0.1
source_coef_B = 1e4
[Mesh]
type = GeneratedMesh
dim = 1
nx = 10
[]
[Variables]
[T]
[]
[]
[FunctorMaterials]
[source_mat]
type = ADParsedFunctorMaterial
expression = 'B - A * (T - T_inf)^2'
functor_symbols = 'T T_inf A B'
functor_names = 'T ${T_ambient} ${source_coef_A} ${source_coef_B}'
property_name = 'source_term'
[]
[heat_flux_mat]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T ${T_ambient} ${htc}'
property_name = 'heat_flux'
[]
[]
[Kernels]
[diff]
type = FunctionDiffusion
variable = T
function = ${k}
[]
[source]
type = FunctorKernel
variable = T
functor = source_term
functor_on_rhs = true
[]
[]
[BCs]
[left_bc]
type = DirichletBC
variable = T
boundary = left
value = ${T_ambient}
[]
[right_bc]
type = FunctorNeumannBC
variable = T
boundary = right
functor = heat_flux
flux_is_inward = false
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_max_its = 10
l_tol = 1e-3
[]
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/enthalpy_equation/1d_test_h_fp-nonlinearFV.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 = ${nx}
[]
[]
[Physics]
[NavierStokes]
[Flow]
[flow]
compressibility = 'weakly-compressible'
velocity_variable = 'vel_x'
density = 'rho'
dynamic_viscosity = 'mu'
initial_velocity = '${bulk_u} 0 0'
initial_pressure = '${p_ref}'
inlet_boundaries = 'left'
# momentum_inlet_types = 'fixed-velocity'
# momentum_inlet_functors = '${bulk_u} 0'
momentum_inlet_types = 'flux-velocity'
flux_inlet_pps = '${bulk_u}'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_functors = '${p_ref}'
momentum_advection_interpolation = ${advected_interp_method}
pressure_two_term_bc_expansion = false
momentum_two_term_bc_expansion = false
[]
[]
[FluidHeatTransfer]
[energy]
coupled_flow_physics = flow
solve_for_enthalpy = true
# There is no fluid temperature (auxiliary) variable when solving for enthalpy
# with nonlinear finite volume, because we need T_from_p_h to be computed on-the-fly
# rather than on an auxiliary kernel update which does not preserve automatic differentiation
# fluid_temperature_variable = 'T_fluid'
fp = 'lead'
thermal_conductivity = 'k'
specific_heat = 'cp'
initial_enthalpy = '${fparse 800 * 240}'
energy_inlet_types = 'flux-velocity'
# specifies inlet temperature, not inlet enthalpy
energy_inlet_functors = '${T_in}'
# Source term
external_heat_source = source_func
# Numerical scheme
energy_advection_interpolation = ${advected_interp_method}
energy_two_term_bc_expansion = true
[]
[]
[]
[]
[FluidProperties]
[lead]
type = LeadFluidProperties
[]
[]
[FunctorMaterials]
[fluid_props_to_mat_props]
type = GeneralFunctorFluidProps
fp = lead
pressure = ${p_ref}
T_fluid = 'T_fluid'
speed = 1
porosity = 1
characteristic_length = 1
[]
[source_func]
type = ADParsedFunctorMaterial
property_name = source_func
functor_names = 'rho'
expression = ${q_source}
[]
[]
[AuxVariables]
[T_out]
type = MooseVariableFVReal
[AuxKernel]
type = FunctorAux
functor = 'T_fluid'
[]
[]
[]
[Postprocessors]
[T_out_sim]
type = PointValue
variable = T_out
point = '${fparse L * (nx-0.5)/ nx} 0 0'
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[Outputs]
[out]
type = CSV
hide = 'area_pp_left'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/bulk_heat_transfer/flow-around-square-linear-fluidonly-physics.i)
mu = 0.01
rho = 1.1
k = 0.0005
cp = 10
h_conv = 5
inlet_temp = 300
advected_interp_method = 'upwind'
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmin = 0
ymin = 0
ymax = 0.1
xmax = 0.1
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = generated_mesh
block_name = subdomain1
bottom_left = '0.04 0.04 0'
block_id = 1
top_right = '0.06 0.06 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = 0
paired_block = 1
new_boundary = interface
[]
[delete]
type = BlockDeletionGenerator
input = interface
block = 1
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
[Physics]
[NavierStokes]
[FlowSegregated]
[flow]
compressibility = 'weakly-compressible'
block = '0'
velocity_variable = 'vel_x vel_y'
density = ${rho}
dynamic_viscosity = ${mu}
initial_velocity = '0.1 0.01 0'
initial_pressure = '0.2'
inlet_boundaries = 'left'
momentum_inlet_types = 'fixed-velocity'
momentum_inlet_functors = '0.1 0'
wall_boundaries = 'top bottom interface'
momentum_wall_types = 'noslip noslip noslip'
outlet_boundaries = 'right'
momentum_outlet_types = 'fixed-pressure'
pressure_functors = '1.4'
momentum_advection_interpolation = ${advected_interp_method}
momentum_two_term_bc_expansion = false
pressure_two_term_bc_expansion = false
orthogonality_correction = false
[]
[]
[FluidHeatTransferSegregated]
[energy]
coupled_flow_physics = flow
block = '0'
thermal_conductivity = '${k}'
specific_heat = '${cp}'
initial_temperature = '${inlet_temp}'
energy_inlet_types = 'fixed-temperature'
energy_inlet_functors = '${inlet_temp}'
energy_wall_types = 'heatflux heatflux convection'
energy_wall_functors = '0 0 boundary_value:htc'
energy_advection_interpolation = ${advected_interp_method}
energy_two_term_bc_expansion = false
[]
[]
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[conv_data]
type = GenericFunctorMaterial
prop_names = 'htc boundary_value'
prop_values = '${h_conv} 350'
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
energy_l_abs_tol = 1e-13
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 = 0.8
energy_equation_relaxation = 1.0
pressure_variable_relaxation = 0.3
num_iterations = 1000
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/convergence/parent.i)
# Heat conduction with fixed temperature on left and convection BC on right:
#
# d/dx(-k dT/dx) = S'''(T) (0,1)X(0,1)
# T = T_inf x = 0
# -k dT/dx = htc (T - T_inf) x = 1
#
# Source is temperature-dependent and is calculated in the child app:
# S(T) = B - A * (T - T_inf)^2
k = 15.0
htc = 100.0
T_ambient = 300.0
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[T]
[]
[]
[AuxVariables]
[S_parent]
[]
[]
[FunctorMaterials]
[heat_flux_mat]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T ${T_ambient} ${htc}'
property_name = 'heat_flux'
[]
[]
[Kernels]
[diff]
type = FunctionDiffusion
variable = T
function = ${k}
[]
[source]
type = CoupledForce
variable = T
v = S_parent
[]
[]
[BCs]
[left_bc]
type = DirichletBC
variable = T
boundary = left
value = ${T_ambient}
[]
[right_bc]
type = FunctorNeumannBC
variable = T
boundary = right
functor = heat_flux
flux_is_inward = false
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
multiapp_fixed_point_convergence = fp_conv
[]
[MultiApps]
[source_app]
type = FullSolveMultiApp
positions = '0 0 0'
input_files = child.i
execute_on = 'TIMESTEP_END'
[]
[]
[Transfers]
[T_to_child]
type = MultiAppCopyTransfer
to_multi_app = source_app
source_variable = T
variable = T_child
execute_on = 'SAME_AS_MULTIAPP'
[]
[S_from_child]
type = MultiAppCopyTransfer
from_multi_app = source_app
source_variable = S
variable = S_parent
execute_on = 'SAME_AS_MULTIAPP'
[]
[]
[Postprocessors]
[n_fp_its]
type = NumFixedPointIterations
execute_on = 'TIMESTEP_END'
[]
[]
[Outputs]
csv = true
execute_on = 'FINAL'
[]
(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} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(test/tests/functormaterials/output/output.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 1
xmin = 0.0
xmax = 4.0
ymin = 0.0
ymax = 6.0
[]
[FunctorMaterials]
[parsed_fmat]
type = ParsedFunctorMaterial
expression = 't + x + y + z'
property_name = 'prop1'
outputs = 'exodus'
output_properties = 'prop1'
[]
[parsed_vector_fmat]
type = GenericVectorFunctorMaterial
prop_names = 'prop1_vec'
prop_values = '1 2 3'
outputs = 'exodus'
output_properties = 'prop1_vec'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
# Get the t to be equal to 4
time = 4.0
[]
[Outputs]
exodus = true
execute_on = 'INITIAL'
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/rayleigh-bernard-two-phase-physics_heated.i)
mu = 1.0
rho = 1e3
mu_d = 0.3
rho_d = 1.0
dp = 0.01
U_lid = 0.0
g = -9.81
advected_interp_method = 'upwind'
T_fluid_top = 1
# Currently required
k = 1
k_d = 1
cp = 1
cp_d = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = .1
ymin = 0
ymax = .1
nx = 10
ny = 11
[]
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system phi_system'
[]
# We are using a Materials block to order the functor creation.
# See #30827
[Materials]
[T_from_p_h]
type = ParsedFunctorMaterial
property_name = 'T_from_p_h_functor'
expression = 'h / cp_mixture'
functor_names = 'h cp_mixture'
[]
[h_from_p_T]
type = ParsedFunctorMaterial
property_name = 'h_from_p_T_functor'
expression = 'cp_mixture * T_fluid'
functor_names = 'T_fluid cp_mixture'
[]
[density_1]
type = ParsedFunctorMaterial
property_name = 'rho'
expression = '${rho} * (1. - 0.9 * T_fluid)'
functor_names = 'T_fluid'
[]
[density_2]
type = ParsedFunctorMaterial
property_name = 'rho_d'
expression = '${rho_d} * (1. - 0.9 * T_fluid)'
functor_names = 'T_fluid'
[]
[]
[Physics]
[NavierStokes]
[FlowSegregated]
[flow]
compressibility = 'weakly-compressible'
density = 'rho_mixture'
dynamic_viscosity = 'mu_mixture'
gravity = '0 ${g} 0'
# Initial conditions
initial_velocity = '1e-12 1e-12 0'
initial_pressure = 0.2
wall_boundaries = 'top left right bottom'
momentum_wall_types = 'noslip noslip noslip noslip'
momentum_wall_functors = '${U_lid} 0; 0 0; 0 0; 0 0'
orthogonality_correction = false
pressure_two_term_bc_expansion = true
momentum_advection_interpolation = ${advected_interp_method}
[]
[]
[FluidHeatTransferSegregated]
[heat]
system_names = 'energy_system'
# allows non-constant cp
solve_for_enthalpy = true
initial_temperature = ${T_fluid_top}
thermal_conductivity = 'k_mixture'
specific_heat = 'cp_mixture'
energy_wall_boundaries = 'top bottom'
energy_wall_types = 'fixed-temperature fixed-temperature'
energy_wall_functors = '0 1'
use_nonorthogonal_correction = false
energy_two_term_bc_expansion = true
energy_advection_interpolation = ${advected_interp_method}
[]
[]
[TwoPhaseMixtureSegregated]
[mixture]
system_names = 'phi_system'
phase_1_fraction_name = 'phase_1'
phase_2_fraction_name = 'phase_2'
# not fully mixed initialization
initial_phase_fraction = 'unstable'
add_phase_transport_equation = true
phase_advection_interpolation = '${advected_interp_method}'
phase_fraction_diffusivity = 1e-3
fluid_heat_transfer_physics = heat
# 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
# To match Rayleigh Bernard nonlinear test setup
add_gravity_term_in_slip_velocity = false
[]
[]
[]
[]
[Functions]
[unstable]
type = ParsedFunction
expression = 'if(y > 0.05, 1, 0)'
[]
[]
[Executioner]
type = PIMPLE
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
end_time = 1e8
[TimeStepper]
type = IterationAdaptiveDT
optimal_iterations = 10
iteration_window = 2
growth_factor = 2
cutback_factor = 0.5
dt = 1e-3
[]
# Systems
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
active_scalar_systems = 'phi_system'
momentum_equation_relaxation = 0.8
active_scalar_equation_relaxation = '0.7'
energy_equation_relaxation = '0.5'
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
energy_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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_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
energy_l_abs_tol = 1e-13
active_scalar_l_abs_tol = 1e-13
momentum_l_tol = 0
pressure_l_tol = 0
energy_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 = '0.0 0.0 0.0'
[]
[Outputs]
exodus = false
[out]
type = CSV
execute_on = 'FINAL'
[]
[]
[AuxVariables]
[U]
order = CONSTANT
family = MONOMIAL
fv = true
[]
[]
[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_x]
type = ElementExtremeFunctorValue
functor = 'Darcy_coefficient_vec_out_x'
value_type = max
[]
[max_drag_coefficient_y]
type = ElementExtremeFunctorValue
functor = 'Darcy_coefficient_vec_out_y'
value_type = max
[]
[]
(test/tests/outputs/csv/all_columns_child.i)
# Solves the nonlinear equation
# S(T) = B - A * (T - T_inf)^2
# on each node.
T_ambient = 300.0
source_coef_A = 0.1
source_coef_B = 1e4
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[S]
[]
[]
[AuxVariables]
[T_child]
[]
[]
[FunctorMaterials]
[equation_mat]
type = ADParsedFunctorMaterial
expression = 'B - A * (T - T_inf)^2 - S'
functor_symbols = 'T T_inf A B S'
functor_names = 'T_child ${T_ambient} ${source_coef_A} ${source_coef_B} S'
property_name = 'equation'
[]
[]
[Kernels]
[equation_kernel]
type = FunctorKernel
variable = S
functor = equation
functor_on_rhs = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
[]
(test/tests/functormaterials/output/output_ad.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 1
xmin = 0.0
xmax = 4.0
ymin = 0.0
ymax = 6.0
[]
[FunctorMaterials]
[parsed_fmat]
type = ADParsedFunctorMaterial
expression = 't + x + y + z'
property_name = 'prop1'
outputs = 'exodus'
output_properties = 'prop1'
[]
[parsed_vector_fmat]
type = ADGenericVectorFunctorMaterial
prop_names = 'prop1_vec'
prop_values = '1 2 3'
outputs = 'exodus'
output_properties = 'prop1_vec'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
# Get the t to be equal to 4
time = 4.0
[]
[Outputs]
exodus = true
execute_on = 'INITIAL'
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/bulk_heat_transfer/flow-around-square-linear-fluidonly.i)
mu = 0.01
rho = 1.1
k = 0.0005
cp = 10
h_conv = 5
advected_interp_method = 'upwind'
[Mesh]
[generated_mesh]
type = GeneratedMeshGenerator
dim = 2
nx = 10
ny = 10
xmin = 0
ymin = 0
ymax = 0.1
xmax = 0.1
[]
[subdomain1]
type = SubdomainBoundingBoxGenerator
input = generated_mesh
block_name = subdomain1
bottom_left = '0.04 0.04 0'
block_id = 1
top_right = '0.06 0.06 0'
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = subdomain1
primary_block = 0
paired_block = 1
new_boundary = interface
[]
[delete]
type = BlockDeletionGenerator
input = interface
block = 1
[]
[]
[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
block = 0
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = 0.1
solver_sys = u_system
block = 0
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.01
block = 0
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = 0.2
block = 0
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 300
block = 0
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = true
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[p_diffusion]
type = LinearFVAnisotropicDiffusion
variable = pressure
diffusion_tensor = Ainv
use_nonorthogonal_correction = true
[]
[HbyA_divergence]
type = LinearFVDivergence
variable = pressure
face_flux = HbyA
force_boundary_execution = true
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = true
[]
[]
[LinearFVBCs]
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_x
functor = '0.1'
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'left'
variable = vel_y
functor = '0.0'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'top bottom interface'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'right'
variable = pressure
functor = 1.4
[]
[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
[]
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = 300
boundary = 'left'
[]
[walls_T]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
functor = 0.0
boundary = 'top bottom'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = right
[]
[fluid_solid]
type = LinearFVConvectiveHeatTransferBC
variable = T_fluid
T_solid = boundary_value
T_fluid = T_fluid
boundary = interface
h = ${h_conv}
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[]
[Functions]
[boundary_value]
type = ConstantFunction
value = 350
[]
[]
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-13
pressure_l_abs_tol = 1e-13
energy_l_abs_tol = 1e-13
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 = 0.8
energy_equation_relaxation = 1.0
pressure_variable_relaxation = 0.3
num_iterations = 1000
pressure_absolute_tolerance = 1e-10
momentum_absolute_tolerance = 1e-10
energy_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'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
print_fields = false
continue_on_max_its = true
[]
[Outputs]
exodus = true
execute_on = timestep_end
[]
(test/tests/functormaterials/functor_change/fp_parent.i)
# Heat conduction with fixed temperature on left and convection BC on right:
#
# d/dx(-k dT/dx) = S'''(T) (0,1)X(0,1)
# T = T_inf x = 0
# -k dT/dx = htc (T - T_inf) x = 1
#
# Source is temperature-dependent and is calculated in the child app:
# S(T) = B - A * (T - T_inf)^2
k = 15.0
htc = 100.0
T_ambient = 300.0
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[T_nodal]
[]
[T_elem]
type = MooseVariableFVReal
[]
[]
[AuxVariables]
[S_parent]
[]
[]
[FunctorMaterials]
[heat_flux_mat_nodal]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T_nodal ${T_ambient} ${htc}'
property_name = 'heat_flux_nodal'
[]
[heat_flux_mat_elem]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T_elem ${T_ambient} ${htc}'
property_name = 'heat_flux_elem'
[]
[]
[Kernels]
[T_nodal_diff]
type = FunctionDiffusion
variable = T_nodal
function = ${k}
[]
[T_nodal_source]
type = CoupledForce
variable = T_nodal
v = S_parent
[]
[]
[FVKernels]
[T_elem_diff]
type = FVDiffusion
variable = T_elem
coeff = ${k}
[]
[T_elem_source]
type = FVCoupledForce
variable = T_elem
v = S_parent
[]
[]
[BCs]
[left_bc_nodal]
type = DirichletBC
variable = T_nodal
boundary = left
value = ${T_ambient}
[]
[right_bc_nodal]
type = FunctorNeumannBC
variable = T_nodal
boundary = right
functor = heat_flux_nodal
flux_is_inward = false
[]
[]
[FVBCs]
[left_bc_elem]
type = FVDirichletBC
variable = T_elem
boundary = left
value = ${T_ambient}
[]
[right_bc_elem]
type = FVFunctorNeumannBC
variable = T_elem
boundary = right
functor = heat_flux_elem
factor = -1
[]
[]
[MultiApps]
[source_app]
type = FullSolveMultiApp
positions = '0 0 0'
input_files = fp_child.i
execute_on = 'TIMESTEP_END'
[]
[]
[Transfers]
[T_to_child]
type = MultiAppCopyTransfer
to_multi_app = source_app
source_variable = T_nodal
variable = T_child
execute_on = 'SAME_AS_MULTIAPP'
[]
[S_from_child]
type = MultiAppCopyTransfer
from_multi_app = source_app
source_variable = S
variable = S_parent
execute_on = 'SAME_AS_MULTIAPP'
[]
[]
[FunctorMaterials]
[nodal_mat]
type = ADFunctorChangeFunctorMaterial
functor = T_nodal
change_over = fixed_point
take_absolute_value = false
prop_name = T_nodal_change
[]
[elem_mat]
type = ADFunctorChangeFunctorMaterial
functor = T_elem
change_over = fixed_point
take_absolute_value = false
prop_name = T_elem_change
[]
[S_mat]
type = ADFunctorChangeFunctorMaterial
functor = S_parent
change_over = fixed_point
take_absolute_value = false
prop_name = S_change
[]
[]
[Postprocessors]
[T_nodal_avg]
type = AverageNodalVariableValue
variable = T_nodal
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_elem_avg]
type = ElementAverageValue
variable = T_elem
execute_on = 'INITIAL TIMESTEP_END'
[]
[S_avg]
type = ElementAverageValue
variable = S_parent
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_nodal_max_change]
type = ElementExtremeFunctorValue
functor = T_nodal_change
value_type = max
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_elem_max_change]
type = ElementExtremeFunctorValue
functor = T_elem_change
value_type = max
execute_on = 'INITIAL TIMESTEP_END'
[]
[S_max_change]
type = ElementExtremeFunctorValue
functor = S_change
value_type = max
execute_on = 'TIMESTEP_BEGIN'
[]
[fp_it]
type = NumFixedPointIterations
get_index_instead_of_count = true
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Convergence]
[fp_conv]
type = IterationCountConvergence
max_iterations = 5
converge_at_max_iterations = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
multiapp_fixed_point_convergence = fp_conv
[]
[Outputs]
[console]
type = Console
new_row_detection_columns = all
execute_postprocessors_on = 'INITIAL MULTIAPP_FIXED_POINT_ITERATION_END'
[]
[out]
type = CSV
new_row_detection_columns = all
execute_on = 'INITIAL MULTIAPP_FIXED_POINT_ITERATION_END'
[]
[]
(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} ${mu_d}'
prop_names = 'rho_mixture mu_mixture'
phase_1_fraction = 'phase_2'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
nl_rel_tol = 1e-10
# dt = 0.1
# end_time = 1.0
# nl_max_its = 10
[]
[Debug]
show_var_residual_norms = true
[]
[Preconditioning]
[SMP]
type = SMP
full = true
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
[]
[]
[Outputs]
exodus = true
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '${rho} * ${l} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/wcns/materials/1d_test_cpT.i)
L = 30
bulk_u = 0.01
p_ref = 101325.0
T_in = 860
q_source = 50000
A_cp = 976.78
B_cp = 1.0634
rho = 2000
advected_interp_method = 'upwind'
[Mesh]
[gmg]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = ${L}
nx = 10
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = ${advected_interp_method}
velocity_interp_method = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = ${bulk_u}
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
initial_condition = ${p_ref}
two_term_boundary_expansion = false
[]
[T]
type = INSFVEnergyVariable
two_term_boundary_expansion = false
initial_condition = ${T_in}
[]
[]
[FVKernels]
[mass]
type = WCNSFVMassAdvection
variable = pressure
rho = 'rho'
[]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = 'rho'
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu'
momentum_component = 'x'
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
[]
[temp_conduction]
type = FVDiffusion
coeff = 'k'
variable = T
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T
[]
[source]
type = FVBodyForce
variable = T
function = source_func
[]
[]
[FVBCs]
[inlet-u]
type = INSFVInletVelocityBC
boundary = 'left'
variable = vel_x
functor = ${bulk_u}
[]
[inlet_T]
type = FVDirichletBC
variable = T
boundary = 'left'
value = ${T_in}
[]
[outlet_p]
type = INSFVOutletPressureBC
boundary = 'right'
variable = pressure
function = ${p_ref}
[]
[]
[Functions]
[source_func]
type = ParsedFunction
expression = '${q_source}'
[]
[]
[FunctorMaterials]
[converter_to_regular_T]
type = FunctorADConverter
ad_props_in = 'T'
reg_props_out = 'T_nAD'
[]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T'
rho = 'rho'
cp = 'cp'
assumed_constant_cp = false
h_in = 'h'
# Alternative to providing 'h': set the fluid property and the pressure parameter
# fp = 'fp'
# pressure = 'pressure'
[]
[rho]
type = ADParsedFunctorMaterial
property_name = 'rho'
expression = '${rho}'
[]
[mu]
type = ADParsedFunctorMaterial
property_name = 'mu'
expression = '4.5e-3'
[]
[k]
type = ADParsedFunctorMaterial
property_name = 'k'
expression = '0.7'
[]
[h]
type = ADParsedFunctorMaterial
property_name = 'h'
functor_names = 'T ${A_cp} ${B_cp}'
functor_symbols = 'T A_cp B_cp'
expression = 'A_cp * T + B_cp * T * T / 2'
[]
[cp]
type = ADParsedFunctorMaterial
property_name = 'cp'
functor_names = 'T ${A_cp} ${B_cp}'
functor_symbols = 'T A_cp B_cp'
expression = 'A_cp+B_cp*T'
[]
[]
[Executioner]
type = Steady
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
nl_abs_tol = 1e-9
nl_max_its = 50
line_search = 'none'
automatic_scaling = true
off_diagonals_in_auto_scaling = true
[]
[Postprocessors]
[H_in]
type = VolumetricFlowRate
vel_x = 'vel_x'
advected_quantity = 'rho_h'
boundary = 'left'
[]
[H_out]
type = VolumetricFlowRate
vel_x = 'vel_x'
advected_quantity = 'rho_h'
boundary = 'right'
[]
[Q]
type = FunctionElementIntegral
function = 'source_func'
execute_on = 'initial'
[]
[balance_in_percent]
type = ParsedPostprocessor
expression = '(H_out + H_in - Q) / H_in * 100'
pp_names = 'H_in H_out Q'
[]
[T_out]
type = SideAverageValue
variable = T
boundary = 'right'
[]
[T_analytical_outlet]
type = Receiver
default = ${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}
[]
[error_T]
type = ParsedPostprocessor
expression = 'T_out - T_analytical_outlet'
pp_names = 'T_out T_analytical_outlet'
[]
[]
[Outputs]
csv = true
[]
(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'
[]
[]
(test/tests/functormaterials/parsed_functor_material/parsed_functor_material.i)
[Mesh]
type = GeneratedMesh
dim = 3
nx = 2
ny = 2
nz = 2
xmin = 0.0
xmax = 4.0
ymin = 0.0
ymax = 6.0
zmin = 0.0
zmax = 10.0
[]
[Functions]
[fn1]
type = ParsedFunction
# The max value on elements should be:
# 2 * 3 + 0.5 * 4.5 + 7.5 - 4 = 11.75
expression = '2 * x + 0.5 * y + z - t'
[]
[fn2]
type = ConstantFunction
value = 3
[]
[]
[FunctorMaterials]
[parsed_fmat]
type = ParsedFunctorMaterial
expression = 'A * B^2 + 2 + pi + e + t + x + y + z'
functor_names = 'fn1 fn2'
functor_symbols = 'A B'
property_name = 'prop1'
[]
[]
[Postprocessors]
# The value should be:
# 11.75 * 3^2 + 2 + pi + e + 4 + 3 + 4.5 + 7.5 = 132.60987448204884
[get_prop1]
type = ElementExtremeFunctorValue
functor = prop1
value_type = max
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
time = 4.0
[]
[Outputs]
csv = true
execute_on = 'INITIAL'
[]
(test/tests/executioners/nl_divergence_tolerance/nl_divergence_tolerance.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[./u]
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[force]
type = FVCoupledForce
v = v
variable = u
[]
[]
[FunctorMaterials]
[parsed]
type = ADParsedFunctorMaterial
property_name = 'v'
functor_names = 'u'
expression = 'if(u>0.1,1e6,0)'
[]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
line_search = 'none'
solve_type = NEWTON
nl_max_its = 5
nl_div_tol = 10
petsc_options = '-snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(test/tests/postprocessors/discrete_variable_residual_norm/part_fv.i)
[Variables]
[T_fv]
type = MooseVariableFVReal
[]
[]
[FunctorMaterials]
[heat_flux_mat_elem]
type = ADParsedFunctorMaterial
expression = 'htc * (T - T_inf)'
functor_symbols = 'T T_inf htc'
functor_names = 'T_fv ${T_ambient} ${htc}'
property_name = 'heat_flux_elem'
[]
[source_mat_elem]
type = ADParsedFunctorMaterial
expression = '-B + A * (T - T_inf)^2'
functor_symbols = 'A B T T_inf'
functor_names = '${source_coef_A} ${source_coef_B} T_fv ${T_ambient}'
property_name = 'source_elem'
[]
[]
[FVKernels]
[T_fv_diff]
type = FVDiffusion
variable = T_fv
coeff = ${k}
[]
[T_fv_source]
type = FVFunctorElementalKernel
variable = T_fv
functor_name = source_elem
[]
[]
[FVBCs]
[left_bc_elem]
type = FVDirichletBC
variable = T_fv
boundary = left
value = ${T_ambient}
[]
[right_bc_elem]
type = FVFunctorNeumannBC
variable = T_fv
boundary = right
functor = heat_flux_elem
factor = -1
[]
[]
[Postprocessors]
[fv_A_l1]
type = DiscreteVariableResidualNorm
variable = T_fv
block = 'blockA'
norm_type = l_1
execute_on = 'FINAL'
[]
[fv_B_l1]
type = DiscreteVariableResidualNorm
variable = T_fv
block = 'blockB'
norm_type = l_1
execute_on = 'FINAL'
[]
[]
(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
[]
[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
[]
[]
(test/tests/postprocessors/side_integral/side_integral_functor_fe.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[FunctorMaterials]
[test_fmat]
type = ADParsedFunctorMaterial
property_name = test_prop
expression = '10'
[]
[]
[Postprocessors]
[test_pp]
type = ADSideIntegralFunctorPostprocessor
boundary = top
functor = test_prop
functor_argument = face # results in error due to no face info in mesh
execute_on = 'INITIAL'
[]
[]
[Problem]
solve = false
[]
[Executioner]
type = Steady
[]
(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/lid-driven/segregated/lid-driven-turb-energy.i)
##########################################################
# Lid-driven cavity test
# Reynolds: 5,000
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model with energy transport
# Standard wall functions without temperature wall functions
# SIMPLE Solve
##########################################################
### Thermophysical Properties ###
mu = 2e-5
rho = 1.0
k = 0.01
cp = 10.0
Pr_t = 0.9
### Operation Conditions ###
lid_velocity = 1.0
side_length = 0.1
### Initial Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * lid_velocity)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / side_length}'
### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09
### Modeling parameters ###
bulk_wall_treatment = false
walls = 'left top right bottom'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq
pressure_tag = "pressure_grad"
[GlobalParams]
rhie_chow_user_object = 'rc'
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${side_length}
ymin = 0
ymax = ${side_length}
nx = 12
ny = 12
[]
# Prevent test diffing on distributed parallel element numbering
allow_renumbering = false
[]
[Problem]
nl_sys_names = 'u_system v_system pressure_system energy_system TKE_system TKED_system'
previous_nl_solution_required = true
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolatorSegregated
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Variables]
[vel_x]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = u_system
two_term_boundary_expansion = false
[]
[vel_y]
type = INSFVVelocityVariable
initial_condition = 0.0
solver_sys = v_system
two_term_boundary_expansion = false
[]
[pressure]
type = INSFVPressureVariable
solver_sys = pressure_system
initial_condition = 0.2
two_term_boundary_expansion = false
[]
[T_fluid]
type = INSFVEnergyVariable
solver_sys = energy_system
initial_condition = 1.0
two_term_boundary_expansion = false
[]
[TKE]
type = INSFVEnergyVariable
solver_sys = TKE_system
initial_condition = ${k_init}
two_term_boundary_expansion = false
[]
[TKED]
type = INSFVEnergyVariable
solver_sys = TKED_system
initial_condition = ${eps_init}
two_term_boundary_expansion = false
[]
[]
[FVKernels]
[u_advection]
type = INSFVMomentumAdvection
variable = vel_x
rho = ${rho}
momentum_component = 'x'
[]
[u_viscosity]
type = INSFVMomentumDiffusion
variable = vel_x
mu = ${mu}
momentum_component = 'x'
[]
[u_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_x
mu = 'mu_t'
momentum_component = 'x'
complete_expansion = true
u = vel_x
v = vel_y
[]
[u_pressure]
type = INSFVMomentumPressure
variable = vel_x
momentum_component = 'x'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[v_advection]
type = INSFVMomentumAdvection
variable = vel_y
rho = ${rho}
momentum_component = 'y'
[]
[v_viscosity]
type = INSFVMomentumDiffusion
variable = vel_y
mu = ${mu}
momentum_component = 'y'
[]
[v_viscosity_turbulent]
type = INSFVMomentumDiffusion
variable = vel_y
mu = 'mu_t'
momentum_component = 'y'
complete_expansion = true
u = vel_x
v = vel_y
[]
[v_pressure]
type = INSFVMomentumPressure
variable = vel_y
momentum_component = 'y'
pressure = pressure
extra_vector_tags = ${pressure_tag}
[]
[p_diffusion]
type = FVAnisotropicDiffusion
variable = pressure
coeff = "Ainv"
coeff_interp_method = 'average'
[]
[p_source]
type = FVDivergence
variable = pressure
vector_field = "HbyA"
force_boundary_execution = true
[]
[temp_advection]
type = INSFVEnergyAdvection
variable = T_fluid
[]
[temp_conduction]
type = FVDiffusion
coeff = ${k}
variable = T_fluid
[]
[temp_turb_conduction]
type = FVDiffusion
coeff = 'k_t'
variable = T_fluid
[]
[TKE_advection]
type = INSFVTurbulentAdvection
variable = TKE
rho = ${rho}
[]
[TKE_diffusion]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = ${mu}
[]
[TKE_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKE
coeff = 'mu_t'
scaling_coef = ${sigma_k}
[]
[TKE_source_sink]
type = INSFVTKESourceSink
variable = TKE
u = vel_x
v = vel_y
epsilon = TKED
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[TKED_advection]
type = INSFVTurbulentAdvection
variable = TKED
rho = ${rho}
walls = ${walls}
[]
[TKED_diffusion]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = ${mu}
walls = ${walls}
[]
[TKED_diffusion_turbulent]
type = INSFVTurbulentDiffusion
variable = TKED
coeff = 'mu_t'
scaling_coef = ${sigma_eps}
walls = ${walls}
[]
[TKED_source_sink]
type = INSFVTKEDSourceSink
variable = TKED
u = vel_x
v = vel_y
tke = TKE
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
C1_eps = ${C1_eps}
C2_eps = ${C2_eps}
walls = ${walls}
wall_treatment = ${wall_treatment}
[]
[]
[FVBCs]
[top_x]
type = INSFVNoSlipWallBC
variable = vel_x
boundary = 'top'
function = ${lid_velocity}
[]
[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
[]
[T_hot]
type = FVDirichletBC
variable = T_fluid
boundary = 'top'
value = 1
[]
[T_cold]
type = FVDirichletBC
variable = T_fluid
boundary = 'bottom'
value = 0
[]
[walls_mu_t]
type = INSFVTurbulentViscosityWallFunction
boundary = 'left right top bottom'
variable = mu_t
u = vel_x
v = vel_y
rho = ${rho}
mu = ${mu}
mu_t = 'mu_t'
tke = TKE
wall_treatment = ${wall_treatment}
[]
[]
[AuxVariables]
[mu_t]
type = MooseVariableFVReal
initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
two_term_boundary_expansion = false
[]
[]
[AuxKernels]
[compute_mu_t]
type = kEpsilonViscosityAux
variable = mu_t
C_mu = ${C_mu}
tke = TKE
epsilon = TKED
mu = ${mu}
rho = ${rho}
u = vel_x
v = vel_y
bulk_wall_treatment = ${bulk_wall_treatment}
walls = ${walls}
wall_treatment = ${wall_treatment}
execute_on = 'NONLINEAR'
[]
[]
[FunctorMaterials]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T_fluid'
rho = ${rho}
cp = ${cp}
[]
[k_t]
type = ADParsedFunctorMaterial
expression = 'mu_t * cp / Pr_t'
functor_names = 'mu_t ${cp} ${Pr_t}'
functor_symbols = 'mu_t cp Pr_t'
property_name = 'k_t'
[]
[]
[Executioner]
type = SIMPLENonlinearAssembly
rhie_chow_user_object = 'rc'
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
energy_system = 'energy_system'
turbulence_systems = 'TKED_system TKE_system'
pressure_gradient_tag = ${pressure_tag}
momentum_equation_relaxation = 0.8
pressure_variable_relaxation = 0.5
energy_equation_relaxation = 0.9
turbulence_equation_relaxation = '0.8 0.8'
num_iterations = 500
pressure_absolute_tolerance = 1e-12
momentum_absolute_tolerance = 1e-12
energy_absolute_tolerance = 1e-12
turbulence_absolute_tolerance = '1e-12 1e-12'
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
momentum_l_abs_tol = 1e-14
energy_l_abs_tol = 1e-14
pressure_l_abs_tol = 1e-14
turbulence_l_abs_tol = 1e-14
momentum_l_max_its = 30
pressure_l_max_its = 30
momentum_l_tol = 0.0
energy_l_tol = 0.0
pressure_l_tol = 0.0
turbulence_l_tol = 0.0
print_fields = false
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '0.01 0.099 0.0'
continue_on_max_its = true
[]
[Outputs]
csv = true
perf_graph = false
print_nonlinear_residuals = false
print_linear_residuals = true
[]
[VectorPostprocessors]
[side_bottom]
type = SideValueSampler
boundary = 'bottom'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_top]
type = SideValueSampler
boundary = 'top'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[side_left]
type = SideValueSampler
boundary = 'left'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[side_right]
type = SideValueSampler
boundary = 'right'
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[horizontal_center]
type = LineValueSampler
start_point = '${fparse 0.01 * side_length} ${fparse 0.499 * side_length} 0'
end_point = '${fparse 0.99 * side_length} ${fparse 0.499 * side_length} 0'
num_points = ${Mesh/gen/nx}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'x'
execute_on = 'timestep_end'
[]
[vertical_center]
type = LineValueSampler
start_point = '${fparse 0.499 * side_length} ${fparse 0.01 * side_length} 0'
end_point = '${fparse 0.499 * side_length} ${fparse 0.99 * side_length} 0'
num_points = ${Mesh/gen/ny}
variable = 'vel_x vel_y pressure TKE TKED'
sort_by = 'y'
execute_on = 'timestep_end'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/ins/natural_convection/linear_segregated/2d/diff_heated_cavity_linear_buoyancy.i)
################################################################################
# MATERIAL PROPERTIES
################################################################################
rho_0 = 3279.
mu = 1.0
k_cond = 38.0
cp = ${fparse 640}
alpha_b = 3.26e-5
T_0 = 875.0
walls = 'right left top bottom'
[GlobalParams]
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
advected_interp_method = 'upwind'
u = vel_x
v = vel_y
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system'
previous_nl_solution_required = true
[]
################################################################################
# GEOMETRY
################################################################################
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 1
xmax = 2.0
ymin = 1.0
ymax = 2.0
nx = 15
ny = 15
[]
[]
################################################################################
# EQUATIONS: VARIABLES, KERNELS & BCS
################################################################################
[UserObjects]
[ins_rhie_chow_interpolator]
type = RhieChowMassFlux
u = vel_x
v = vel_y
pressure = pressure
rho = 'rho'
p_diffusion_kernel = p_diffusion
body_force_kernel_names = 'u_buoyancy; v_buoyancy'
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
initial_condition = 0
solver_sys = pressure_system
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = 875
[]
[]
[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'
[]
[u_buoyancy]
type = LinearFVMomentumBuoyancy
variable = vel_x
rho = 'rho'
reference_rho = ${rho_0}
gravity = '0 -9.81 0'
momentum_component = 'x'
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
mu = ${mu}
momentum_component = 'y'
use_nonorthogonal_correction = false
[]
[v_pressure]
type = LinearFVMomentumPressure
variable = vel_y
pressure = pressure
momentum_component = 'y'
[]
[v_buoyancy]
type = LinearFVMomentumBuoyancy
variable = vel_y
rho = 'rho'
reference_rho = ${rho_0}
gravity = '0 -9.81 0'
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 = false
[]
####### FUEL ENERGY EQUATION #######
[heat_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k_cond}
[]
[]
[LinearFVBCs]
[no-slip-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_x
boundary = ${walls}
functor = 0
[]
[no-slip-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = vel_y
boundary = ${walls}
functor = 0
[]
[T_cold]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
boundary = 'right'
functor = 870.0
[]
[T_hot]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
boundary = 'left'
functor = 880.0
[]
[T_all]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
boundary = 'top bottom'
functor = 0.0
[]
[pressure]
type = LinearFVPressureFluxBC
boundary = 'top bottom left right'
variable = pressure
HbyA_flux = HbyA
Ainv = Ainv
[]
[]
[FunctorMaterials]
[rho_function]
type = ParsedFunctorMaterial
property_name = 'rho'
functor_names = 'T_fluid'
expression = '${rho_0}*(1-${alpha_b}*(T_fluid-${T_0})) '
[]
[]
################################################################################
# EXECUTION / SOLVE
################################################################################
[Executioner]
type = SIMPLE
momentum_l_abs_tol = 1e-11
pressure_l_abs_tol = 1e-11
energy_l_abs_tol = 1e-11
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 = 1500
pressure_absolute_tolerance = 1e-8
momentum_absolute_tolerance = 1e-8
energy_absolute_tolerance = 1e-8
print_fields = false
momentum_l_max_its = 300
pin_pressure = true
pressure_pin_value = 0.0
pressure_pin_point = '1.5 1.5 0.0'
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
[]
################################################################################
# SIMULATION OUTPUTS
################################################################################
[Outputs]
exodus = true
[]
(modules/navier_stokes/test/tests/finite_volume/ins/cht/conjugate_heat_transfer/cht_rob-rob.i)
### benchmark sources:
### https://doi.org/10.1016/j.compfluid.2018.06.016
### https://doi.org/10.1016/0017-9310(74)90087-8
b = 0.01 # plate thickness
l = 0.2 # plate length
nxi = 24 # nx in the inlet/entrance region
nyf = 18 # ny in fluid
nxf = 24 # nx in the main fluid region
nys = 8 # ny in the solid domain
fx1_bias = 1.00 # bdry layer bias - fluid
fx2_bias = '${fparse 1.0/1.00}' # bdry layer bias - solid
fy_bias = 1.20 # bdry layer bias - fluid
sy_bias = '${fparse 1.0/1.05}' # bdry layer bias - solid
k_s = 0.2876
rho = 0.3525
mu = 3.95e-5
k = 0.06808
cp = 1142.6
vin = 12.0
Tin = 1000.0
T_s_bottom = 600.0
P_out = 1.03e5
h_s = 1.0
h_f = 1.0
advected_interp_method = 'upwind'
[Mesh]
[fluid_channel]
type = GeneratedMeshGenerator
dim = 2
nx = ${nxf}
ny = ${nyf}
xmin = 0
xmax = ${l}
ymin = 0
ymax = '${fparse 10.0*b}'
subdomain_ids = '1'
subdomain_name = 'fluid'
bias_x = '${fx1_bias}'
bias_y = '${fparse fy_bias}'
boundary_name_prefix = 'fluid'
[]
[solid_base]
type = GeneratedMeshGenerator
dim = 2
nx = ${nxf}
ny = ${nys}
xmin = 0
xmax = ${l}
ymin = '${fparse -b}'
ymax = 0
subdomain_ids = '2'
subdomain_name = 'solid'
bias_x = ${fx1_bias}
bias_y = '${fparse sy_bias}'
boundary_id_offset = 10
boundary_name_prefix = 'solid'
[]
[entrance]
type = GeneratedMeshGenerator
dim = 2
nx = '${fparse 2.0*nxi}'
ny = ${nyf}
xmin = '${fparse -2.0*l}'
xmax = 0
ymin = 0
ymax = '${fparse 10.0*b}'
subdomain_ids = '0'
subdomain_name = 'entrance'
bias_x = ${fx2_bias}
bias_y = '${fparse fy_bias}'
boundary_id_offset = 20
boundary_name_prefix = 'ent'
[]
[smg]
type = StitchedMeshGenerator
inputs = 'entrance fluid_channel solid_base'
stitch_boundaries_pairs = 'ent_right fluid_left;
fluid_bottom solid_top'
prevent_boundary_ids_overlap = false
[]
[interface]
type = SideSetsBetweenSubdomainsGenerator
input = 'smg'
primary_block = 'fluid'
paired_block = 'solid'
new_boundary = interface
[]
[symmetry_transform]
type = SymmetryTransformGenerator
input = interface
mirror_point = '0 0 0'
mirror_normal_vector = '0 1 0'
[]
inactive = 'symmetry_transform'
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system energy_system solid_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
block = '0 1'
[]
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
initial_condition = ${vin}
solver_sys = u_system
block = '0 1'
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
initial_condition = 0.0
block = '0 1'
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
initial_condition = ${P_out}
block = '0 1'
[]
[T_fluid]
type = MooseLinearVariableFVReal
solver_sys = energy_system
initial_condition = ${Tin}
block = '0 1'
[]
[T_solid]
type = MooseLinearVariableFVReal
solver_sys = solid_energy_system
initial_condition = ${T_s_bottom}
block = 2
[]
[]
[LinearFVKernels]
[u_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_x
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'x'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[v_advection_stress]
type = LinearWCNSFVMomentumFlux
variable = vel_y
advected_interp_method = ${advected_interp_method}
mu = ${mu}
u = vel_x
v = vel_y
momentum_component = 'y'
rhie_chow_user_object = 'rc'
use_nonorthogonal_correction = false
[]
[u_pressure]
type = LinearFVMomentumPressure
variable = vel_x
pressure = pressure
momentum_component = 'x'
[]
[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
[]
[h_advection]
type = LinearFVEnergyAdvection
variable = T_fluid
advected_quantity = temperature
cp = ${cp}
advected_interp_method = ${advected_interp_method}
rhie_chow_user_object = 'rc'
[]
[conduction]
type = LinearFVDiffusion
variable = T_fluid
diffusion_coeff = ${k}
use_nonorthogonal_correction = false
[]
[solid-conduction]
type = LinearFVDiffusion
variable = T_solid
diffusion_coeff = ${k_s}
use_nonorthogonal_correction = false
[]
[]
[LinearFVBCs]
# velocity BCs
[inlet-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_left'
variable = vel_x
functor = ${vin}
[]
[inlet-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_left'
variable = vel_y
functor = '0.000'
[]
[walls-u]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_bottom interface'
variable = vel_x
functor = 0.0
[]
[walls-v]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'ent_bottom interface'
variable = vel_y
functor = 0.0
[]
[outlet_p]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = 'fluid_right'
variable = pressure
functor = ${P_out}
[]
[outlet_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_right'
variable = vel_x
use_two_term_expansion = false
[]
[outlet_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_right'
variable = vel_y
use_two_term_expansion = false
[]
# freestream BCs for top of fluid domain
[freestream_u]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_top ent_top'
variable = vel_x
use_two_term_expansion = false
[]
[freestream_v]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = 'fluid_top ent_top'
variable = vel_y
use_two_term_expansion = false
[]
[freestream_p]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
boundary = 'fluid_top ent_top'
variable = pressure
functor = 0
[]
# temperature BCs
[inlet_T]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_fluid
functor = ${Tin}
boundary = 'ent_left'
[]
[heated_wall_solid]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
variable = T_solid
functor = ${T_s_bottom}
boundary = 'solid_bottom'
[]
[insulated_fluid]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_fluid
functor = 0
boundary = 'ent_top ent_bottom fluid_top'
[]
[insulated_solid]
type = LinearFVAdvectionDiffusionFunctorNeumannBC
variable = T_solid
functor = 0
boundary = 'solid_left solid_right'
[]
[outlet_T]
type = LinearFVAdvectionDiffusionOutflowBC
variable = T_fluid
use_two_term_expansion = false
boundary = 'fluid_right'
[]
[fluid_solid]
type = LinearFVRobinCHTBC
variable = T_fluid
boundary = interface
h = ${h_f}
incoming_flux = heat_flux_to_fluid_interface
surface_temperature = interface_temperature_solid_interface
thermal_conductivity = ${k}
[]
[solid_fluid]
type = LinearFVRobinCHTBC
variable = T_solid
boundary = interface
h = ${h_s}
incoming_flux = heat_flux_to_solid_interface
surface_temperature = interface_temperature_fluid_interface
thermal_conductivity = ${k_s}
[]
[]
[FunctorMaterials]
[rhocpT]
property_name = 'rhocpT'
type = ParsedFunctorMaterial
functor_names = 'T_fluid'
expression = '${rho}*${cp}*T_fluid'
[]
[]
[Postprocessors]
[h_in]
type = VolumetricFlowRate
boundary = 'ent_left'
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
subtract_mesh_velocity = false
[]
[h_out]
type = VolumetricFlowRate
boundary = 'fluid_right fluid_top ent_top interface'
vel_x = vel_x
vel_y = vel_y
rhie_chow_user_object = rc
advected_quantity = 'rhocpT'
advected_interp_method = upwind
subtract_mesh_velocity = false
[]
[]
[VectorPostprocessors]
[y_vs_ts]
type = LineValueSampler
variable = 'T_solid'
start_point = '0.05 -1e-9 0' # making sure we are always in the domain
end_point = '0.05 ${fparse -b+1e-9} 0'
num_points = 8
sort_by = id
warn_discontinuous_face_values = false
[]
[y_vs_tf]
type = LineValueSampler
variable = 'T_fluid'
start_point = '0.05 1e-9 0' # making sure we are always in the domain
end_point = '0.05 ${fparse b-1e-9} 0'
num_points = 12
sort_by = id
warn_discontinuous_face_values = false
[]
[]
[Executioner]
type = SIMPLE
num_iterations = 1000
momentum_systems = 'u_system v_system'
pressure_system = 'pressure_system'
rhie_chow_user_object = 'rc'
momentum_l_abs_tol = 1e-10
pressure_l_abs_tol = 1e-10
momentum_l_tol = 0
pressure_l_tol = 0
momentum_equation_relaxation = 0.9
pressure_variable_relaxation = 0.3
momentum_absolute_tolerance = 1e-7
pressure_absolute_tolerance = 1e-7
momentum_petsc_options_iname = '-pc_type -pc_hypre_type'
momentum_petsc_options_value = 'hypre boomeramg'
pressure_petsc_options_iname = '-pc_type -pc_hypre_type'
pressure_petsc_options_value = 'hypre boomeramg'
energy_system = 'energy_system'
solid_energy_system = 'solid_energy_system'
energy_l_abs_tol = 1e-10
solid_energy_l_abs_tol = 1e-10
energy_l_tol = 0
solid_energy_l_tol = 0
energy_equation_relaxation = 1.0
energy_absolute_tolerance = 1e-7
solid_energy_absolute_tolerance = 1e-7
energy_petsc_options_iname = '-pc_type -pc_hypre_type'
energy_petsc_options_value = 'hypre boomeramg'
solid_energy_petsc_options_iname = '-pc_type -pc_hypre_type'
solid_energy_petsc_options_value = 'hypre boomeramg'
cht_interfaces = 'interface'
cht_solid_flux_relaxation = 1.0
cht_fluid_flux_relaxation = 1.0
cht_solid_temperature_relaxation = 1.0
cht_fluid_temperature_relaxation = 1.0
max_cht_fpi = 2
print_fields = false
[]
[Outputs]
exodus = true
csv = true
execute_on = timestep_end
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-transient.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
density_interp_method = 'average'
mu_interp_method = 'average'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${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'
[]
[]
(test/tests/executioners/nl_divergence_tolerance/nl_abs_divergence_tolerance.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[./u]
type = MooseVariableFVReal
[../]
[]
[FVKernels]
[./diff]
type = FVDiffusion
variable = u
coeff = 1
[../]
[force]
type = FVCoupledForce
v = v
variable = u
[]
[]
[FunctorMaterials]
[parsed]
type = ADParsedFunctorMaterial
property_name = 'v'
functor_names = 'u'
expression = 'if(u>0.1,1e6,0)'
[]
[]
[FVBCs]
[./left]
type = FVDirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = FVDirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
line_search = 'none'
solve_type = NEWTON
nl_max_its = 5
nl_abs_div_tol = 1e+5
nl_div_tol = 1e+50
petsc_options = '-snes_converged_reason -ksp_converged_reason'
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
(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'
[]
(test/tests/convergence/default_steady_state_convergence/base.i)
# Solves the IVPs
#
# dS/dt = CS*(S1 - S) x in (x1,x2)
# S(0) = S0
#
# dT/dt = CT*(T1 - T) x in (x3,x4)
# T(0) = T0
#
# on each node, which have the solutions
#
# S(t) = S1 + (S0 - S1) exp(-CS t)
# T(t) = T1 + (T0 - T1) exp(-CT t)
#
# Also define the aux variable:
#
# U(S) = S^2
S0 = 500.0
S1 = 300.0
CS = 100.0
T0 = 500.0
T1 = 300.0
CT = 1.0
x1 = 0
x2 = 10
x3 = 11
x4 = 13
ss_tol = 1e-6
[Mesh]
[S_meshgen]
type = GeneratedMeshGenerator
dim = 1
xmin = ${x1}
xmax = ${x2}
nx = 1
subdomain_ids = 0
subdomain_name = S_mesh
[]
[T_meshgen]
type = GeneratedMeshGenerator
dim = 1
xmin = ${x3}
xmax = ${x4}
nx = 1
subdomain_ids = 1
subdomain_name = T_mesh
[]
[combined]
type = CombinerGenerator
inputs = 'S_meshgen T_meshgen'
[]
[]
[Variables]
[S]
block = S_mesh
initial_condition = ${S0}
[]
[T]
initial_condition = ${T0}
[]
[]
[FunctorMaterials]
[S_mat]
type = ADParsedFunctorMaterial
expression = 'CS*(S1 - S)'
functor_symbols = 'CS S1 S'
functor_names = '${CS} ${S1} S'
property_name = 'S_source'
[]
[T_mat]
type = ADParsedFunctorMaterial
expression = 'CT*(T1 - T)'
functor_symbols = 'CT T1 T'
functor_names = '${CT} ${T1} T'
property_name = 'T_source'
[]
[]
[Kernels]
[S_time]
type = TimeDerivative
variable = S
[]
[S_source]
type = FunctorKernel
variable = S
functor = S_source
functor_on_rhs = true
[]
[T_time]
type = TimeDerivative
variable = T
[]
[T_source]
type = FunctorKernel
variable = T
functor = T_source
functor_on_rhs = true
[]
[]
[AuxVariables]
[U]
block = S_mesh
[]
[]
[AuxKernels]
[U_aux]
type = ParsedAux
variable = U
expression = 'S^2'
functor_names = 'S'
functor_symbols = 'S'
[]
[]
[Executioner]
type = Transient
dt = 1.0
end_time = 100.0
steady_state_detection = true
steady_state_convergence = steady_conv
solve_type = NEWTON
[]
[Postprocessors]
[num_time_steps]
type = NumTimeSteps
execute_on = 'TIMESTEP_END'
[]
[]
[Outputs]
[out]
type = CSV
execute_on = 'FINAL'
[]
[]
(test/tests/convergence/child.i)
# Solves the nonlinear equation
# S(T) = B - A * (T - T_inf)^2
# on each node.
T_ambient = 300.0
source_coef_A = 0.1
source_coef_B = 1e4
[Mesh]
type = GeneratedMesh
dim = 2
nx = 5
ny = 5
[]
[Variables]
[S]
[]
[]
[AuxVariables]
[T_child]
[]
[]
[FunctorMaterials]
[equation_mat]
type = ADParsedFunctorMaterial
expression = 'B - A * (T - T_inf)^2 - S'
functor_symbols = 'T T_inf A B S'
functor_names = 'T_child ${T_ambient} ${source_coef_A} ${source_coef_B} S'
property_name = 'equation'
[]
[]
[Kernels]
[equation_kernel]
type = FunctorKernel
variable = S
functor = equation
functor_on_rhs = true
[]
[]
[Executioner]
type = Steady
solve_type = NEWTON
nl_max_its = 10
nl_abs_tol = 1e-8
nl_rel_tol = 1e-8
l_tol = 1e-3
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-advection-slip.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'
[GlobalParams]
rhie_chow_user_object = 'rc'
mu_interp_method = 'average'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = vel_x
v = vel_y
pressure = pressure
[]
[]
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${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} * ${U}'
pp_names = ''
[]
[rho_outlet]
type = SideAverageValue
boundary = 'right'
variable = 'rho_mixture_var'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/segregated/channel-drift-flux.i)
mu = 1.0
rho = 10.0
mu_d = 0.1
rho_d = 1.0
l = 2
# 'average' leads to slight oscillations, upwind may be preferred
# This method is selected for consistency with the original nonlinear input
advected_interp_method = 'average'
# TODO remove need for those
cp = 1
k = 1
cp_d = 1
k_d = 1
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = '${fparse l * 5}'
ymin = '${fparse -l / 2}'
ymax = '${fparse l / 2}'
nx = 10
ny = 4
[]
uniform_refine = 0
[]
[Problem]
linear_sys_names = 'u_system v_system pressure_system phi_system'
previous_nl_solution_required = true
[]
[Variables]
[vel_x]
type = MooseLinearVariableFVReal
solver_sys = u_system
initial_condition = 1
[]
[vel_y]
type = MooseLinearVariableFVReal
solver_sys = v_system
[]
[pressure]
type = MooseLinearVariableFVReal
solver_sys = pressure_system
[]
[phase_2]
type = MooseLinearVariableFVReal
solver_sys = phi_system
[]
[]
[LinearFVKernels]
[flow_p_diffusion]
type = LinearFVAnisotropicDiffusion
diffusion_tensor = Ainv
use_nonorthogonal_correction = false
variable = pressure
[]
[flow_HbyA_divergence]
type = LinearFVDivergence
face_flux = HbyA
force_boundary_execution = true
variable = pressure
[]
[flow_ins_momentum_flux_x]
type = LinearWCNSFVMomentumFlux
advected_interp_method = ${advected_interp_method}
momentum_component = x
mu = mu_mixture
rhie_chow_user_object = ins_rhie_chow_interpolator
u = vel_x
use_deviatoric_terms = false
use_nonorthogonal_correction = false
v = vel_y
variable = vel_x
[]
[flow_ins_momentum_flux_y]
type = LinearWCNSFVMomentumFlux
advected_interp_method = ${advected_interp_method}
momentum_component = y
mu = mu_mixture
rhie_chow_user_object = ins_rhie_chow_interpolator
u = vel_x
use_deviatoric_terms = false
use_nonorthogonal_correction = false
v = vel_y
variable = vel_y
[]
[mixture_drift_flux_x]
type = LinearWCNSFV2PMomentumDriftFlux
density_interp_method = average
fraction_dispersed = phase_2
momentum_component = x
rhie_chow_user_object = ins_rhie_chow_interpolator
rho_d = ${rho_d}
u_slip = vel_slip_x
v_slip = vel_slip_y
variable = vel_x
[]
[mixture_drift_flux_y]
type = LinearWCNSFV2PMomentumDriftFlux
density_interp_method = average
fraction_dispersed = phase_2
momentum_component = y
rhie_chow_user_object = ins_rhie_chow_interpolator
rho_d = ${rho_d}
u_slip = vel_slip_x
v_slip = vel_slip_y
variable = vel_y
[]
[flow_ins_momentum_pressure_x]
type = LinearFVMomentumPressure
momentum_component = x
pressure = pressure
variable = vel_x
[]
[flow_ins_momentum_pressure_y]
type = LinearFVMomentumPressure
momentum_component = y
pressure = pressure
variable = vel_y
[]
[flow_momentum_friction_0_x]
type = LinearFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
momentum_component = x
mu = mu_mixture
variable = vel_x
[]
[flow_momentum_friction_0_y]
type = LinearFVMomentumFriction
Darcy_name = Darcy_coefficient_vec
momentum_component = y
mu = mu_mixture
variable = vel_y
[]
# Mixture phase equation
[mixture_ins_phase_2_advection]
type = LinearFVScalarAdvection
advected_interp_method = upwind
rhie_chow_user_object = ins_rhie_chow_interpolator
u_slip = vel_slip_x
v_slip = vel_slip_y
variable = phase_2
[]
[mixture_phase_interface_reaction]
type = LinearFVReaction
coeff = 0.1
variable = phase_2
[]
[mixture_phase_interface_source]
type = LinearFVSource
scaling_factor = 0.1
source_density = phase_1
variable = phase_2
[]
[]
[LinearFVBCs]
[vel_x_left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = left
functor = 1
variable = vel_x
[]
[vel_y_left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = left
functor = 0
variable = vel_y
[]
[pressure_extrapolation_inlet_left]
type = LinearFVExtrapolatedPressureBC
boundary = left
use_two_term_expansion = true
variable = pressure
[]
[vel_x_right]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = right
use_two_term_expansion = true
variable = vel_x
[]
[vel_y_right]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = right
use_two_term_expansion = true
variable = vel_y
[]
[pressure_right]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = right
functor = 0
variable = pressure
[]
[vel_x_bottom]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = bottom
functor = 0
variable = vel_x
[]
[vel_y_bottom]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = bottom
functor = 0
variable = vel_y
[]
[vel_x_top]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = top
functor = 0
variable = vel_x
[]
[vel_y_top]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = top
functor = 0
variable = vel_y
[]
[pressure_extrapolation_top_bottom]
type = LinearFVExtrapolatedPressureBC
boundary = 'top bottom'
use_two_term_expansion = true
variable = pressure
[]
[phase_2_left]
type = LinearFVAdvectionDiffusionFunctorDirichletBC
boundary = left
functor = 0.1
variable = phase_2
[]
[phase_2_right]
type = LinearFVAdvectionDiffusionOutflowBC
boundary = right
use_two_term_expansion = true
variable = phase_2
[]
[]
[FunctorMaterials]
[flow_ins_speed_material]
type = ADVectorMagnitudeFunctorMaterial
execute_on = ALWAYS
outputs = none
vector_magnitude_name = speed
x_functor = vel_x
y_functor = vel_y
[]
[mixture_phase_1_fraction]
type = ParsedFunctorMaterial
execute_on = ALWAYS
expression = '1 - phase_2'
functor_names = phase_2
output_properties = phase_1
outputs = all
property_name = phase_1
[]
[mixture_mixture_material]
type = WCNSLinearFVMixtureFunctorMaterial
execute_on = ALWAYS
limit_phase_fraction = true
outputs = all
phase_1_fraction = phase_2
phase_1_names = '${rho_d} ${mu_d} ${cp_d} ${k_d}'
phase_2_names = '${rho} ${mu} ${cp} ${k}'
prop_names = 'rho_mixture mu_mixture cp_mixture k_mixture'
[]
[mixture_slip_x]
type = WCNSFV2PSlipVelocityFunctorMaterial
execute_on = ALWAYS
gravity = '0 0 0'
linear_coef_name = Darcy_coefficient
momentum_component = x
mu = mu_mixture
outputs = all
particle_diameter = 0.01
rho = ${rho}
rho_d = ${rho_d}
slip_velocity_name = vel_slip_x
u = vel_x
v = vel_y
[]
[mixture_slip_y]
type = WCNSFV2PSlipVelocityFunctorMaterial
execute_on = ALWAYS
gravity = '0 0 0'
linear_coef_name = Darcy_coefficient
momentum_component = y
mu = mu_mixture
outputs = all
particle_diameter = 0.01
rho = ${rho}
rho_d = ${rho_d}
slip_velocity_name = vel_slip_y
u = vel_x
v = vel_y
[]
[mixture_dispersed_drag]
type = NSFVDispersePhaseDragFunctorMaterial
drag_coef_name = Darcy_coefficient
execute_on = ALWAYS
mu = mu_mixture
outputs = all
particle_diameter = 0.01
rho = rho_mixture
u = vel_x
v = vel_y
[]
[]
[UserObjects]
[ins_rhie_chow_interpolator]
type = RhieChowMassFlux
p_diffusion_kernel = flow_p_diffusion
pressure = pressure
rho = rho_mixture
u = vel_x
v = vel_y
[]
[]
[Executioner]
type = SIMPLE
rhie_chow_user_object = 'ins_rhie_chow_interpolator'
# 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_hypre_type'
active_scalar_petsc_options_value = 'hypre boomeramg'
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
[]
[Outputs]
csv = true
[]
[Postprocessors]
[Re]
type = ParsedPostprocessor
expression = '10.0 * 2 * 1'
[]
[average_phase2]
type = ElementAverageValue
variable = phase_2
[]
[dp]
type = PressureDrop
boundary = 'left right'
downstream_boundary = right
pressure = pressure
upstream_boundary = left
[]
[max_phase2]
type = ElementExtremeValue
variable = phase_2
[]
[]