InternalVolumetricFlowRate

Computes the volumetric flow rate of an advected quantity through an internal boundary.

Input Parameters

boundaryThe list of boundary IDs from the mesh where this boundary condition applies
C++ Type:std::vector<BoundaryName>
Options:
Description:The list of boundary IDs from the mesh where this boundary condition applies
vel_xThe x-axis velocity
C++ Type:std::vector<VariableName>
Options:
Description:The x-axis velocity

Required Parameters

advected_interp_methodupwindThe interpolation to use for the advected quantity. Options are 'upwind' and 'average', with the default being 'upwind'.
Default:upwind
C++ Type:MooseEnum
Options:average, upwind
Description:The interpolation to use for the advected quantity. Options are 'upwind' and 'average', with the default being 'upwind'.
advected_mat_prop0The advected material property of which to study the flow
Default:0
C++ Type:MaterialPropertyName
Options:
Description:The advected material property of which to study the flow
advected_variableThe advected variable quantity of which to study the flow
C++ Type:std::vector<VariableName>
Options:
Description:The advected variable quantity of which to study the flow
execute_onTIMESTEP_ENDThe list of flag(s) indicating when this object should be executed, the available options include NONE, INITIAL, LINEAR, NONLINEAR, TIMESTEP_END, TIMESTEP_BEGIN, FINAL, CUSTOM.
Default:TIMESTEP_END
C++ Type:ExecFlagEnum
Options:NONE, INITIAL, LINEAR, NONLINEAR, TIMESTEP_END, TIMESTEP_BEGIN, FINAL, CUSTOM, TRANSFER
Description:The list of flag(s) indicating when this object should be executed, the available options include NONE, INITIAL, LINEAR, NONLINEAR, TIMESTEP_END, TIMESTEP_BEGIN, FINAL, CUSTOM.
fvFalseWhether finite volume variables are used
Default:False
C++ Type:bool
Options:
Description:Whether finite volume variables are used
prop_getter_suffixAn optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Options:
Description:An optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
vel_yThe y-axis velocity
C++ Type:std::vector<VariableName>
Options:
Description:The y-axis velocity
vel_zThe z-axis velocity
C++ Type:std::vector<VariableName>
Options:
Description:The z-axis velocity

Optional Parameters

allow_duplicate_execution_on_initialFalseIn the case where this UserObject is depended upon by an initial condition, allow it to be executed twice during the initial setup (once before the IC and again after mesh adaptivity (if applicable).
Default:False
C++ Type:bool
Options:
Description:In the case where this UserObject is depended upon by an initial condition, allow it to be executed twice during the initial setup (once before the IC and again after mesh adaptivity (if applicable).
control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Options:
Description:Adds user-defined labels for accessing object parameters via control logic.
enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Options:
Description:Set the enabled status of the MooseObject.
force_postauxFalseForces the UserObject to be executed in POSTAUX
Default:False
C++ Type:bool
Options:
Description:Forces the UserObject to be executed in POSTAUX
force_preauxFalseForces the UserObject to be executed in PREAUX
Default:False
C++ Type:bool
Options:
Description:Forces the UserObject to be executed in PREAUX
force_preicFalseForces the UserObject to be executed in PREIC during initial setup
Default:False
C++ Type:bool
Options:
Description:Forces the UserObject to be executed in PREIC during initial setup
implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Options:
Description:Determines whether this object is calculated using an implicit or explicit form
outputsVector of output names were you would like to restrict the output of variables(s) associated with this object
C++ Type:std::vector<OutputName>
Options:
Description:Vector of output names were you would like to restrict the output of variables(s) associated with this object
use_displaced_meshFalseWhether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Default:False
C++ Type:bool
Options:
Description:Whether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.

Advanced Parameters

Input Files

(modules/navier_stokes/test/tests/postprocessors/conservation_INSFV.i)
(modules/navier_stokes/test/tests/postprocessors/conservation_PINSFV.i)
(modules/navier_stokes/test/tests/postprocessors/conservation_INSFE.i)

(modules/navier_stokes/test/tests/postprocessors/conservation_INSFV.i)

mu=1.1
rho=1
advected_interp_method='average'
velocity_interp_method='average'

[GlobalParams]
  two_term_boundary_expansion = true
[]

[Mesh]
  inactive = 'mesh internal_boundary_bot internal_boundary_top'
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1'
    dy = '1 1 1'
    ix = '5'
    iy = '5 5 5'
    subdomain_id = '1
                    2
                    3'
  []
  [internal_boundary_bot]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    new_boundary = 'internal_bot'
    primary_block = 1
    paired_block = 2
  []
  [internal_boundary_top]
    type = SideSetsBetweenSubdomainsGenerator
    input = internal_boundary_bot
    new_boundary = 'internal_top'
    primary_block = 2
    paired_block = 3
  []
  [diverging_mesh]
    type = FileMeshGenerator
    file = 'expansion_quad.e'
  []
[]

[Problem]
  fv_bcs_integrity_check = true
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 0
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [temperature]
    type = INSFVEnergyVariable
  []
[]

[AuxVariables]
  [advected_density]
    order = CONSTANT
    family = MONOMIAL
    fv = true
    initial_condition = ${rho}
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    vel = 'velocity'
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    advected_quantity = 'rhou'
    vel = 'velocity'
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
  []
  [u_viscosity]
    type = FVDiffusion
    variable = u
    coeff = ${mu}
    force_boundary_execution = true
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_quantity = 'rhov'
    vel = 'velocity'
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
  []
  [v_viscosity]
    type = FVDiffusion
    variable = v
    coeff = ${mu}
    force_boundary_execution = true
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []

  [temp_advection]
    type = INSFVEnergyAdvection
    vel = 'velocity'
    variable = temperature
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
  []
  [temp_source]
    type = FVBodyForce
    variable = temperature
    function = 10
    block = 1
  []
[]

[FVBCs]
  inactive = 'noslip-u noslip-v'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 1
  []
  [noslip-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 0
  []
  [noslip-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 0
  []
  [free-slip-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = u
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = v
  []
  [axis-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'left'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
  []
  [axis-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'left'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = y
  []
  [axis-p]
    type = INSFVSymmetryPressureBC
    boundary = 'left'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
  [inlet_temp]
    type = FVNeumannBC
    boundary = 'bottom'
    variable = temperature
    value = 300
  []
[]

[Materials]
  [ins_fv]
    type = INSFVMaterial
    u = 'u'
    v = 'v'
    pressure = 'pressure'
    temperature = 'temperature'
    rho = ${rho}
  []
  [advected_material_property]
    type = ADGenericConstantMaterial
    prop_names = 'advected_rho cp'
    prop_values ='${rho} 1'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      200                lu           NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Postprocessors]
  [inlet_mass_variable]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = advected_density
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [inlet_mass_constant]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = ${rho}
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [inlet_mass_matprop]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_mat_prop = 'advected_rho'
    fv = true
  []
  [mid1_mass]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_mass]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_mass]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []

  [inlet_momentum_x]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid1_momentum_x]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_momentum_x]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_momentum_x]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []

  [inlet_momentum_y]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid1_momentum_y]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_momentum_y]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_momentum_y]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []

  [inlet_advected_energy]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
  []
  [mid1_advected_energy]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_advected_energy]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_advected_energy]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
  []
[]

[Outputs]
  exodus = false
  csv = true
  inactive = 'console_mass console_momentum_x console_momentum_y console_energy'
  [console_mass]
    type = Console
    start_step = 1
    show = 'inlet_mass_variable inlet_mass_constant inlet_mass_matprop mid1_mass mid2_mass outlet_mass'
  []
  [console_momentum_x]
    type = Console
    start_step = 1
    show = 'inlet_momentum_x mid1_momentum_x mid2_momentum_x outlet_momentum_x'
  []
  [console_momentum_y]
    type = Console
    start_step = 1
    show = 'inlet_momentum_y mid1_momentum_y mid2_momentum_y outlet_momentum_y'
  []
  [console_energy]
    type = Console
    start_step = 1
    show = 'inlet_advected_energy mid1_advected_energy mid2_advected_energy outlet_advected_energy'
  []
[]

(modules/navier_stokes/test/tests/postprocessors/conservation_PINSFV.i)

mu=1.1
rho=1
advected_interp_method='average'
velocity_interp_method='average'

[Mesh]
  inactive = 'mesh internal_boundary_bot internal_boundary_top'
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1'
    dy = '1 1 1'
    ix = '5'
    iy = '5 5 5'
    subdomain_id = '1
                    2
                    3'
  []
  [internal_boundary_bot]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    new_boundary = 'internal_bot'
    primary_block = 1
    paired_block = 2
  []
  [internal_boundary_top]
    type = SideSetsBetweenSubdomainsGenerator
    input = internal_boundary_bot
    new_boundary = 'internal_top'
    primary_block = 2
    paired_block = 3
  []
  [diverging_mesh]
    type = FileMeshGenerator
    file = 'expansion_quad.e'
  []
[]

[Problem]
  kernel_coverage_check = false
  fv_bcs_integrity_check = true
[]

[GlobalParams]
  two_term_boundary_expansion = true
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0
  []
  [v]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [temperature]
    type = INSFVEnergyVariable
  []
[]

[AuxVariables]
  [advected_density]
    order = CONSTANT
    family = MONOMIAL
    fv = true
    initial_condition = ${rho}
  []
  [porosity]
    order = CONSTANT
    family = MONOMIAL
    fv = true
    initial_condition = 0.5
  []
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    vel = 'velocity'
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    porosity = porosity
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_quantity = 'rhou'
    vel = 'velocity'
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    porosity = porosity
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    force_boundary_execution = true
    porosity = porosity
    mu = ${mu}
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_quantity = 'rhov'
    vel = 'velocity'
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    porosity = porosity
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    force_boundary_execution = true
    porosity = porosity
    mu = ${mu}
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [temp_advection]
    type = PINSFVEnergyAdvection
    vel = 'velocity'
    variable = temperature
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    pressure = pressure
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    porosity = porosity
  []
  [temp_source]
    type = FVBodyForce
    variable = temperature
    function = 10
    block = 1
  []
[]

[FVBCs]
  inactive = 'noslip-u noslip-v'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 1
  []
  [noslip-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 0
  []
  [noslip-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 0
  []
  [free-slip-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = u
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = v
  []
  [axis-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
    porosity = porosity
  []
  [axis-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = y
    porosity = porosity
  []
  [axis-p]
    type = INSFVSymmetryPressureBC
    boundary = 'left'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
  [inlet_temp]
    type = FVNeumannBC
    boundary = 'bottom'
    variable = temperature
    value = 300
  []
[]

[Materials]
  [ins_fv]
    type = INSFVMaterial
    u = 'u'
    v = 'v'
    pressure = 'pressure'
    temperature = 'temperature'
    rho = ${rho}
  []
  [advected_material_property]
    type = ADGenericConstantMaterial
    prop_names = 'advected_rho cp'
    prop_values ='${rho} 1'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      200                lu           NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Postprocessors]
  [inlet_mass_variable]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = advected_density
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [inlet_mass_constant]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = ${rho}
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [inlet_mass_matprop]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_mat_prop = 'advected_rho'
    fv = true
  []
  [mid1_mass]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_mass]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_mass]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []

  [inlet_momentum_x]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid1_momentum_x]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_momentum_x]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_momentum_x]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_variable = u
    fv = true
    advected_interp_method = ${advected_interp_method}
  []

  [inlet_momentum_y]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid1_momentum_y]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [mid2_momentum_y]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []
  [outlet_momentum_y]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_variable = v
    fv = true
    advected_interp_method = ${advected_interp_method}
  []

  [inlet_advected_energy]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
  []
  [mid1_advected_energy]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
  []
  [mid2_advected_energy]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
  []
  [outlet_advected_energy]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_mat_prop = 'rho_cp_temp'
    fv = true
  []
[]

[Outputs]
  exodus = false
  csv = true
  inactive = 'console_mass console_momentum_x console_momentum_y console_energy'
  [console_mass]
    type = Console
    start_step = 1
    show = 'inlet_mass_variable inlet_mass_constant inlet_mass_matprop mid1_mass mid2_mass outlet_mass'
  []
  [console_momentum_x]
    type = Console
    start_step = 1
    show = 'inlet_momentum_x mid1_momentum_x mid2_momentum_x outlet_momentum_x'
  []
  [console_momentum_y]
    type = Console
    start_step = 1
    show = 'inlet_momentum_y mid1_momentum_y mid2_momentum_y outlet_momentum_y'
  []
  [console_energy]
    type = Console
    start_step = 1
    show = 'inlet_advected_energy mid1_advected_energy mid2_advected_energy outlet_advected_energy'
  []
[]

(modules/navier_stokes/test/tests/postprocessors/conservation_INSFE.i)

[Mesh]
  second_order = true
  inactive = 'mesh internal_boundary_bot internal_boundary_top'
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1'
    dy = '1 1 1'
    ix = '5'
    iy = '5 5 5'
    subdomain_id = '1
                    2
                    3'
  []
  [internal_boundary_bot]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    new_boundary = 'internal_bot'
    primary_block = 1
    paired_block = 2
  []
  [internal_boundary_top]
    type = SideSetsBetweenSubdomainsGenerator
    input = internal_boundary_bot
    new_boundary = 'internal_top'
    primary_block = 2
    paired_block = 3
  []
  [diverging_mesh]
    type = FileMeshGenerator
    file = 'expansion_quad.e'
  []
[]

[Modules]
  [IncompressibleNavierStokes]
    equation_type = steady-state

    # no slip BCs
    velocity_boundary = 'bottom right left'
    velocity_function = '0 1    0 0   0 0'
    pressure_boundary = 'top'
    pressure_function = '1'

    density_name = rho
    dynamic_viscosity_name = mu

    integrate_p_by_parts = false
    order = SECOND
  []
[]

[Materials]
  [const]
    type = GenericConstantMaterial
    block = '1 2 3'
    prop_names = 'rho mu'
    prop_values = '1  1'
  []
  [ADconst]
    type = ADGenericConstantMaterial
    block = '1 2 3'
    prop_names = 'rho_ad'
    prop_values = '1'
  []
[]

[Preconditioning]
  [SMP_PJFNK]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type -sub_pc_factor_levels'
  petsc_options_value = '300                bjacobi  ilu          4'
  line_search = none
  nl_rel_tol = 1e-12
  nl_max_its = 6
  l_tol = 1e-6
  l_max_its = 300
[]

[Postprocessors]
  [inlet_mass_constant]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = 1
  []
  [inlet_mass_matprop]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = vel_x
    vel_y = vel_y
    advected_mat_prop = 'rho_ad'
  []
  [mid1_mass]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = vel_x
    vel_y = vel_y
  []
  [mid2_mass]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = vel_x
    vel_y = vel_y
  []
  [outlet_mass]
    type = VolumetricFlowRate
    boundary = top
    vel_x = vel_x
    vel_y = vel_y
  []

  [inlet_momentum_x]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_x
  []
  [mid1_momentum_x]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_x
  []
  [mid2_momentum_x]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_x
  []
  [outlet_momentum_x]
    type = VolumetricFlowRate
    boundary = top
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_x
  []

  [inlet_momentum_y]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_y
  []
  [mid1_momentum_y]
    type = InternalVolumetricFlowRate
    boundary = internal_bot
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_y
  []
  [mid2_momentum_y]
    type = InternalVolumetricFlowRate
    boundary = internal_top
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_y
  []
  [outlet_momentum_y]
    type = VolumetricFlowRate
    boundary = top
    vel_x = vel_x
    vel_y = vel_y
    advected_variable = vel_y
  []
[]

[Outputs]
  exodus = false
  csv = true
  inactive = 'console_mass console_momentum_x console_momentum_y'
  [console_mass]
    type = Console
    start_step = 1
    show = 'inlet_mass_variable inlet_mass_constant inlet_mass_matprop mid1_mass mid2_mass outlet_mass'
  []
  [console_momentum_x]
    type = Console
    start_step = 1
    show = 'inlet_momentum_x mid1_momentum_x mid2_momentum_x outlet_momentum_x'
  []
  [console_momentum_y]
    type = Console
    start_step = 1
    show = 'inlet_momentum_y mid1_momentum_y mid2_momentum_y outlet_momentum_y'
  []
[]

Input Parameters
Input Files

Install MOOSE

New Users

Examples and Tutorials

Application Usage

Physics and Syntax

Application Development

Framework Development

MOOSEDocs

Infrastructure

Questions

Information and Tools

INL Applications and Remote Access

InternalVolumetricFlowRate

Input Parameters

Required Parameters

Optional Parameters

Advanced Parameters

Input Files