- boundaryThe list of boundary IDs from the mesh where this boundary condition applies
C++ Type:std::vector<BoundaryName>
Description:The list of boundary IDs from the mesh where this boundary condition applies
- vel_xThe x-axis velocity
C++ Type:std::vector<VariableName>
Description:The x-axis velocity
InternalVolumetricFlowRate
Computes the volumetric flow rate of an advected quantity through an internal boundary.
Input 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
- 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.
- 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_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'
[]
[]
(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'
p = 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'
p = 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_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'
p = 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'
p = 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'
[]
[]