INSFVInletVelocityBC

functor

C++ Type:MooseFunctorName

Unit:(no unit assumed)

Controllable:No

Description:The name of the functor whose value is imposed on the boundary. A functor is any of the following: a variable, a functor material property, a function, a postprocessor or a number.

variable

C++ Type:NonlinearVariableName

Unit:(no unit assumed)

Controllable:No

Description:The name of the variable that this boundary condition applies to

boundary

C++ Type:std::vector<BoundaryName>

Controllable:No

Description:The list of boundary IDs from the mesh where this object applies

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-symmetry.i)

mu=1.1
rho=1.1

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  two_term_boundary_expansion = true
  advected_interp_method = 'average'
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
  []
  [v]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[ICs]
  [u]
    type = FunctionIC
    function = 'exact_u'
    variable = u
  []
  [v]
    type = FunctionIC
    function = 'exact_v'
    variable = v
  []
  [pressure]
    type = FunctionIC
    function = 'exact_p'
    variable = pressure
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[FVBCs]
  [u_wall]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'right'
    function = 'exact_u'
  []
  [v_wall]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'right'
    function = 'exact_v'
  []
  [u_axis]
    type = INSFVSymmetryVelocityBC
    variable = u
    boundary = 'left'
    mu = ${mu}
    u = u
    v = v
    momentum_component = 'x'
  []
  [v_axis]
    type = INSFVSymmetryVelocityBC
    variable = v
    boundary = 'left'
    mu = ${mu}
    u = u
    v = v
    momentum_component = 'y'
  []
  [p_axis]
    type = INSFVSymmetryPressureBC
    variable = pressure
    boundary = 'left'
  []
  [p]
    type = INSFVOutletPressureBC
    variable = pressure
    function = 'exact_p'
    boundary = 'top'
  []
  [inlet_u]
    type = INSFVInletVelocityBC
    variable = u
    function = 'exact_u'
    boundary = 'bottom'
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = v
    function = 'exact_v'
    boundary = 'bottom'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin(x*pi)*cos(y*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '2*pi^2*mu*sin(x*pi)*cos(y*pi) - 2*pi*rho*sin(x*pi)*sin(y*pi)*cos(1.3*x)*cos(y*pi) + 2*pi*rho*sin(x*pi)*cos(x*pi)*cos(y*pi)^2 - 1.5*sin(1.5*x)*cos(1.6*y)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'cos(1.3*x)*cos(y*pi)'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '1.69*mu*cos(1.3*x)*cos(y*pi) + pi^2*mu*cos(1.3*x)*cos(y*pi) - 1.3*rho*sin(1.3*x)*sin(x*pi)*cos(y*pi)^2 - 2*pi*rho*sin(y*pi)*cos(1.3*x)^2*cos(y*pi) + pi*rho*cos(1.3*x)*cos(x*pi)*cos(y*pi)^2 - 1.6*sin(1.6*y)*cos(1.5*x)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'cos(1.5*x)*cos(1.6*y)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-pi*rho*sin(y*pi)*cos(1.3*x) + pi*rho*cos(x*pi)*cos(y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu       NONZERO               superlu_dist'
  line_search = 'none'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-12
[]

[Outputs]
  exodus = false
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/diverging.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  file = diverging.msh
  uniform_refine = 2
[]

[Problem]
  coord_type = 'RZ'
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1e-15
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-15
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

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

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
    # we can think of the axis as a slip wall boundary, no normal velocity and no viscous shear
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
[]

[FVBCs]
  active = 'inlet-u inlet-v free-slip-wall-u free-slip-wall-v outlet-p axis-u axis-v'

  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 1
  []
  [free-slip-wall-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = u
    momentum_component = 'x'
  []
  [free-slip-wall-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = v
    momentum_component = 'y'
  []
  [no-slip-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 0
  []
  [no-slip-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 0
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
  [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
  []
[]

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

[Debug]
  show_var_residual_norms = true
[]

[Postprocessors]
  [in]
    type = SideIntegralVariablePostprocessor
    variable = v
    boundary = 'bottom'
  []
  [out]
    type = SideIntegralVariablePostprocessor
    variable = v
    boundary = 'top'
  []
  [num_lin]
    type = NumLinearIterations
    outputs = 'console'
  []
  [num_nl]
    type = NumNonlinearIterations
    outputs = 'console'
  []
  [cum_lin]
    type = CumulativeValuePostprocessor
    outputs = 'console'
    postprocessor = 'num_lin'
  []
  [cum_nl]
    type = CumulativeValuePostprocessor
    outputs = 'console'
    postprocessor = 'num_nl'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/wcns/materials/2d-transient.i)

l = 10
velocity_interp_method = 'rc'
advected_interp_method = 'average'

# Operating conditions
inlet_temp = 300
outlet_pressure = 1e5
inlet_v = 0.001

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = ${l}
    ymin = 0
    ymax = 1
    nx = 20
    ny = 10
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  rho = 'rho'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = ${inlet_v}
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-15
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${outlet_pressure}
  []
  [T]
    type = INSFVEnergyVariable
    initial_condition = ${inlet_temp}
  []
[]

[AuxVariables]
  [velocity_norm]
    type = MooseVariableFVReal
  []
  [power_density]
    type = MooseVariableFVReal
    initial_condition = 1e4
  []
[]

[FVKernels]
  [mass_time]
    type = WCNSFVMassTimeDerivative
    variable = pressure
    drho_dt = drho_dt
  []
  [mass]
    type = WCNSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = 'rho'
  []

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

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

  [temp_time]
    type = WCNSFVEnergyTimeDerivative
    variable = T
    rho = rho
    drho_dt = drho_dt
    h = h
    dh_dt = dh_dt
  []
  [temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = T
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [heat_source]
    type = FVCoupledForce
    variable = T
    v = power_density
  []
[]

[FVBCs]
  [no_slip_x]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'top bottom'
    function = 0
  []

  [no_slip_y]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'top bottom'
    function = 0
  []

  # Inlet
  [inlet_u]
    type = INSFVInletVelocityBC
    variable = u
    boundary = 'left'
    function = ${inlet_v}
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = v
    boundary = 'left'
    function = 0
  []
  [inlet_T]
    type = FVDirichletBC
    variable = T
    boundary = 'left'
    value = ${inlet_temp}
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    variable = pressure
    boundary = 'right'
    function = ${outlet_pressure}
  []
[]

[FluidProperties]
  [fp]
    type = FlibeFluidProperties
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T'
    rho = 'rho'
  []
  [fluid_props_to_mat_props]
    type = GeneralFunctorFluidProps
    fp = fp
    pressure = 'pressure'
    T_fluid = 'T'
    speed = 'velocity_norm'

    # even though we provide rho from the parameters, we
    # want to get rho from the fluid properties
    force_define_density = true

    # To initialize with a high viscosity
    mu_rampdown = 'mu_rampdown'

    # For porous flow
    characteristic_length = 1
    porosity = 1
  []
[]

[AuxKernels]
  [speed]
    type = VectorMagnitudeAux
    variable = 'velocity_norm'
    x = u
    y = v
  []
[]

[Functions]
  [mu_rampdown]
    type = PiecewiseLinear
    x = '1 2 3 4'
    y = '1e3 1e2 1e1 1'
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'

  [TimeStepper]
    type = IterationAdaptiveDT
    dt = 1e-3
    optimal_iterations = 6
  []
  end_time = 15

  nl_abs_tol = 1e-12
  nl_max_its = 50
  line_search = 'none'

  automatic_scaling = true
  off_diagonals_in_auto_scaling = true
  compute_scaling_once = false
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/1d-rc-epsjump.i)

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

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '30 30'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
  []
[]

[ICs]
  inactive = 'porosity_continuous'
  [porosity_1]
    type = ConstantIC
    variable = porosity
    block = 1
    value = 1
  []
  [porosity_2]
    type = ConstantIC
    variable = porosity
    block = 2
    value = 0.5
  []
  [porosity_continuous]
    type = FunctionIC
    variable = porosity
    block = '1 2'
    function = smooth_jump
  []
[]

[Functions]
  [smooth_jump]
    type = ParsedFunction
    expression = '1 - 0.5 * 1 / (1 + exp(-30*(x-1)))'
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  line_search = 'none'
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/pins/mms/1d-rc.i)

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

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '5 5'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.8
  []
[]

[Problem]
  error_on_jacobian_nonzero_reallocation = true
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'cos((1/2)*x*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '0.25*pi^2*mu*cos((1/2)*x*pi) - 1.25*pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) + 0.8*cos(x)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin(x)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressureFlux
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    functor = 'exact_u'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

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

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

[Outputs]
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_total_viscosity_material/steady.i)

von_karman_const = 0.41

H = 1 #halfwidth of the channel
L = 150

Re = 100

rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * 2 * H / Re}'

advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${L}'
    dy = '0.667 0.333'
    ix = '200'
    iy = '10  1'
  []
[]

[Functions]
  [delta_func]
    type = ParsedFunction
    expression = '1.0-x/150'
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_length]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

[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}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_x
    rho = ${rho}
    mixing_length = mixing_length
    momentum_component = 'x'
    u = vel_x
    v = vel_y
  []
  [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}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_y
    rho = ${rho}
    mixing_length = mixing_length
    momentum_component = 'y'
    u = vel_x
    v = vel_y
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []
[]

[AuxKernels]
  [mixing_length]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_length
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
    delta = 0.5
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0'
  []
  [wall-u]
    type = INSFVWallFunctionBC
    variable = vel_x
    boundary = 'top'
    u = vel_x
    v = vel_y
    mu = ${mu}
    rho = ${rho}
    momentum_component = x
  []
  [wall-v]
    type = INSFVWallFunctionBC
    variable = vel_y
    boundary = 'top'
    u = vel_x
    v = vel_y
    mu = ${mu}
    rho = ${rho}
    momentum_component = y
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = total_viscosity
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = total_viscosity
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[FunctorMaterials]
  [total_viscosity]
    type = MixingLengthTurbulentViscosityFunctorMaterial
    u = 'vel_x' #computes total viscosity = mu_t + mu
    v = 'vel_y' #property is called total_viscosity
    mixing_length = mixing_length
    mu = ${mu}
    rho = ${rho}
  []
[]

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

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1
    ymin = 0
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[Problem]
  coord_type = 'RZ'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = false
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = false
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 'exact_v'
  []
  [no-slip-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 'exact_u'
  []
  [no-slip-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 'exact_v'
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 'exact_p'
  []
  [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
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin(x*pi)^2*sin((1/2)*y*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin(x*pi)^2*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/4)*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) + (4*x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^4*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)^2*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x - (-2*x*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) + 2*x*pi^2*mu*sin((1/2)*y*pi)*cos(x*pi)^2 + 2*pi*mu*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos(y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*cos(x*pi)*cos(y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)*cos(y*pi) + 2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi))/x'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc.i)

mu = 1.1
rho = 1.1

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = 0
    ymax = 1
    nx = 20
    ny = 10
  []
[]

[GlobalParams]
  advected_interp_method = 'average'
  velocity_interp_method = 'rc'
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  inactive = 'lambda'
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [lambda]
    family = SCALAR
    order = FIRST
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []
[]

[FVKernels]
  inactive = 'mean-pressure'
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    rho = ${rho}
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [mean-pressure]
    type = FVIntegralValueConstraint
    variable = pressure
    lambda = lambda
    phi0 = 0.01
  []
[]

[FVBCs]
  # Select desired boundary conditions
  active = 'inlet-u inlet-v outlet-p free-slip-u free-slip-v'

  # Possible inlet boundary conditions
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-p]
    type = INSFVOutletPressureBC
    boundary = 'left'
    variable = pressure
    function = 1
  []

  # Possible wall boundary conditions
  [free-slip-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    momentum_component = 'y'
  []
  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    function = 0
  []
  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  # Possible outlet boundary conditions
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
  [outlet-p-novalue]
    type = INSFVMassAdvectionOutflowBC
    boundary = 'right'
    variable = pressure
    u = superficial_vel_x
    v = superficial_vel_y
    rho = ${rho}
  []
  [outlet-u]
    type = PINSFVMomentumAdvectionOutflowBC
    boundary = 'right'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    porosity = porosity
    momentum_component = 'x'
    rho = ${rho}
  []
  [outlet-v]
    type = PINSFVMomentumAdvectionOutflowBC
    boundary = 'right'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    porosity = porosity
    momentum_component = 'y'
    rho = ${rho}
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      300                lu           NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-11
  nl_abs_tol = 1e-14
[]

# Some basic Postprocessors to visually examine the solution
[Postprocessors]
  [inlet-p]
    type = SideIntegralVariablePostprocessor
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = superficial_vel_x
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/2d/2d-segregated-energy.i)

mu = 2.6
rho = 1.0
k = 5.0
cp = 700
alpha = 150
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '0.3'
    dy = '0.3'
    ix = '3'
    iy = '3'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system energy_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 = 0.5
    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
    initial_condition = 300
    solver_sys = energy_system
    two_term_boundary_expansion = false
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []

  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []
  [ambient_convection]
    type = NSFVEnergyAmbientConvection
    variable = T_fluid
    T_ambient = 350
    alpha = 'alpha'
  []
[]

[FVBCs]
  inactive = "symmetry-u symmetry-v symmetry-p"
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0.0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_y
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1.4
  []
  [zero-grad-pressure]
    type = FVFunctionNeumannBC
    variable = pressure
    boundary = 'top left bottom'
    function = 0.0
  []
  [inlet_t]
    type = FVDirichletBC
    boundary = 'left'
    variable = T_fluid
    value = 300
  []

  ### Inactive by default, some tests will turn these on ###
  [symmetry-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  ##########################################################
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  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 = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  energy_system = 'energy_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  energy_equation_relaxation = 0.999
  num_iterations = 100
  pressure_absolute_tolerance = 1e-10
  momentum_absolute_tolerance = 1e-10
  energy_absolute_tolerance = 1e-10
  print_fields = false
  continue_on_max_its = true
[]

[Materials]
  [const_functor]
    type = ADGenericFunctorMaterial
    prop_names = 'cp alpha'
    prop_values = '${cp} ${alpha}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

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

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/2d/2d-segregated-scalar.i)

mu = 2.6
rho = 1.0
diff = 1.5
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '0.3'
    dy = '0.3'
    ix = '3'
    iy = '3'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system scalar_1_system scalar_2_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 = 0.5
    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
  []
  [scalar_1]
    type = INSFVScalarFieldVariable
    solver_sys = scalar_1_system
    initial_condition = 1.2
  []
  [scalar_2]
    type = INSFVScalarFieldVariable
    solver_sys = scalar_2_system
    initial_condition = 1.2
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []

  [scalar_1_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar_1
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_1_diffusion]
    type = FVDiffusion
    coeff = ${diff}
    variable = scalar_1
  []
  [scalar_1_src]
    type = FVBodyForce
    variable = scalar_1
    value = 1.0
  []
  [scalar_1_coupled_source]
    type = FVCoupledForce
    variable = scalar_1
    v = scalar_2
    coef = 0.1
  []

  [scalar_2_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar_2
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_2_diffusion]
    type = FVDiffusion
    coeff = '${fparse 2*diff}'
    variable = scalar_2
  []
  [scalar_2_src]
    type = FVBodyForce
    variable = scalar_2
    value = 5.0
  []
  [scalar_2_coupled_source]
    type = FVCoupledForce
    variable = scalar_2
    v = scalar_1
    coef = 0.05
  []
[]

[FVBCs]
  inactive = "symmetry-u symmetry-v symmetry-p"
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0.0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_y
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1.4
  []
  [inlet_scalar_1]
    type = FVDirichletBC
    boundary = 'left'
    variable = scalar_1
    value = 1
  []
  [inlet_scalar_2]
    type = FVDirichletBC
    boundary = 'left'
    variable = scalar_2
    value = 2
  []

  ### Inactive by default, some tests will turn these on ###
  [symmetry-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  ##########################################################
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  passive_scalar_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  passive_scalar_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  passive_scalar_systems = 'scalar_1_system scalar_2_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  passive_scalar_equation_relaxation = '0.9 0.9'
  num_iterations = 100
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  passive_scalar_absolute_tolerance = '1e-13 1e-13'
  print_fields = false
[]

[Outputs]
  exodus = true
  [csv]
    type = CSV
    execute_on = FINAL
  []
[]

[Postprocessors]
  inactive = "out1 out2 in1 in2"
  [out1]
    type = VolumetricFlowRate
    vel_x = vel_x
    vel_y = vel_y
    advected_quantity = 'scalar_1'
    boundary = right
    execute_on = FINAL
    outputs = csv
  []
  [in1]
    type = VolumetricFlowRate
    vel_x = vel_x
    vel_y = vel_y
    advected_quantity = 'scalar_1'
    boundary = left
    execute_on = FINAL
    outputs = csv
  []
  [out2]
    type = VolumetricFlowRate
    vel_x = vel_x
    vel_y = vel_y
    advected_quantity = 'scalar_2'
    boundary = right
    execute_on = FINAL
    outputs = csv
  []
  [in2]
    type = VolumetricFlowRate
    vel_x = vel_x
    vel_y = vel_y
    advected_quantity = 'scalar_2'
    boundary = left
    execute_on = FINAL
    outputs = csv
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_total_viscosity_material/mixing_length_total_viscosity.i)

von_karman_const = 0.41

H = 1 #halfwidth of the channel
L = 150

Re = 13700

rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}

advected_interp_method='upwind'
velocity_interp_method='rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${L}'
    dy = '0.667 0.333'
    ix = '200'
    iy = '10  1'
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_length]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

[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}
    momentum_component = 'x'
  []
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_x
    rho = ${rho}
    mixing_length = mixing_length
    momentum_component = 'x'
    u = vel_x
    v = vel_y
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
  []

  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_y
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_y
    rho = ${rho}
    mixing_length = mixing_length
    momentum_component = 'y'
    u = vel_x
    v = vel_y
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []
[]

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_length
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
    delta = 0.5
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0'
  []
  [wall-u]
    type = INSFVWallFunctionBC
    variable = vel_x
    boundary = 'top'
    u = vel_x
    v = vel_y
    mu = ${mu}
    rho = ${rho}
    momentum_component = x
  []
  [wall-v]
    type = INSFVWallFunctionBC
    variable = vel_y
    boundary = 'top'
    u = vel_x
    v = vel_y
    mu = ${mu}
    rho = ${rho}
    momentum_component = y
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = total_viscosity
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = total_viscosity
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[FunctorMaterials]
  [total_viscosity]
    type = MixingLengthTurbulentViscosityFunctorMaterial
    u = 'vel_x'                             #computes total viscosity = mu_t + mu
    v = 'vel_y'                             #property is called total_viscosity
    mixing_length = mixing_length
    mu = ${mu}
    rho = ${rho}
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  [TimeStepper]
    type = IterationAdaptiveDT
    optimal_iterations = 6
    dt = 1e-3
  []
  nl_abs_tol = 1e-8
  end_time = 1e9
[]

[Outputs]
  [out]
    type = Exodus
    execute_on = 'final'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-transient.i)

# Fluid properties
mu = 1.1
rho = 1.1
cp = 1.1
k = 1e-3

# Operating conditions
u_inlet = 1
T_inlet = 200
T_solid = 190
p_outlet = 10
h_fs = 0.01

# Numerical scheme
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = -1
    ymax = 1
    nx = 50
    ny = 20
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = ${u_inlet}
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1e-12
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = ${T_inlet}
  []
[]

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

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

  [energy_time]
    type = INSFVEnergyTimeDerivative
    variable = T_fluid
    rho = ${rho}
    dh_dt = dh_dt
  []
  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    variable = T_fluid
    coeff = ${k}
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = 0
  []
  [inlet-T]
    type = FVNeumannBC
    variable = T_fluid
    value = '${fparse u_inlet * rho * cp * T_inlet}'
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_y
    function = 0
  []

  [symmetry-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet_u]
    type = INSFVMomentumAdvectionOutflowBC
    variable = vel_x
    u = vel_x
    v = vel_y
    boundary = 'right'
    momentum_component = 'x'
    rho = ${rho}
  []
  [outlet_v]
    type = INSFVMomentumAdvectionOutflowBC
    variable = vel_y
    u = vel_x
    v = vel_y
    boundary = 'right'
    momentum_component = 'y'
    rho = ${rho}
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '${p_outlet}'
  []
[]

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv T_solid'
    prop_values = '${h_fs} ${T_solid}'
  []
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '${cp}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  line_search = 'none'
  nl_rel_tol = 7e-13
  dt = 0.4
  end_time = 0.8
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/controls/switch-pressure-bc/test.i)

rho = 1
mu = 1
l = 1
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'
outlet_pressure = 1e5
inlet_v = 1

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = ${l}
    ymin = 0
    ymax = 1
    nx = 4
    ny = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = ${inlet_v}
  []
  [vel_y]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${outlet_pressure}
  []
[]

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

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

[FVBCs]
  [free_slip_x]
    type = INSFVNaturalFreeSlipBC
    variable = vel_x
    boundary = 'top bottom'
    momentum_component = 'x'
  []

  [free_slip_y]
    type = INSFVNaturalFreeSlipBC
    variable = vel_y
    boundary = 'top bottom'
    momentum_component = 'y'
  []

  # Inlet
  [inlet_u]
    type = INSFVInletVelocityBC
    variable = vel_x
    boundary = 'left'
    function = ${inlet_v}
  []
  [inlet_u_later]
    type = INSFVInletVelocityBC
    variable = vel_x
    boundary = 'right'
    function = ${fparse -1 * inlet_v}
    enable = false
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = vel_y
    boundary = 'left'
    function = 0
  []
  [inlet_v_later]
    type = INSFVInletVelocityBC
    variable = vel_y
    boundary = 'right'
    function = 0
    enable = false
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    variable = pressure
    boundary = 'right'
    function = ${outlet_pressure}
  []
  [outlet_p_later]
    type = INSFVOutletPressureBC
    variable = pressure
    boundary = 'left'
    function = ${fparse 2 * outlet_pressure}
    enable = false
  []
[]

[Functions]
  [conditional_function]
    type = ParsedFunction
    expression = 't > 1.5'
  []
[]

[Controls]
  [p_threshold]
    type = ConditionalFunctionEnableControl
    conditional_function = conditional_function
    disable_objects = 'FVBCs::outlet_p FVBCs::inlet_u FVBCs::inlet_v'
    enable_objects = 'FVBCs::outlet_p_later FVBCs::inlet_u_later FVBCs::inlet_v_later'
    execute_on = 'INITIAL TIMESTEP_BEGIN'
  []
[]

[FunctorMaterials]
  [const_functor]
    type = ADGenericFunctorMaterial
    prop_names = 'rho mu'
    prop_values = '${rho} ${mu}'
  []
[]

[Postprocessors]
  [pressure_right]
    type = SideAverageValue
    variable = pressure
    boundary = right
  []

  [pressure_left]
    type = SideAverageValue
    variable = pressure
    boundary = right
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  end_time = 3
  line_search = 'bt'
  nl_abs_tol = 1e-8
  abort_on_solve_fail = true
[]

[Outputs]
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc-friction.i)

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

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '2.5 2.5'
    dy = '1.0'
    ix = '20 20'
    iy = '20'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  inactive = 'lambda'
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [lambda]
    family = SCALAR
    order = FIRST
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []
[]

[FVKernels]
  inactive = 'mean-pressure'
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_x
    momentum_component = 'x'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    mu = ${mu}
    rho = ${rho}
    speed = speed
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_y
    momentum_component = 'y'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []

  [mean-pressure]
    type = FVIntegralValueConstraint
    variable = pressure
    lambda = lambda
    phi0 = 0.01
  []
[]

[FVBCs]
  inactive = 'free-slip-u free-slip-v'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [free-slip-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = superficial_vel_y
    momentum_component = 'y'
  []
  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

[FunctorMaterials]
  [darcy]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Darcy_coefficient Forchheimer_coefficient'
    prop_values = '0.1 0.1 0.1 0.1 0.1 0.1'
  []
  [speec]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  nl_rel_tol = 1e-11
  nl_abs_tol = 1e-14
[]

# Some basic Postprocessors to visually examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = superficial_vel_x
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-mixing-length.i)

Re = 1e4
von_karman_const = 0.2

D = 1
rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * D / Re}'

advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = 0
    ymax = '${fparse 0.5 * D}'
    nx = 20
    ny = 10
    bias_y = '${fparse 1 / 1.2}'
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [scalar]
    type = INSFVScalarFieldVariable
  []
[]

[AuxVariables]
  [mixing_length]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

[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}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_x
    rho = ${rho}
    mixing_length = 'mixing_length'
    momentum_component = 'x'
    u = vel_x
    v = vel_y
  []
  [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}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_y
    rho = ${rho}
    mixing_length = 'mixing_length'
    momentum_component = 'y'
    u = vel_x
    v = vel_y
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []

  [scalar_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_diffusion_rans]
    type = INSFVMixingLengthScalarDiffusion
    variable = scalar
    mixing_length = 'mixing_length'
    u = vel_x
    v = vel_y
    schmidt_number = 1.0
  []
  [scalar_src]
    type = FVBodyForce
    variable = scalar
    value = 0.1
  []
[]

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top bottom'
    variable = 'mixing_length'
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0'
  []
  [inlet_scalar]
    type = FVDirichletBC
    boundary = 'left'
    variable = scalar
    value = 1
  []
  [wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_x
    function = 0
  []
  [wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_y
    function = 0
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = 'total_viscosity'
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = 'total_viscosity'
    momentum_component = y
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[FunctorMaterials]
  [total_viscosity]
    type = MixingLengthTurbulentViscosityFunctorMaterial
    u = 'vel_x' #computes total viscosity = mu_t + mu
    v = 'vel_y' #property is called total_viscosity
    mixing_length = 'mixing_length'
    mu = ${mu}
    rho = ${rho}
  []
[]

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

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/wall_distance_capped_mixing_length_aux/capped_mixing_length.i)

von_karman_const = 0.41

H = 1 #halfwidth of the channel
L = 150

Re = 13700

rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}

advected_interp_method='upwind'
velocity_interp_method='rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${L}'
    dy = '0.667 0.333'
    ix = '100'
    iy = '10  1'
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_len]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_shear_stress]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_yplus]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

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

  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = v
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = v
    rho = ${rho}
    mixing_length = mixing_len
    momentum_component = 'y'
    u = u
    v = v
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
[]

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_len
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
    delta = 0.5
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [wall-u]
    type = INSFVWallFunctionBC
    variable = u
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = x
  []
  [wall-v]
    type = INSFVWallFunctionBC
    variable = v
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = y
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  [TimeStepper]
    type = IterationAdaptiveDT
    optimal_iterations = 6
    dt = 1e-3
  []
  nl_abs_tol = 1e-8
  end_time = 1e9
[]

[Outputs]
  [out]
    type = Exodus
    execute_on = 'final'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/rotated/rotated-pp-flow.i)

mu=0.5
rho=1.1
advected_interp_method='average'
velocity_interp_method='average'
two_term_boundary_expansion=true

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 10
    ny = 2
  []
  [rotate]
    type = TransformGenerator
    input = gen
    transform = 'rotate'
    vector_value = '45 0 0'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[AuxVariables]
  [vel_exact_x][]
  [vel_exact_y][]
  [p_exact][]
[]

[AuxKernels]
  [u_exact]
    type = FunctionAux
    variable = vel_exact_x
    function = exact_u
  []
  [v_exact]
    type = FunctionAux
    variable = vel_exact_y
    function = exact_v
  []
  [p_exact]
    type = FunctionAux
    variable = p_exact
    function = exact_p
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = ${two_term_boundary_expansion}
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = ${two_term_boundary_expansion}
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = ${two_term_boundary_expansion}
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'top bottom'
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'top bottom'
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = '0.25*sqrt(2)*(1.0 - 1/2*(-x + y)^2)/mu'
    symbol_names = 'mu'
    symbol_values = '${mu}'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = '0.25*sqrt(2)*rho*(1.0 - 1/2*(-x + y)^2)/mu'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '0'
  []
  [exact_v]
    type = ParsedFunction
    expression = '0.25*sqrt(2)*(1.0 - 1/2*(-x + y)^2)/mu'
    symbol_names = 'mu'
    symbol_values = '${mu}'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = '0.25*sqrt(2)*rho*(1.0 - 1/2*(-x + y)^2)/mu'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '0'
  []
  [exact_p]
    type = ParsedFunction
    expression = '-1/2*sqrt(2)*(x + y) + 10.0'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '0'
  []
[]

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

[Outputs]
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2Error
    variable = u
    function = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2Error
    variable = v
    function = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    variable = pressure
    function = exact_p
    type = ElementL2Error
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

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

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

pressure_tag = "pressure_grad"

restricted_blocks = '1'

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

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

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

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

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []

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

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

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

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

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

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

(modules/navier_stokes/test/tests/finite_volume/wcns/channel-flow/2d-transient.i)

rho = 'rho'
l = 10
velocity_interp_method = 'rc'
advected_interp_method = 'average'

# Artificial fluid properties
# For a real case, use a GeneralFluidFunctorProperties and a viscosity rampdown
# or initialize very well!
k = 1
cp = 1000
mu = 1e2

# Operating conditions
inlet_temp = 300
outlet_pressure = 1e5
inlet_v = 0.001

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = ${l}
    ymin = 0
    ymax = 1
    nx = 20
    ny = 10
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = ${inlet_v}
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1e-15
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${outlet_pressure}
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = ${inlet_temp}
  []
[]

[AuxVariables]
  [mixing_length]
    type = MooseVariableFVReal
  []
  [power_density]
    type = MooseVariableFVReal
    initial_condition = 1e4
  []
[]

[FVKernels]
  inactive = 'u_turb v_turb temp_turb'
  [mass_time]
    type = WCNSFVMassTimeDerivative
    variable = pressure
    drho_dt = drho_dt
  []
  [mass]
    type = WCNSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_time]
    type = WCNSFVMomentumTimeDerivative
    variable = vel_x
    drho_dt = drho_dt
    rho = rho
    momentum_component = 'x'
  []
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
  []
  [u_turb]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_x
    rho = ${rho}
    mixing_length = 'mixing_length'
    momentum_component = 'x'
    u = vel_x
    v = vel_y
  []

  [v_time]
    type = WCNSFVMomentumTimeDerivative
    variable = vel_y
    drho_dt = drho_dt
    rho = rho
    momentum_component = 'y'
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    momentum_component = 'y'
    mu = ${mu}
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []
  [v_turb]
    type = INSFVMixingLengthReynoldsStress
    variable = vel_y
    rho = ${rho}
    mixing_length = 'mixing_length'
    momentum_component = 'y'
    u = vel_x
    v = vel_y
  []

  [temp_time]
    type = WCNSFVEnergyTimeDerivative
    variable = T_fluid
    rho = rho
    drho_dt = drho_dt
    h = h
    dh_dt = dh_dt
  []
  [temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = T_fluid
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [heat_source]
    type = FVCoupledForce
    variable = T_fluid
    v = power_density
  []
  [temp_turb]
    type = WCNSFVMixingLengthEnergyDiffusion
    variable = T_fluid
    rho = rho
    cp = cp
    mixing_length = 'mixing_length'
    schmidt_number = 1
    u = vel_x
    v = vel_y
  []
[]

[FVBCs]
  [no_slip_x]
    type = INSFVNoSlipWallBC
    variable = vel_x
    boundary = 'top bottom'
    function = 0
  []

  [no_slip_y]
    type = INSFVNoSlipWallBC
    variable = vel_y
    boundary = 'top bottom'
    function = 0
  []

  # Inlet
  [inlet_u]
    type = INSFVInletVelocityBC
    variable = vel_x
    boundary = 'left'
    function = ${inlet_v}
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = vel_y
    boundary = 'left'
    function = 0
  []
  [inlet_T]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'left'
    value = ${inlet_temp}
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    variable = pressure
    boundary = 'right'
    function = ${outlet_pressure}
  []
[]

[FluidProperties]
  [fp]
    type = FlibeFluidProperties
  []
[]

[FunctorMaterials]
  [const_functor]
    type = ADGenericFunctorMaterial
    prop_names = 'cp k'
    prop_values = '${cp} ${k}'
  []
  [rho]
    type = RhoFromPTFunctorMaterial
    fp = fp
    temperature = T_fluid
    pressure = pressure
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T_fluid'
    rho = ${rho}
  []
[]

[AuxKernels]
  inactive = 'mixing_len'
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_length
    execute_on = 'initial'
    delta = 0.5
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'

  [TimeStepper]
    type = IterationAdaptiveDT
    dt = 1e-3
    optimal_iterations = 6
  []
  end_time = 15

  nl_abs_tol = 1e-9
  nl_max_its = 50
  line_search = 'none'

  automatic_scaling = true
  off_diagonals_in_auto_scaling = true
  compute_scaling_once = false
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/3d/3d-segregated-energy.i)

mu = 0.002
rho = 1.0
k = 5.0
cp = 700
alpha = 150
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 3
    dx = '0.2'
    dy = '0.2'
    dz = '0.8'
    ix = '3'
    iy = '3'
    iz = '12'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system w_system pressure_system energy_system'
  previous_nl_solution_required = true
  error_on_jacobian_nonzero_reallocation = true
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    w = vel_z
    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
  []
  [vel_z]
    type = INSFVVelocityVariable
    initial_condition = 0.5
    solver_sys = w_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
    initial_condition = 300
    solver_sys = energy_system
    two_term_boundary_expansion = false
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [w_advection]
    type = INSFVMomentumAdvection
    variable = vel_z
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [w_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_z
    mu = ${mu}
    momentum_component = 'z'
  []
  [w_pressure]
    type = INSFVMomentumPressure
    variable = vel_z
    momentum_component = 'z'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []
  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []
  [ambient_convection]
    type = NSFVEnergyAmbientConvection
    variable = T_fluid
    T_ambient = 350
    alpha = 'alpha'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_x
    function = '0'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_y
    function = '0'
  []
  [inlet-w]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_z
    function = '1.1'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom '
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom'
    variable = vel_y
    function = 0.0
  []
  [walls-w]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom'
    variable = vel_z
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'front'
    variable = pressure
    function = 1.4
  []
  [zero-grad-pressure]
    type = FVFunctionNeumannBC
    variable = pressure
    boundary = 'back left right top bottom'
    function = 0.0
  []
  [inlet_t]
    type = FVDirichletBC
    boundary = 'back'
    variable = T_fluid
    value = 300
  []
[]

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

[Executioner]
  type = SIMPLENonlinearAssembly
  # petsc_options_iname = '-pc_type -pc_hypre_type -pc_factor_shift_type'
  # petsc_options_value = 'hypre boomeramg NONZERO'
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system w_system'
  pressure_system = 'pressure_system'
  energy_system = 'energy_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  energy_equation_relaxation = 0.95
  num_iterations = 150
  pressure_absolute_tolerance = 1e-11
  momentum_absolute_tolerance = 1e-11
  energy_absolute_tolerance = 1e-11
  print_fields = false

  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
[]

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

(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/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/ins/variables/caching/3d-rc.i)

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

pressure_cell_gradient_caching = true
velocity_cell_gradient_caching = true

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    zmin = -1
    zmax = 1
    nx = 15
    ny = 5
    nz = 5
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    w = w
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    cache_cell_gradients = ${velocity_cell_gradient_caching}
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
    cache_cell_gradients = ${velocity_cell_gradient_caching}
  []
  [w]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
    cache_cell_gradients = ${velocity_cell_gradient_caching}
  []
  [pressure]
    type = INSFVPressureVariable
    cache_cell_gradients = ${pressure_cell_gradient_caching}
  []
[]

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

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

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

  [w_advection]
    type = INSFVMomentumAdvection
    variable = w
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'z'
  []
  [w_viscosity]
    type = INSFVMomentumDiffusion
    variable = w
    mu = ${mu}
    momentum_component = 'z'
  []
  [w_pressure]
    type = INSFVMomentumPressure
    variable = w
    momentum_component = 'z'
    pressure = pressure
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []
  [inlet-w]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = w
    function = 0
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom front back'
    variable = u
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom front back'
    variable = v
    momentum_component = 'y'
  []
  [walls-w]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom front back'
    variable = w
    momentum_component = 'z'
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

[Postprocessors]
  [physical]
    type = MemoryUsage
    mem_type = physical_memory
    value_type = total
    # by default MemoryUsage reports the peak value for the current timestep
    # out of all samples that have been taken (at linear and non-linear iterations)
    execute_on = 'INITIAL TIMESTEP_END NONLINEAR LINEAR'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart'
  petsc_options_value = 'asm      100               '
  line_search = 'none'
  nl_abs_tol = 1e-8
[]

[Outputs]
  hide = 'physical'
  perf_graph = true
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/jeffery-hamel/wedge_dirichlet_fv.i)

mu=1
rho=1

# This input file tests whether we can converge to the semi-analytical
# solution for flow in a 2D wedge.
[GlobalParams]
  velocity_interp_method = 'rc'
  advected_interp_method = 'average'
  rhie_chow_user_object = 'rc'
  alpha_degrees = 15
  Re = 30
  K = -9.78221333616
  f = f_theta
[]

[Mesh]
  [file]
    type = FileMeshGenerator
    file = wedge_8x12.e
  []
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
  []
  [vel_y]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [lambda]
    family = SCALAR
    order = FIRST
  []
[]

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

  [mean_zero_pressure]
    type = FVIntegralValueConstraint
    variable = pressure
    lambda = lambda
    phi0 = 0.0
  []

  [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
  []
[]

[FVBCs]
  [no_slip_x]
    type = INSFVNoSlipWallBC
    variable = vel_x
    boundary = 'top_wall bottom_wall'
    function = 0
  []

  [no_slip_y]
    type = INSFVNoSlipWallBC
    variable = vel_y
    boundary = 'top_wall bottom_wall'
    function = 0
  []

  [inlet_x]
    type = INSFVInletVelocityBC
    variable = vel_x
    boundary = 'inlet outlet'
    function = vel_x_exact
  []

  [inlet_y]
    type = INSFVInletVelocityBC
    variable = vel_y
    boundary = 'inlet outlet'
    function = vel_y_exact
  []
[]

[Functions]
  [f_theta]
    # Non-dimensional solution values f(eta), 0 <= eta <= 1 for
    # alpha=15 deg, Re=30.  Note: this introduces an input file
    # ordering dependency: this Function must appear *before* the two
    # functions below which use it since apparently proper dependency
    # resolution is not done in this scenario.
    type = PiecewiseLinear
    data_file = 'f.csv'
    format = 'columns'
  []
  [vel_x_exact]
    type = WedgeFunction
    var_num = 0
    mu = 1
    rho = 1
  []
  [vel_y_exact]
    type = WedgeFunction
    var_num = 1
    mu = 1
    rho = 1
  []
[]

[FunctorMaterials]
  [mu]
    type = ADGenericFunctorMaterial
    prop_names = 'mu'
    prop_values = '${mu}'
  []
[]

[Preconditioning]
  [SMP_NEWTON]
    type = SMP
    solve_type = NEWTON
  []
[]

[Executioner]
  type = Transient
  dt = 1.e-2
  dtmin = 1.e-2
  num_steps = 5
  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-13
  nl_abs_tol = 1e-11
  nl_max_its = 10
  l_tol = 1e-6
  l_max_its = 300
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/materials/ergun/ergun.i)

# This file simulates flow of fluid in a porous elbow for the purpose of verifying
# correct implementation of the various different solution variable sets. This input
# tests correct implementation of the primitive superficial variable set. Flow enters on the top
# and exits on the right. Because the purpose is only to test the equivalence of
# different equation sets, no solid energy equation is included.

porosity_left = 0.4
porosity_right = 0.6
pebble_diameter = 0.06

mu = 1.81e-5 # This has been increased to avoid refining the mesh
M = 28.97e-3
R = 8.3144598

# inlet mass flowrate, kg/s
mdot = -10.0

# inlet mass flux (superficial)
mflux_in_superficial = ${fparse mdot / (pi * 0.5 * 0.5)}

# inlet mass flux (interstitial)
mflux_in_interstitial = ${fparse mflux_in_superficial / porosity_left}

p_initial = 201325.0
T_initial = 300.0
rho_initial = ${fparse p_initial / T_initial * M / R}

vel_y_initial = ${fparse mflux_in_interstitial / rho_initial}
vel_x_initial = 0.0

superficial_vel_y_initial = ${fparse mflux_in_superficial / rho_initial}
superficial_vel_x_initial = 1e-12

# Computation parameters
velocity_interp_method = 'rc'
advected_interp_method = 'upwind'

# ==============================================================================
# GEOMETRY AND MESH
# ==============================================================================

[Mesh]
  [fmg]
    type = FileMeshGenerator
    file = 'ergun_in.e'
  []
  coord_type = RZ
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[GlobalParams]
  porosity = porosity
  pebble_diameter = ${pebble_diameter}
  fp = fp

  # rho for the kernels. Must match fluid property!
  rho = ${rho_initial}

  fv = true
  velocity_interp_method = ${velocity_interp_method}
  advected_interp_method = ${advected_interp_method}

  # behavior at time of test creation
  two_term_boundary_expansion = false
  rhie_chow_user_object = 'rc'
[]

# ==============================================================================
# VARIABLES AND KERNELS
# ==============================================================================

[Variables]
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${p_initial}
  []
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${superficial_vel_x_initial}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${superficial_vel_y_initial}
  []
[]

[FVKernels]
  # Mass Equation.
  [mass]
    type = PINSFVMassAdvection
    variable = 'pressure'
  []

  # Momentum x component equation.
  [vel_x_time]
    type = PINSFVMomentumTimeDerivative
    variable = 'superficial_vel_x'
    momentum_component = 'x'
  []
  [vel_x_advection]
    type = PINSFVMomentumAdvection
    variable = 'superficial_vel_x'
    momentum_component = 'x'
  []
  [vel_x_viscosity]
    type = PINSFVMomentumDiffusion
    variable = 'superficial_vel_x'
    momentum_component = 'x'
    mu = 'mu'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = 'superficial_vel_x'
    pressure = pressure
    momentum_component = 'x'
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = 'superficial_vel_x'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    momentum_component = 'x'
    speed = speed
    mu = 'mu'
  []

  # Momentum y component equation.
  [vel_y_time]
    type = PINSFVMomentumTimeDerivative
    variable = 'superficial_vel_y'
    momentum_component = 'y'
  []
  [vel_y_advection]
    type = PINSFVMomentumAdvection
    variable = 'superficial_vel_y'
    momentum_component = 'y'
  []
  [vel_y_viscosity]
    type = PINSFVMomentumDiffusion
    variable = 'superficial_vel_y'
    momentum_component = 'y'
    mu = 'mu'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = 'superficial_vel_y'
    pressure = pressure
    momentum_component = 'y'
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = 'superficial_vel_y'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    momentum_component = 'y'
    mu = 'mu'
    speed = speed
  []
  [gravity]
    type = PINSFVMomentumGravity
    variable = 'superficial_vel_y'
    gravity = '0 -9.81 0'
    momentum_component = 'y'
  []
[]

# ==============================================================================
# AUXVARIABLES AND AUXKERNELS
# ==============================================================================

[AuxVariables]
  [T_fluid]
    initial_condition = ${T_initial}
    order = CONSTANT
    family = MONOMIAL
  []
  [vel_x]
    initial_condition = ${fparse vel_x_initial}
    order = CONSTANT
    family = MONOMIAL
  []
  [vel_y]
    initial_condition = ${fparse vel_y_initial}
    order = CONSTANT
    family = MONOMIAL
  []
  [porosity_out]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [vel_x]
    type = FunctorAux
    variable = vel_x
    functor = vel_x_mat
  []
  [vel_y]
    type = FunctorAux
    variable = vel_y
    functor = vel_y_mat
  []
  [porosity_out]
    type = FunctorAux
    variable = porosity_out
    functor = porosity
  []
[]

# ==============================================================================
# FLUID PROPERTIES, MATERIALS AND USER OBJECTS
# ==============================================================================

[FluidProperties]
  [fp]
    type = IdealGasFluidProperties
    k = 0.0
    mu = ${mu}
    gamma = 1.4
    molar_mass = ${M}
  []
[]

[FunctorMaterials]
  [enthalpy]
    type = INSFVEnthalpyMaterial
    temperature = 'T_fluid'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = 'superficial_vel_x'
    superficial_vel_y = 'superficial_vel_y'
    porosity = porosity
    vel_x = vel_x_mat
    vel_y = vel_y_mat
  []
  [kappa]
    type = FunctorKappaFluid
  []
  [const_Fdrags_mat]
    type = FunctorErgunDragCoefficients
    porosity = porosity
  []
  [fluidprops]
    type = GeneralFunctorFluidProps
    mu_rampdown = mu_func
    porosity = porosity
    characteristic_length = ${pebble_diameter}
    T_fluid = 'T_fluid'
    pressure = 'pressure'
    speed = 'speed'
  []
[]

d = 0.05

[Functions]
  [mu_func]
    type = PiecewiseLinear
    x = '1 3 5 10 15 20'
    y = '1e5 1e4 1e3 1e2 1e1 1'
  []
  [real_porosity_function]
    type = ParsedFunction
    expression = 'if (x < 0.6 - ${d}, ${porosity_left}, if (x > 0.6 + ${d}, ${porosity_right},
        (x-(0.6-${d}))/(2*${d})*(${porosity_right}-${porosity_left}) + ${porosity_left}))'
  []
  [porosity]
    type = ParsedFunction
    expression = 'if (x < 0.6 - ${d}, ${porosity_left}, if (x > 0.6 + ${d}, ${porosity_right},
        (x-(0.6-${d}))/(2*${d})*(${porosity_right}-${porosity_left}) + ${porosity_left}))'
  []
[]

# ==============================================================================
# BOUNDARY CONDITIONS
# ==============================================================================

[FVBCs]
  [outlet_p]
    type = INSFVOutletPressureBC
    variable = 'pressure'
    function = ${p_initial}
    boundary = 'right'
  []

  ## No or Free slip BC
  [free-slip-wall-x]
    type = INSFVNaturalFreeSlipBC
    boundary = 'bottom wall_1 wall_2 left'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [free-slip-wall-y]
    type = INSFVNaturalFreeSlipBC
    boundary = 'bottom wall_1 wall_2 left'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  ## Symmetry
  [symmetry-x]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = 'mu'
    momentum_component = 'x'
  []
  [symmetry-y]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = 'mu'
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'left'
    variable = 'pressure'
  []

  ## inlet
  [inlet_vel_x]
    type = INSFVInletVelocityBC
    variable = 'superficial_vel_x'
    function = ${superficial_vel_x_initial}
    boundary = 'top'
  []
  [inlet_vel_y]
    type = INSFVInletVelocityBC
    variable = 'superficial_vel_y'
    function = ${superficial_vel_y_initial}
    boundary = 'top'
  []
[]
# ==============================================================================
# EXECUTION PARAMETERS
# ==============================================================================

[Executioner]
  type = Transient

  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -ksp_gmres_restart'
  petsc_options_value = 'asm      lu           NONZERO                   200'
  line_search = 'none'

  # Problem time parameters
  dtmin = 0.01
  dtmax = 2000
  end_time = 3000
  # must be the same as the fluid

  # Iterations parameters
  l_max_its = 50
  l_tol     = 1e-8
  nl_max_its = 25
  # nl_rel_tol = 5e-7
  nl_abs_tol = 2e-7

  # Automatic scaling
  automatic_scaling = true
  verbose = true

  [TimeStepper]
    type = IterationAdaptiveDT
    dt                 = 0.025
    cutback_factor     = 0.5
    growth_factor      = 2.0
  []

  # Steady state detection.
  steady_state_detection = true
  steady_state_tolerance = 1e-7
  steady_state_start_time = 400
[]

# ==============================================================================
# POSTPROCESSORS DEBUG AND OUTPUTS
# ==============================================================================

[Postprocessors]
  [mass_flow_in]
    type = VolumetricFlowRate
    boundary = 'top'
    vel_x = 'superficial_vel_x'
    vel_y = 'superficial_vel_y'
    advected_quantity = ${rho_initial}
    execute_on = 'INITIAL TIMESTEP_END'
  []
  [mass_flow_out]
    type = VolumetricFlowRate
    boundary = 'right'
    vel_x = 'superficial_vel_x'
    vel_y = 'superficial_vel_y'
    advected_quantity = ${rho_initial}
    execute_on = 'INITIAL TIMESTEP_END'
  []
  [p_in]
    type = SideAverageValue
    variable = pressure
    boundary = 'top'
  []
  [dP]
    type = LinearCombinationPostprocessor
    pp_names = 'p_in'
    pp_coefs = '1.0'
    b = ${fparse -p_initial}
  []
[]

[Outputs]
  exodus = true
  print_linear_residuals = false
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/2d/2d-segregated-velocity-rz.i)

mu = 2.6
rho = 1.0
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  coord_type = 'RZ'
  rz_coord_axis = X
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1.25'
    dy = '0.2'
    ix = '30'
    iy = '7'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_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 = 0.5
    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
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0.0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_y
    function = 0.0
  []
  [symmetry_u]
    type = INSFVSymmetryVelocityBC
    variable = vel_x
    boundary = 'bottom'
    momentum_component = 'x'
    mu = ${mu}
    u = vel_x
    v = vel_y
  []
  [symmetry_v]
    type = INSFVSymmetryVelocityBC
    variable = vel_y
    boundary = 'bottom'
    momentum_component = 'y'
    mu = ${mu}
    u = vel_x
    v = vel_y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1.4
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-15
  pressure_l_abs_tol = 1e-15
  momentum_l_tol = 0
  pressure_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  num_iterations = 100
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  print_fields = false
  continue_on_max_its = true
[]

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

(modules/navier_stokes/test/tests/finite_volume/ins/multiapp-scalar-transport/scalar-transport.i)

diff=1e-3
advected_interp_method='average'
velocity_interp_method='rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  active = 'rc'
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
    a_u = ax
    a_v = ay
  []

  [rc_bad]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[Variables]
  [scalar]
    type = INSFVScalarFieldVariable
  []
[]

[AuxVariables]
  [ax]
    type = MooseVariableFVReal
  []
  [ay]
    type = MooseVariableFVReal
  []
  [u]
    type = INSFVVelocityVariable
  []
  [v]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

[FVBCs]
  [inlet_scalar]
    type = FVDirichletBC
    boundary = 'left'
    variable = scalar
    value = 1
  []
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/iks/flow-around-square/flow-around-square.i)

# Water properties
mu = 1.0E-3
rho = 1000.0
k = 0.598
cp = 4186

# Solid properties
cp_s = 830
rho_s = 1680
k_s = 3.5

# Other parameters
p_outlet = 0
u_inlet = -1e-4
h_conv = 50

[Mesh]
  [generated_mesh]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 10
    ny = 10
    xmin = 0
    ymin = 0
    ymax = 0.1
    xmax = 0.1
  []
  [subdomain1]
    input = generated_mesh
    type = SubdomainBoundingBoxGenerator
    block_name = subdomain1
    bottom_left = '0.04 0.04 0'
    block_id = 1
    top_right = '0.06 0.06 0'
  []
  [interface]
    input = subdomain1
    type = SideSetsBetweenSubdomainsGenerator
    primary_block = 0
    paired_block = 1
    new_boundary = interface
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method = 'upwind'
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
    block = 0
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1e-4
    block = 0
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1e-4
    block = 0
  []
  [pressure]
    type = INSFVPressureVariable
    block = 0
  []
  [T]
    type = INSFVEnergyVariable
    initial_condition = 283.15
    scaling = 1e-5
    block = 0
  []
  [Ts]
    type = INSFVEnergyVariable
    initial_condition = 333.15
    scaling = 1e-5
    block = 1
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    rho = ${rho}
    block = 0
  []
  [u_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_x
    rho = ${rho}
    momentum_component = 'x'
    block = 0
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    rho = ${rho}
    momentum_component = 'x'
    block = 0
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
    block = 0
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    block = 0
  []
  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_y
    rho = ${rho}
    momentum_component = 'y'
    block = 0
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    rho = ${rho}
    momentum_component = 'y'
    block = 0
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    block = 0
  []
  [energy_time]
    type = INSFVEnergyTimeDerivative
    variable = T
    rho = ${rho}
    dh_dt = dh_dt
    block = 0
  []
  [temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = T
    block = 0
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T
    block = 0
  []
  [solid_energy_time]
    type = INSFVEnergyTimeDerivative
    variable = Ts
    rho = ${rho_s}
    dh_dt = dh_solid_dt
    block = 1
  []
  [solid_temp_conduction]
    type = FVDiffusion
    coeff = 'k_s'
    variable = Ts
    block = 1
  []
[]

[FVInterfaceKernels]
  [convection]
    type = FVConvectionCorrelationInterface
    variable1 = T
    variable2 = Ts
    subdomain1 = 0
    subdomain2 = 1
    boundary = interface
    h = ${h_conv}
    T_solid = Ts
    T_fluid = T
    wall_cell_is_bulk = true
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'top'
    variable = vel_x
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'top'
    variable = vel_y
    function = ${u_inlet}
  []
  [inlet_T]
    type = FVDirichletBC
    variable = T
    boundary = 'top'
    value = 283.15
  []
  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'left right interface'
    variable = vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'left right interface'
    variable = vel_y
    function = 0
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'bottom'
    variable = pressure
    function = '${p_outlet}'
  []
[]

[FunctorMaterials]
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp k'
    prop_values = '${cp} ${k}'
    block = 0
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T'
    rho = ${rho}
    block = 0
  []
  [solid_functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp_s k_s'
    prop_values = '${cp_s} ${k_s}'
    block = 1
  []
  [solid_ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'Ts'
    rho = ${rho_s}
    cp = ${cp_s}
    block = 1
    h = h_solid
  []
[]

[Executioner]
  type = Transient
  solve_type = NEWTON
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      100                lu           NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-8
  dt = 10
  end_time = 10
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/2d-rc-continuous.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = -1
    ymax = 1
    nx = 8
    ny = 8
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    porosity = porosity
    pressure = pressure
  []
[]

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

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
  []
[]

[ICs]
  [porosity_continuous]
    type = FunctionIC
    variable = porosity
    function = smooth_jump
  []
[]

[GlobalParams]
  porosity = porosity
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    pressure = pressure
    porosity = porosity
    momentum_component = 'y'
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    functor = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    functor = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [smooth_jump]
    type = ParsedFunction
    expression = '1 - 0.5 * 1 / (1 + exp(-30*(x-1))) - 0.01 * y'
  []

  # Output from compute-functions-2d.py
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '15.0*mu*(-1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*exp(30 - 30*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2))*exp(30 - 30*x)/(exp(30 - 30*x) + 1)^2 + 0.01*mu*((1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 0.0002*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3) - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 15.0*pi*exp(30 - 30*x)*sin((1/2)*x*pi)*sin((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) - 450.0*exp(30 - 30*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 900.0*exp(60 - 60*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^3*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 450.0*exp(60 - 60*x)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/((exp(30 - 30*x) + 1)^4*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3)) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 15.0*rho*exp(30 - 30*x)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) - 1/4*pi*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '0.01*mu*(-1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 15.0*mu*((1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*exp(30 - 30*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2))*exp(30 - 30*x)/(exp(30 - 30*x) + 1)^2 - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 0.01*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 0.0002*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3) - mu*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*(-1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 450.0*exp(30 - 30*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 7.5*pi*exp(30 - 30*x)*cos((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 900.0*exp(60 - 60*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^3*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + 450.0*exp(60 - 60*x)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^4*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^3)) - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1)) + 0.01*rho*sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2/(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2 + 15.0*rho*exp(30 - 30*x)*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/((exp(30 - 30*x) + 1)^2*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))^2) + (3/2)*pi*(-0.01*y + 1 - 0.5/(exp(30 - 30*x) + 1))*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    type = ElementL2FunctorError
    approximate = pressure
    exact = exact_p
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/2d/2d-segregated-velocity.i)

mu = 2.6
rho = 1.0
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '0.3'
    dy = '0.3'
    ix = '3'
    iy = '3'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system'
  previous_nl_solution_required = true
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 0.5
    solver_sys = u_system
    two_term_boundary_expansion = false
  []
  [v]
    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
  []
[]

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0.0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1.4
  []
  [zero-grad-pressure]
    type = FVFunctionNeumannBC
    variable = pressure
    boundary = 'top left bottom'
    function = 0.0
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  num_iterations = 150
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  print_fields = false
[]

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

(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/pwcns/channel-flow/2d-transient-gas.i)

# Fluid properties
mu = 'mu'
rho = 'rho'
k = 'k'

# Solid properties
cp_s = 2
rho_s = 4
k_s = 1e-2
h_fs = 10

# Operating conditions
u_inlet = 1
T_inlet = 200
p_outlet = 10
top_side_temperature = 150

# Numerical scheme
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = 0
    ymax = 1
    nx = 20
    ny = 5
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${p_outlet}
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = ${T_inlet}
  []
  [T_solid]
    type = MooseVariableFVReal
    initial_condition = 100
  []
[]

[AuxVariables]
  [porosity]
    type = MooseVariableFVReal
    initial_condition = 0.5
  []
[]

[FVKernels]
  [mass_time]
    type = PWCNSFVMassTimeDerivative
    variable = pressure
    porosity = 'porosity'
    drho_dt = 'drho_dt'
  []
  [mass]
    type = PWCNSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_time]
    type = WCNSFVMomentumTimeDerivative
    variable = superficial_vel_x
    rho = ${rho}
    drho_dt = 'drho_dt'
    momentum_component = 'x'
  []
  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_time]
    type = WCNSFVMomentumTimeDerivative
    variable = superficial_vel_y
    rho = ${rho}
    drho_dt = 'drho_dt'
    momentum_component = 'y'
  []
  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [energy_time]
    type = PINSFVEnergyTimeDerivative
    variable = T_fluid
    h = 'h'
    dh_dt = 'dh_dt'
    rho = ${rho}
    drho_dt = 'drho_dt'
    is_solid = false
    porosity = porosity
  []
  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    variable = T_fluid
    k = ${k}
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = T_fluid
    T_solid = T_solid
    h_solid_fluid = 'h_cv'
  []

  [solid_energy_time]
    type = PINSFVEnergyTimeDerivative
    variable = T_solid
    cp = ${cp_s}
    rho = ${rho_s}
    is_solid = true
    porosity = porosity
  []
  [solid_energy_diffusion]
    type = FVDiffusion
    variable = T_solid
    coeff = ${k_s}
  []
  [solid_energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_solid
    is_solid = true
    T_fluid = T_fluid
    T_solid = T_solid
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVDirichletBC
    variable = T_fluid
    value = ${T_inlet}
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [heated-side]
    type = FVDirichletBC
    boundary = 'top'
    variable = 'T_solid'
    value = ${top_side_temperature}
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = ${p_outlet}
  []
[]

[FluidProperties]
  [fp]
    type = IdealGasFluidProperties
    gamma = 1.4
  []
[]

[FunctorMaterials]
  [fluid_props_to_mat_props]
    type = GeneralFunctorFluidProps
    fp = fp
    pressure = 'pressure'
    T_fluid = 'T_fluid'
    speed = 'speed'

    # To initialize with a high viscosity
    mu_rampdown = 'mu_rampdown'

    # For porous flow
    characteristic_length = 1
    porosity = 'porosity'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv'
    prop_values = '${h_fs}'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    porosity = 'porosity'
    superficial_vel_x = 'superficial_vel_x'
    superficial_vel_y = 'superficial_vel_y'
  []
[]

[Functions]
  [mu_rampdown]
    type = PiecewiseLinear
    x = '1 2 3 4'
    y = '1e3 1e2 1e1 1'
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      100                lu           NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-10
  automatic_scaling = true

  end_time = 3.0
[]

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = VolumetricFlowRate
    boundary = 'right'
    advected_quantity = '1'
    advected_interp_method = ${advected_interp_method}
    vel_x = 'superficial_vel_x'
    vel_y = 'superficial_vel_y'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'right'
  []
  [solid-temp]
    type = ElementAverageValue
    variable = T_solid
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-average-no-slip.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1
    ymin = 0
    ymax = 4
    nx = 10
    ny = 40
  []
[]

[Problem]
  coord_type = 'RZ'
[]

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

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

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 1
  []
  [no-slip-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 0
  []
  [no-slip-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 0
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
  [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
  []
[]

[Postprocessors]
  [in]
    type = SideIntegralVariablePostprocessor
    variable = v
    boundary = 'bottom'
  []
  [out]
    type = SideIntegralVariablePostprocessor
    variable = v
    boundary = 'top'
  []
[]

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

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/2d/2d-segregated-outflow-bcs.i)

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

pressure_tag = "pressure_grad"

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 50
    ny = 10
  []
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system'
  previous_nl_solution_required = true
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 0.5
    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
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '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_u]
    type = INSFVMomentumAdvectionOutflowBC
    variable = vel_x
    u = vel_x
    v = vel_y
    boundary = 'right'
    momentum_component = 'x'
    rho = ${rho}
  []
  [outlet_v]
    type = INSFVMomentumAdvectionOutflowBC
    variable = vel_y
    u = vel_x
    v = vel_y
    boundary = 'right'
    momentum_component = 'y'
    rho = ${rho}
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.90
  pressure_variable_relaxation = 0.35
  num_iterations = 100
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  print_fields = false
[]

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

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated-comparison/segregated-nonlinear.i)

mu = 2.6
rho = 1.0
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '0.3'
    dy = '0.3'
    ix = '3'
    iy = '3'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_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 = 0.5
    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
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0.0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_y
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1.4
  []
  [zero-grad-pressure]
    type = FVFunctionNeumannBC
    variable = pressure
    boundary = 'top left bottom'
    function = 0.0
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  num_iterations = 2
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  print_fields = false
[]

[Outputs]
  exodus = true
  execute_on = TIMESTEP_END
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_eddy_viscosity_aux/mixing_length_eddy_viscosity.i)

von_karman_const = 0.41

H = 1 #halfwidth of the channel
L = 150

Re = 13700

rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}

advected_interp_method='upwind'
velocity_interp_method='rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${L}'
    dy = '0.667 0.333'
    ix = '100'
    iy = '10  1'
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_len]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_shear_stress]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_yplus]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [eddy_viscosity]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

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

  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = v
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = v
    rho = ${rho}
    mixing_length = mixing_len
    momentum_component = 'y'
    u = u
    v = v
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
[]

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_len
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
    delta = 0.5
  []
  [turbulent_viscosity]
    type = INSFVMixingLengthTurbulentViscosityAux
    variable = eddy_viscosity
    mixing_length = mixing_len
    u = u
    v = v
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [wall-u]
    type = INSFVWallFunctionBC
    variable = u
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = x
  []
  [wall-v]
    type = INSFVWallFunctionBC
    variable = v
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = y
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  [TimeStepper]
    type = IterationAdaptiveDT
    optimal_iterations = 6
    dt = 1e-3
  []
  nl_abs_tol = 1e-8
  end_time = 1e9
[]

[Outputs]
  [out]
    type = Exodus
    execute_on = 'final'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/bfs/BFS_ERCOFTAC.i)

##########################################################
# ERCOFTAC test case foe BFS
# Case Number: 031
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Equilibrium + Newton wall treatement
# SIMPLE solve
##########################################################

Re = 5100

rho = 1.0
bulk_u = 1.0
H = 1.0
mu = '${fparse rho * bulk_u * H/ Re}'

advected_interp_method = 'upwind'

pressure_tag = "pressure_grad"

### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09

### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / H}'

### Modeling parameters ###
bulk_wall_treatment = false
walls = 'bottom wall-side top'
wall_treatment = 'eq_incremental' # Options: eq_newton, eq_incremental, eq_linearized, neq

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${fparse 10.0*H} ${fparse 20.0*H}'
    dy = '${H} ${fparse 5*H}'
    ix = '8 16'
    iy = '2 8'
    subdomain_id = '
                    2 1
                    1 1
                  '
  []
  [corner_walls]
    type = SideSetsBetweenSubdomainsGenerator
    input = gen
    primary_block = '1'
    paired_block = '2'
    new_boundary = 'wall-side'
  []
  [delete_bottom]
    type = BlockDeletionGenerator
    input = corner_walls
    block = '2'
  []
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
  previous_nl_solution_required = true
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method = ${advected_interp_method}
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = ${bulk_u}
    solver_sys = u_system
    two_term_boundary_expansion = false
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 0
    solver_sys = v_system
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = 1e-8
    solver_sys = pressure_system
    two_term_boundary_expansion = false
  []
  [TKE]
    type = INSFVEnergyVariable
    solver_sys = TKE_system
    initial_condition = ${k_init}
  []
  [TKED]
    type = INSFVEnergyVariable
    solver_sys = TKED_system
    initial_condition = ${eps_init}
  []
[]

[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
  []

  [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
    k = TKE
    rho = ${rho}
    mu = ${mu}
    mu_t = 'mu_t'
    C1_eps = ${C1_eps}
    C2_eps = ${C2_eps}
    walls = ${walls}
    wall_treatment = ${wall_treatment}
  []
[]

[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_TKE]
    type = INSFVInletIntensityTKEBC
    boundary = 'left'
    variable = TKE
    u = vel_x
    v = vel_y
    intensity = ${intensity}
  []
  [inlet_TKED]
    type = INSFVMixingLengthTKEDBC
    boundary = 'left'
    variable = TKED
    k = TKE
    characteristic_length = '${fparse 2*H}'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    functor = 0
  []
  [walls-u]
    type = FVDirichletBC
    boundary = ${walls}
    variable = vel_x
    value = 0
  []
  [walls-v]
    type = FVDirichletBC
    boundary = ${walls}
    variable = vel_y
    value = 0
  []
  [walls_mu_t]
    type = INSFVTurbulentViscosityWallFunction
    boundary = ${walls}
    variable = mu_t
    u = vel_x
    v = vel_y
    rho = ${rho}
    mu = ${mu}
    mu_t = 'mu_t'
    k = 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}
    k = 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'
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  turbulence_systems = 'TKED_system TKE_system'

  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.7
  pressure_variable_relaxation = 0.3
  turbulence_equation_relaxation = '0.3 0.3'
  num_iterations = 500
  pressure_absolute_tolerance = 1e-12
  momentum_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'

  momentum_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
  pressure_l_tol = 0.0
  turbulence_l_tol = 0.0
  print_fields = false
  continue_on_max_its = true
[]

[Outputs]
  exodus = true
  [console]
    type = Console
    outlier_variable_norms = false
  []
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-effective.i)

mu = 1
rho = 1
cp = 1
u_inlet = 1
T_inlet = 200
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = 0
    ymax = 1
    nx = 100
    ny = 20
  []
  [left]
    type = ParsedSubdomainMeshGenerator
    input = gen
    combinatorial_geometry = 'x > 3 & x < 6'
    block_id = 1
  []
  [right]
    type = ParsedSubdomainMeshGenerator
    input = left
    combinatorial_geometry = 'x < 3'
    block_id = 2
  []
  [more-right]
    type = ParsedSubdomainMeshGenerator
    input = right
    combinatorial_geometry = 'x > 6'
    block_id = 3
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
[]

[AuxVariables]
  [T_solid]
    family = 'MONOMIAL'
    order = 'CONSTANT'
    fv = true
    initial_condition = 100
  []
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion_1]
    type = PINSFVEnergyAnisotropicDiffusion
    kappa = 'kappa'
    variable = T_fluid
    porosity = porosity
    block = '1 2'
  []
  [energy_diffusion_2]
    type = PINSFVEnergyAnisotropicDiffusion
    kappa = 'kappa'
    variable = T_fluid
    porosity = porosity
    block = '3'
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = T_fluid
    T_solid = T_solid
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  inactive = 'inlet-T-dirichlet'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVNeumannBC
    variable = T_fluid
    value = '${fparse u_inlet * rho * cp * T_inlet}'
    boundary = 'left'
  []
  [inlet-T-dirichlet]
    type = FVDirichletBC
    variable = T_fluid
    value = '${T_inlet}'
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.1
  []
[]

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv'
    prop_values = '1'
  []
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '${cp}'
  []
  [kappa]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'kappa'
    prop_values = '1e-3 1e-2 1e-1'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

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

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideAverageValue
    variable = superficial_vel_x
    boundary = 'right'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'right'
  []
  [solid-temp]
    type = ElementAverageValue
    variable = T_solid
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/postprocessors/pressure_drop/drop_insfv.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method = ${advected_interp_method}
  velocity_interp_method = ${velocity_interp_method}
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[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'
  []
[]

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

[AuxVariables]
  [advected_density]
    type = MooseVariableFVReal
    initial_condition = ${rho}
  []
[]

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

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

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

  [temp_advection]
    type = INSFVEnergyAdvection
    variable = temperature
    advected_interp_method = 'upwind'
  []
  [temp_source]
    type = FVBodyForce
    variable = temperature
    function = 10
    block = 1
  []
[]

[FVBCs]
  [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
  []
  [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
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'temperature'
    rho = ${rho}
  []
  [advected_material_property]
    type = ADGenericFunctorMaterial
    prop_names = 'advected_rho cp'
    prop_values ='${rho} 1'
  []
  [vel_functor]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'velocity'
    prop_values = 'u v 0'
  []
[]

[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]
  [pdrop_total]
    type = PressureDrop
    pressure = pressure
    upstream_boundary = 'bottom'
    downstream_boundary = 'top'
    boundary = 'top bottom'
  []
  [pdrop_mid1]
    type = PressureDrop
    pressure = pressure
    upstream_boundary = 'bottom'
    downstream_boundary = 'internal_bot'
    boundary = 'bottom internal_bot'
  []
  [pdrop_mid2]
    type = PressureDrop
    pressure = pressure
    upstream_boundary = 'internal_bot'
    downstream_boundary = 'internal_top'
    boundary = 'internal_top internal_bot'
  []
  [pdrop_mid3]
    type = PressureDrop
    pressure = pressure
    upstream_boundary = 'internal_top'
    downstream_boundary = 'top'
    boundary = 'top internal_top'
  []
  [sum_drops]
    type = ParsedPostprocessor
    expression = 'pdrop_mid1 + pdrop_mid2 + pdrop_mid3'
    pp_names = 'pdrop_mid1 pdrop_mid2 pdrop_mid3'
  []

  [p_upstream]
    type = SideAverageValue
    variable = pressure
    boundary = 'bottom'
  []
  [p_downstream]
    type = SideAverageValue
    variable = pressure
    boundary = 'top'
  []
[]

[Outputs]
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/materials/2d-rc.i)

mu = 0.01
rho = 2000
u_inlet = 1

advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = 0
    ymax = 1
    nx = 10
    ny = 6
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []

  [speed_output]
    type = MooseVariableFVReal
  []

  [vel_x_output]
    type = MooseVariableFVReal
  []

  [vel_y_output]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [speed]
    type = FunctorAux
    variable = 'speed_output'
    functor = 'speed'
  []

  [vel_x]
    type = ADFunctorVectorElementalAux
    variable = 'vel_x_output'
    functor = 'velocity'
    component = 0
  []

  [vel_y]
    type = ADFunctorVectorElementalAux
    variable = 'vel_y_output'
    functor = 'velocity'
    component = 1
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.1
  []
[]

[FunctorMaterials]
  # Testing this object
  [var_mat]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = 'superficial_vel_x'
    superficial_vel_y = 'superficial_vel_y'
    porosity = porosity
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-11
[]

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideAverageValue
    variable = superficial_vel_x
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/fvbcs/wall_function/Re_t395.i)

von_karman_const = 0.41

H = 1 #halfwidth of the channel
L = 150

Re = 13700

rho = 1
bulk_u = 1
mu = ${fparse rho * bulk_u * 2 * H / Re}

advected_interp_method='upwind'
velocity_interp_method='rc'

[GlobalParams]
  two_term_boundary_expansion = true
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${L}'
    dy = '0.667 0.333'
    ix = '200'
    iy = '10  1'
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_len]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_shear_stress]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_yplus]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

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

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

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

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_len
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
  []
  [wall_shear_stress]
    type = WallFunctionWallShearStressAux
    variable = wall_shear_stress
    walls = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
  []
  [wall_yplus]
    type = WallFunctionYPlusAux
    variable = wall_yplus
    walls = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [wall-u]
    type = INSFVWallFunctionBC
    variable = u
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = x
  []
  [wall-v]
    type = INSFVWallFunctionBC
    variable = v
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = y
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = u
    u = u
    v = v
    mu = total_viscosity
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = v
    u = u
    v = v
    mu = total_viscosity
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[FunctorMaterials]
  [total_viscosity]
    type = MixingLengthTurbulentViscosityFunctorMaterial
    u = 'u'                             #computes total viscosity = mu_t + mu
    v = 'v'                             #property is called total_viscosity
    mixing_length = mixing_len
    mu = ${mu}
    rho = ${rho}
  []
[]

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

[Outputs]
  exodus = true
[]

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

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method = ${advected_interp_method}
  velocity_interp_method = ${velocity_interp_method}
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[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'
  []
[]

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

[AuxVariables]
  [advected_density]
    type = MooseVariableFVReal
    initial_condition = ${rho}
  []
[]

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

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

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

  [temp_advection]
    type = INSFVEnergyAdvection
    variable = temperature
    advected_interp_method = 'upwind'
  []
  [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
    momentum_component = 'x'
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = v
    momentum_component = 'y'
  []
  [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
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'temperature'
    rho = ${rho}
  []
  [advected_material_property]
    type = ADGenericFunctorMaterial
    prop_names = 'advected_rho cp'
    prop_values ='${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_quantity = advected_density
  []
  [inlet_mass_constant]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
  [inlet_mass_matprop]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = 'advected_rho'
  []
  [mid1_mass]
    type = VolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
  [mid2_mass]
    type = VolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
  [outlet_mass]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []

  [inlet_momentum_x]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = u
  []

  [inlet_momentum_y]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = v
  []

  [mid1_advected_energy]
    type = VolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_quantity = 'rho_cp_temp'
    advected_interp_method = 'upwind'
  []
  [mid2_advected_energy]
    type = VolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_quantity = 'rho_cp_temp'
    advected_interp_method = 'upwind'
  []
  [outlet_advected_energy]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_quantity = 'rho_cp_temp'
    advected_interp_method = 'upwind'
  []
[]

[Outputs]
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/discontinuous-body-forces.i)

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

[GlobalParams]
  two_term_boundary_expansion = true
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 9
  []
  [subdomain]
    type = SubdomainBoundingBoxGenerator
    bottom_left = '5 -1 0'
    top_right = '10 1 0'
    block_id = 1
    input = gen
  []
[]

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

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_friction_linear]
    type = PINSFVMomentumFriction
    variable = u
    Darcy_name = friction_coefficient
    momentum_component = 'x'
    block = '1'
    standard_friction_formulation = false
    rho = ${rho}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_friction_linear]
    type = PINSFVMomentumFriction
    variable = v
    Darcy_name = friction_coefficient
    momentum_component = 'y'
    block = '1'
    standard_friction_formulation = false
    rho = ${rho}
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[FunctorMaterials]
  [friction_coefficient]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'friction_coefficient'
    prop_values = '25 25 25'
  []
[]

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

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-scalar-transport.i)

mu = 1
rho = 1
k = 1e-3
diff = 1e-3
cp = 1
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[AuxVariables]
  [U]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

[AuxKernels]
  [mag]
    type = VectorMagnitudeAux
    variable = U
    x = vel_x
    y = vel_y
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
  [scalar]
    type = INSFVScalarFieldVariable
  []
[]

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

  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []

  [scalar_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_diffusion]
    type = FVDiffusion
    coeff = ${diff}
    variable = scalar
  []
  [scalar_src]
    type = FVBodyForce
    variable = scalar
    value = 0.1
  []
  [scalar_coupled_source]
    type = FVCoupledForce
    variable = scalar
    v = U
    coef = 0.1
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = 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_t]
    type = FVDirichletBC
    boundary = 'left'
    variable = T_fluid
    value = 1
  []
  [inlet_scalar]
    type = FVDirichletBC
    boundary = 'left'
    variable = scalar
    value = 1
  []
[]

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

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

[Outputs]
  exodus = true
  csv = true
[]

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

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

[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
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method = ${advected_interp_method}
  velocity_interp_method = ${velocity_interp_method}
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
    porosity = porosity
  []
[]

[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
    rho = ${rho}
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    force_boundary_execution = true
    porosity = porosity
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    force_boundary_execution = true
    porosity = porosity
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [temp_advection]
    type = PINSFVEnergyAdvection
    variable = temperature
    advected_interp_method = 'upwind'
  []
  [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
    momentum_component = 'x'
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = v
    momentum_component = 'y'
  []
  [axis-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
  []
  [axis-v]
    type = PINSFVSymmetryVelocityBC
    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
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'temperature'
    rho = ${rho}
  []
  [advected_material_property]
    type = ADGenericFunctorMaterial
    prop_names = 'advected_rho cp'
    prop_values ='${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_quantity = advected_density
  []
  [inlet_mass_constant]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
  [inlet_mass_matprop]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = 'advected_rho'
  []
  [mid1_mass]
    type = VolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
  [mid2_mass]
    type = VolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
  [outlet_mass]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []

  [inlet_momentum_x]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = u
  []

  [inlet_momentum_y]
    type = VolumetricFlowRate
    boundary = bottom
    vel_x = u
    vel_y = v
    advected_quantity = v
  []

  [mid1_advected_energy]
    type = VolumetricFlowRate
    boundary = internal_bot
    vel_x = u
    vel_y = v
    advected_quantity = 'rho_cp_temp'
    advected_interp_method = 'upwind'
  []
  [mid2_advected_energy]
    type = VolumetricFlowRate
    boundary = internal_top
    vel_x = u
    vel_y = v
    advected_quantity = 'rho_cp_temp'
    advected_interp_method = 'upwind'
  []
  [outlet_advected_energy]
    type = VolumetricFlowRate
    boundary = top
    vel_x = u
    vel_y = v
    advected_quantity = 'rho_cp_temp'
    advected_interp_method = 'upwind'
  []
[]

[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'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip.i)

mu = 1.1
rho = 1.1
l = 2
U = 1
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = ${fparse -l / 2}
    ymax = ${fparse l / 2}
    nx = 100
    ny = 20
  []
  uniform_refine = 0
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '${U}'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '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'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  nl_rel_tol = 1e-12
[]

[Preconditioning]
  active = FSP
  [FSP]
    type = FSP
    # It is the starting point of splitting
    topsplit = 'up' # 'up' should match the following block name
    [up]
      splitting = 'u p' # 'u' and 'p' are the names of subsolvers
      splitting_type  = schur
      # Splitting type is set as schur, because the pressure part of Stokes-like systems
      # is not diagonally dominant. CAN NOT use additive, multiplicative and etc.
      #
      # Original system:
      #
      # | Auu Aup | | u | = | f_u |
      # | Apu 0   | | p |   | f_p |
      #
      # is factorized into
      #
      # |I             0 | | Auu  0|  | I  Auu^{-1}*Aup | | u | = | f_u |
      # |Apu*Auu^{-1}  I | | 0   -S|  | 0  I            | | p |   | f_p |
      #
      # where
      #
      # S = Apu*Auu^{-1}*Aup
      #
      # The preconditioning is accomplished via the following steps
      #
      # (1) p* = f_p - Apu*Auu^{-1}f_u,
      # (2) p = (-S)^{-1} p*
      # (3) u = Auu^{-1}(f_u-Aup*p)

      petsc_options_iname = '-pc_fieldsplit_schur_fact_type  -pc_fieldsplit_schur_precondition -ksp_gmres_restart -ksp_rtol -ksp_type'
      petsc_options_value = 'full                            selfp                             300                1e-4      fgmres'
    []
    [u]
      vars = 'vel_x vel_y'
      petsc_options_iname = '-pc_type -pc_hypre_type -ksp_type -ksp_rtol -ksp_gmres_restart -ksp_pc_side'
      petsc_options_value = 'hypre    boomeramg      gmres    5e-1      300                 right'
    []
    [p]
      vars = 'pressure'
      petsc_options_iname = '-ksp_type -ksp_gmres_restart -ksp_rtol -pc_type -ksp_pc_side'
      petsc_options_value = 'gmres    300                5e-1      jacobi    right'
    []
  []
  [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/pins/channel-flow/segregated/2d-heated.i)

mu = 1
rho = 1
k = 1e-3
cp = 1
u_inlet = 1
T_inlet = 200
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '5 5'
    dy = '1.0'
    ix = '10 10'
    iy = '5'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolatorSegregated
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system energy_system solid_energy_system'
  previous_nl_solution_required = true
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
    solver_sys = u_system
    two_term_boundary_expansion = false
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
    solver_sys = v_system
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = false
    solver_sys = pressure_system
  []
  [T_fluid]
    type = INSFVEnergyVariable
    two_term_boundary_expansion = false
    solver_sys = energy_system
    initial_condition = 200
  []
  [T_solid]
    type = MooseVariableFVReal
    two_term_boundary_expansion = false
    solver_sys = solid_energy_system
    initial_condition = 200
  []
[]

[AuxVariables]
  [porosity]
    type = MooseVariableFVReal
    initial_condition = 0.5
    two_term_boundary_expansion = false
  []
[]

[FVKernels]
  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
    extra_vector_tags = ${pressure_tag}
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
    extra_vector_tags = ${pressure_tag}
  []

  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []

  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
    boundaries_to_force = bottom
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    k = ${k}
    variable = T_fluid
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []

  [solid_energy_diffusion]
    type = FVDiffusion
    coeff = ${k}
    variable = T_solid
  []
  [solid_energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_solid
    is_solid = true
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVDirichletBC
    variable = T_fluid
    value = ${T_inlet}
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [heated-side]
    type = FVDirichletBC
    boundary = 'top'
    variable = 'T_solid'
    value = 250
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.1
  []
[]

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv cp'
    prop_values = '0.1 ${cp}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  energy_l_abs_tol = 1e-14
  solid_energy_l_abs_tol = 1e-14
  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'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.4
  energy_equation_relaxation = 1.0
  num_iterations = 160
  pressure_absolute_tolerance = 1e-12
  momentum_absolute_tolerance = 1e-12
  energy_absolute_tolerance = 1e-12
  solid_energy_absolute_tolerance = 1e-12
  print_fields = false
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/pressure-interpolation-corrected.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  Darcy_name = 'Darcy_coefficient'
  Forchheimer_name = 'Forchheimer_coefficient'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    porosity = porosity
    pressure = pressure
    smoothing_layers = 2
  []
[]

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

[AuxVariables]
  [eps_out]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [eps_out]
    type = FunctorAux
    variable = eps_out
    functor = porosity
    execute_on = 'timestep_end'
  []
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
  [u_drag]
    type = PINSFVMomentumFriction
    variable = u
    momentum_component = 'x'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []
  [u_correction]
    type = PINSFVMomentumFrictionCorrection
    variable = u
    momentum_component = 'x'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    pressure = pressure
    porosity = porosity
    momentum_component = 'y'
  []
  [v_drag]
    type = PINSFVMomentumFriction
    variable = v
    momentum_component = 'y'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []
  [v_correction]
    type = PINSFVMomentumFrictionCorrection
    variable = v
    momentum_component = 'y'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    functor = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    functor = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[FunctorMaterials]
  [darcy]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Darcy_coefficient Forchheimer_coefficient'
    prop_values = '${darcy} ${darcy} ${darcy} ${forch} ${forch} ${forch}'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = u
    superficial_vel_y = v
    porosity = porosity
  []
[]

[Functions]
  [porosity]
    type = ParsedFunction
    expression = '.5 + .1 * sin(pi * x / 4) * cos(pi * y / 4)'
  []

  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = 'darcy*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) + (1/2)*forch*rho*sqrt(sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2 + sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.1*pi^2*sin((1/4)*x*pi)*sin((1/4)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.025*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.025*pi^2*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.1*pi^2*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/2)*y*pi)*cos((1/4)*x*pi)^2*cos((1/2)*x*pi)*cos((1/4)*y*pi)^2/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) + 0.025*pi*mu*(0.1*pi*sin((1/4)*x*pi)*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + (1/2)*pi*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*(-0.1*pi*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*sin((1/2)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.1*pi*rho*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.1*pi*rho*sin((1/2)*y*pi)^2*cos((1/4)*x*pi)*cos((1/2)*x*pi)^2*cos((1/4)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/4*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho darcy forch'
    symbol_values = '${mu} ${rho} ${darcy} ${forch}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_v]
    type = ParsedFunction
    expression = 'darcy*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) + (1/2)*forch*rho*sqrt(sin((1/4)*x*pi)^2*cos((1/2)*y*pi)^2 + sin((1/2)*y*pi)^2*cos((1/2)*x*pi)^2)*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(-0.1*pi^2*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*sin((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.025*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/4*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) - mu*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*(0.025*pi^2*sin((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.05*pi^2*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + 0.01*pi^2*sin((1/4)*x*pi)*cos((1/4)*x*pi)^2*cos((1/4)*y*pi)^2*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^3 - 1/16*pi^2*sin((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)) + 0.025*pi*mu*(0.1*pi*sin((1/4)*x*pi)^2*sin((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 1/2*pi*sin((1/4)*x*pi)*sin((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*sin((1/4)*x*pi)*sin((1/4)*y*pi) - 0.025*pi*mu*(-0.1*pi*sin((1/4)*x*pi)*cos((1/4)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 + (1/4)*pi*cos((1/4)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5))*cos((1/4)*x*pi)*cos((1/4)*y*pi) + 0.1*pi*rho*sin((1/4)*x*pi)^3*sin((1/4)*y*pi)*cos((1/2)*y*pi)^2/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - 0.1*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/4)*y*pi)*cos((1/2)*y*pi)/(0.2*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 1)^2 - pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) - 1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)/(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5) + (3/2)*pi*(0.1*sin((1/4)*x*pi)*cos((1/4)*y*pi) + 0.5)*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
    symbol_names = 'mu rho darcy forch'
    symbol_values = '${mu} ${rho} ${darcy} ${forch}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  exodus = false
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    type = ElementL2FunctorError
    approximate = pressure
    exact = exact_p
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/hydraulic-separators/separator-no-jump.i)

# This test describes a test where three parallel channels are
# separated using flow separators that act as slip boundary conditions.
# The different channels have different friction factors
# meaning that we expect different pressure drops.
# Channel 1 expected drop (analytic, Forchheimer only): 5.50E-03 Pa
# Channel 2 expected drop (analytic, Forchheimer only): 4.40E-02 Pa
# Channel 3 expected drop (analytic, Forchheimer only): 1.49E-01 Pa

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

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1'
    dy = '0.25 0.25 0.25'
    ix = '5'
    iy = '2 2 2'
    subdomain_id = '1 2 3'
  []
  [separator-1]
    type = SideSetsBetweenSubdomainsGenerator
    new_boundary = 'separator-1'
    primary_block = 1
    paired_block = 2
    input = mesh
  []
  [separator-2]
    type = SideSetsBetweenSubdomainsGenerator
    new_boundary = 'separator-2'
    primary_block = 2
    paired_block = 3
    input = separator-1
  []
  [inlet-1]
    type = ParsedGenerateSideset
    input = separator-2
    combinatorial_geometry = 'y < 0.25 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-1
  []
  [inlet-2]
    type = ParsedGenerateSideset
    input = inlet-1
    combinatorial_geometry = 'y > 0.25 & y < 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-2
  []
  [inlet-3]
    type = ParsedGenerateSideset
    input = inlet-2
    combinatorial_geometry = 'y > 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-3
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0.1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
  []
  [pressure]
    type = BernoulliPressureVariable
    u = u
    v = v
    rho = ${rho}
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    momentum_component = 'x'
    mu = ${mu}
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    pressure = pressure
    momentum_component = 'x'
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_x
    momentum_component = 'x'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    momentum_component = 'y'
    mu = ${mu}
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    pressure = pressure
    momentum_component = 'y'
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_y
    momentum_component = 'y'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
  []
[]

[FVBCs]
  [inlet-u-1]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1'
    variable = superficial_vel_x
    function = '0.1'
  []
  [inlet-u-2]
    type = INSFVInletVelocityBC
    boundary = 'inlet-2'
    variable = superficial_vel_x
    function = '0.2'
  []
  [inlet-u-3]
    type = INSFVInletVelocityBC
    boundary = 'inlet-3'
    variable = superficial_vel_x
    function = '0.3'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1 inlet-2 inlet-3'
    variable = superficial_vel_y
    function = 0
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-u]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_x
    momentum_component = 'x'
  []

  [separator-v]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-p]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = pressure
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  [const]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '1.0'
  []
  [darcy-1]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '1.0 1.0 1.0'
    block = 1
  []
  [darcy-2]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '2.0 2.0 2.0'
    block = 2
  []
  [darcy-3]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '3.0 3.0 3.0'
    block = 3
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = ' lu       NONZERO               1e-10'
  line_search = 'none'
  nl_rel_tol = 1e-10
  nl_max_its = 10
[]

[Postprocessors]
  [inlet_p1]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'inlet-1'
  []
  [inlet_p2]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'inlet-2'
  []
  [inlet_p3]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'inlet-3'
  []
  [drop-1]
    type = ParsedPostprocessor
    expression = 'inlet_p1 - outlet'
    pp_names = 'inlet_p1'
    constant_names = 'outlet'
    constant_expressions = '0.4'
  []
  [drop-2]
    type = ParsedPostprocessor
    expression = 'inlet_p2 - outlet'
    pp_names = 'inlet_p2'
    constant_names = 'outlet'
    constant_expressions = '0.4'
  []
  [drop-3]
    type = ParsedPostprocessor
    expression = 'inlet_p3 - outlet'
    pp_names = 'inlet_p3'
    constant_names = 'outlet'
    constant_expressions = '0.4'
  []
[]

[Outputs]
  csv = true
  execute_on = final
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-rz-symmetry.i)

mu=1.1
rho=1.1
offset=0e0

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = ${offset}
    xmax = ${fparse 1 + offset}
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[Problem]
  fv_bcs_integrity_check = false
  coord_type = 'RZ'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  two_term_boundary_expansion = true
  advected_interp_method = 'average'
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
  []
  [v]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[ICs]
  [u]
    type = FunctionIC
    function = 'exact_u'
    variable = u
  []
  [v]
    type = FunctionIC
    function = 'exact_v'
    variable = v
  []
  [pressure]
    type = FunctionIC
    function = 'exact_p'
    variable = pressure
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[FVBCs]
  [u_wall]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'right'
    function = 'exact_u'
  []
  [v_wall]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'right'
    function = 'exact_v'
  []
  [p]
    type = INSFVOutletPressureBC
    variable = pressure
    function = 'exact_p'
    boundary = 'top'
  []
  [inlet_u]
    type = INSFVInletVelocityBC
    variable = u
    function = 'exact_u'
    boundary = 'bottom'
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = v
    function = 'exact_v'
    boundary = 'bottom'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin(x*pi)^2*cos(y*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = 'pi^2*mu*sin(x*pi)^2*cos(y*pi) - 2*pi*rho*sin(x*pi)^2*sin(y*pi)*cos(x*pi)*cos(y*pi) - pi*sin(x*pi)*cos(1.6*y) + (4*x*pi*rho*sin(x*pi)^3*cos(x*pi)*cos(y*pi)^2 + rho*sin(x*pi)^4*cos(y*pi)^2)/x - (-2*x*pi^2*mu*sin(x*pi)^2*cos(y*pi) + 2*x*pi^2*mu*cos(x*pi)^2*cos(y*pi) + 2*pi*mu*sin(x*pi)*cos(x*pi)*cos(y*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos(y*pi)'
  []
  [forcing_v]
    type = ParsedFunction
    expression = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1.6*sin(1.6*y)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*cos(y*pi)^2 + 2*x*pi*rho*sin(x*pi)*cos(x*pi)^2*cos(y*pi)^2 + rho*sin(x*pi)^2*cos(x*pi)*cos(y*pi)^2)/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'cos(1.6*y)*cos(x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*cos(x*pi)*cos(y*pi) + rho*sin(x*pi)^2*cos(y*pi))/x'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu       NONZERO               superlu_dist'
  line_search = 'none'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-12
[]

[Outputs]
  exodus = false
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/1d-rc.i)

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

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '30 30'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1
  []
[]

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

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/hydraulic-separators/separator-mixing.i)

# This test is designed to check for energy conservation
# in separated channels. The three inlet temperatures should be
# preserved at the outlets.

rho=1.1
mu=1e-4
k=2.1
cp=5.5
advected_interp_method='upwind'
velocity_interp_method='rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '0.25 1.0 0.25'
    dy = '0.25 0.25 0.25'
    ix = '4 20 4'
    iy = '5 5 5'
    subdomain_id = '1 2 5 1 3 5 1 4 5'
  []
  [separator-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    primary_block = '2'
    paired_block = '3'
    new_boundary = 'separator-1'
  []
  [separator-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = separator-1
    primary_block = '3'
    paired_block = '4'
    new_boundary = 'separator-2'
  []
  [jump-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = separator-2
    primary_block = '1'
    paired_block = '2'
    new_boundary = jump-1
  []
  [jump-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = jump-1
    primary_block = '1'
    paired_block = '3'
    new_boundary = jump-2
  []
  [jump-3]
    type = SideSetsBetweenSubdomainsGenerator
    input = jump-2
    primary_block = '1'
    paired_block = '4'
    new_boundary = jump-3
  []
  [outlet-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = jump-3
    primary_block = '2'
    paired_block = '5'
    new_boundary = outlet-1
  []
  [outlet-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = outlet-1
    primary_block = '3'
    paired_block = '5'
    new_boundary = outlet-2
  []
  [outlet-3]
    type = SideSetsBetweenSubdomainsGenerator
    input = outlet-2
    primary_block = '4'
    paired_block = '5'
    new_boundary = outlet-3
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0.1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
  []
  [pressure]
    type = BernoulliPressureVariable
    u = superficial_vel_x
    v = superficial_vel_y
    rho = ${rho}
    pressure_drop_sidesets = 'jump-1 jump-2 jump-3 outlet-1 outlet-2 outlet-3'
    pressure_drop_form_factors = '0.1 0.2 0.3 0.1 0.2 0.3'
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = 300
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    momentum_component = 'x'
    mu = ${mu}
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    pressure = pressure
    momentum_component = 'x'
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_x
    momentum_component = 'x'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    momentum_component = 'y'
    mu = ${mu}
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    pressure = pressure
    momentum_component = 'y'
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_y
    momentum_component = 'y'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
  []

  [temp_conduction]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
  []
  [temp_source]
    type = FVBodyForce
    variable = T_fluid
    function = heating
    block = '2 3 4'
  []
[]

[Functions]
  [heating]
    type = ParsedFunction
    expression = 'if(y<0.25, 10, if(y<0.5, 20, 30))'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = '0.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []

  [inlet-T]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'left'
    value = 300
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-u]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_x
    momentum_component = 'x'
  []

  [separator-v]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-p]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = pressure
  []

  [separator-T]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = T_fluid
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  [porosity]
    type = ADPiecewiseByBlockFunctorMaterial
    prop_name = porosity
    subdomain_to_prop_value = '1 0.8
                               2 0.7
                               3 0.6
                               4 0.5
                               5 0.8'
  []
  [darcy-1]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '1.0 1.0 1.0'
    block = '1 5'
  []
  [darcy-2]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '3.0 3.0 3.0'
    block = 2
  []
  [darcy-3]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '1.5 1.5 1.5'
    block = 3
  []
  [darcy-4]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Forchheimer_coefficient'
    prop_values = '0.75 0.75 0.75'
    block = 4
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T_fluid'
    rho = ${rho}
    cp = ${cp}
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = ' lu       NONZERO               1e-10'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [outlet_T1]
    type = SideAverageValue
    variable = 'T_fluid'
    boundary = 'right'
  []
[]

[Outputs]
  csv = true
  execute_on = final
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-2d.i)

rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1'
    dy = '0.5'
    ix = '3 3'
    iy = '2'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    porosity = porosity
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [v]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = BernoulliPressureVariable
    u = u
    v = v
    porosity = porosity
    rho = ${rho}
  []
[]

[AuxVariables]
  [porosity]
    type = PiecewiseConstantVariable
  []
[]

[ICs]
  [porosity_1]
    type = ConstantIC
    variable = porosity
    block = 1
    value = 1
  []
  [porosity_2]
    type = ConstantIC
    variable = porosity
    block = 2
    value = 0.5
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    pressure = pressure
    momentum_component = 'y'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = u
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = v
    momentum_component = 'y'
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-transient.i)

# Fluid properties
mu = 1
rho = 1
cp = 1
k = 1e-3

# Solid properties
cp_s = 2
rho_s = 4
k_s = 1e-2
h_fs = 10

# Operating conditions
u_inlet = 1
T_inlet = 200
p_outlet = 10
top_side_temperature = 150

# Numerical scheme
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = 0
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${p_outlet}
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
  [T_solid]
    type = MooseVariableFVReal
    initial_condition = 100
  []
[]

[AuxVariables]
  [porosity]
    type = MooseVariableFVReal
    initial_condition = 0.5
  []
[]

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

  [u_time]
    type = INSFVMomentumTimeDerivative
    variable = superficial_vel_x
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = superficial_vel_y
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [energy_time]
    type = PINSFVEnergyTimeDerivative
    variable = T_fluid
    cp = ${cp}
    rho = ${rho}
    is_solid = false
    porosity = porosity
  []
  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    variable = T_fluid
    k = ${k}
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []

  [solid_energy_time]
    type = PINSFVEnergyTimeDerivative
    variable = T_solid
    cp = ${cp_s}
    rho = ${rho_s}
    is_solid = true
    porosity = porosity
  []
  [solid_energy_diffusion]
    type = FVDiffusion
    variable = T_solid
    coeff = ${k_s}
  []
  [solid_energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_solid
    is_solid = true
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVNeumannBC
    variable = T_fluid
    value = '${fparse u_inlet * rho * cp * T_inlet}'
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [heated-side]
    type = FVDirichletBC
    boundary = 'top'
    variable = 'T_solid'
    value = ${top_side_temperature}
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = ${p_outlet}
  []
[]

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv'
    prop_values = '${h_fs}'
  []
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '${cp}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

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

  end_time = 1.5
[]

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideAverageValue
    variable = superficial_vel_x
    boundary = 'right'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'right'
  []
  [solid-temp]
    type = ElementAverageValue
    variable = T_solid
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/2d/2d-segregated-velocity-rz-slip.i)

mu = 2.6
rho = 1.0
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  coord_type = 'RZ'
  rz_coord_axis = X
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1.25'
    dy = '0.2'
    ix = '30'
    iy = '7'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_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 = 0.5
    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
  []
[]

[FVKernels]
  inactive = 'u_friction v_friction'
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = vel_x
    u = vel_x
    v = vel_y
    momentum_component = 'x'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    standard_friction_formulation = false
    rho = ${rho}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = vel_y
    u = vel_x
    v = vel_y
    momentum_component = 'y'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    standard_friction_formulation = false
    rho = ${rho}
  []
  [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
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '0.0'
  []
  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = vel_y
    momentum_component = 'y'
  []
  [symmetry_u]
    type = INSFVSymmetryVelocityBC
    variable = vel_x
    boundary = 'bottom'
    momentum_component = 'x'
    mu = ${mu}
    u = vel_x
    v = vel_y
  []
  [symmetry_v]
    type = INSFVSymmetryVelocityBC
    variable = vel_y
    boundary = 'bottom'
    momentum_component = 'y'
    mu = ${mu}
    u = vel_x
    v = vel_y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1.4
  []
[]

[FunctorMaterials]
  [darcy]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Darcy_coefficient Forchheimer_coefficient'
    prop_values = '0.1 0.1 0.1 0.1 0.1 0.1'
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.5
  pressure_variable_relaxation = 0.3
  num_iterations = 150
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  print_fields = false
  continue_on_max_its = true
[]

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

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/cartesian-version/2d-rc-no-slip-walls.i)

mu=1.1
rho=1.1

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = -1
    xmax = 1
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  two_term_boundary_expansion = true
  advected_interp_method = 'average'
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
  []
  [v]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[ICs]
  [u]
    type = FunctionIC
    function = 'exact_u'
    variable = u
  []
  [v]
    type = FunctionIC
    function = 'exact_v'
    variable = v
  []
  [pressure]
    type = FunctionIC
    function = 'exact_p'
    variable = pressure
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[FVBCs]
  [u_walls]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'left right'
    function = 'exact_u'
  []
  [v_walls]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'left right'
    function = 'exact_v'
  []
  [p]
    type = INSFVOutletPressureBC
    variable = pressure
    function = 'exact_p'
    boundary = 'top'
  []
  [inlet_u]
    type = INSFVInletVelocityBC
    variable = u
    function = 'exact_u'
    boundary = 'bottom'
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = v
    function = 'exact_v'
    boundary = 'bottom'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin(x*pi)*cos(y*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '2*pi^2*mu*sin(x*pi)*cos(y*pi) - 2*pi*rho*sin(x*pi)*sin(y*pi)*cos(1.3*x)*cos(y*pi) + 2*pi*rho*sin(x*pi)*cos(x*pi)*cos(y*pi)^2 + 1.5*cos(1.5*x)*cos(1.6*y)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'cos(1.3*x)*cos(y*pi)'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '1.69*mu*cos(1.3*x)*cos(y*pi) + pi^2*mu*cos(1.3*x)*cos(y*pi) - 1.3*rho*sin(1.3*x)*sin(x*pi)*cos(y*pi)^2 - 2*pi*rho*sin(y*pi)*cos(1.3*x)^2*cos(y*pi) + pi*rho*cos(1.3*x)*cos(x*pi)*cos(y*pi)^2 - 1.6*sin(1.5*x)*sin(1.6*y)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin(1.5*x)*cos(1.6*y)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-pi*rho*sin(y*pi)*cos(1.3*x) + pi*rho*cos(x*pi)*cos(y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu       NONZERO               superlu_dist'
  line_search = 'none'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-12
[]

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

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

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

restricted_blocks = '1'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

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

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

[Problem]
  kernel_coverage_check = false
[]

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

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

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

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

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

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

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

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

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

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/turbulence/channel/channel_ERCOFTAC.i)

##########################################################
# ERCOFTAC test case foe turbulent channel flow
# Case Number: 032
# Author: Dr. Mauricio Tano
# Last Update: November, 2023
# Turbulent model using:
# k-epsilon model
# Equilibrium + Newton wall treatement
# SIMPLE solve
##########################################################

H = 1 #halfwidth of the channel
L = 30

Re = 13700

rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * 2 * H / Re}'

advected_interp_method = 'upwind'

pressure_tag = "pressure_grad"

### k-epsilon Closure Parameters ###
sigma_k = 1.0
sigma_eps = 1.3
C1_eps = 1.44
C2_eps = 1.92
C_mu = 0.09

### Initial and Boundary Conditions ###
intensity = 0.01
k_init = '${fparse 1.5*(intensity * bulk_u)^2}'
eps_init = '${fparse C_mu^0.75 * k_init^1.5 / H}'

### Modeling parameters ###
bulk_wall_treatment = false
walls = 'top'
wall_treatment = 'eq_newton' # Options: eq_newton, eq_incremental, eq_linearized, neq

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = ${L}
    ymin = 0
    ymax = ${H}
    nx = 20
    ny = 5
    bias_y = 0.7
  []
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system TKE_system TKED_system'
  previous_nl_solution_required = true
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method = ${advected_interp_method}
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = ${bulk_u}
    solver_sys = u_system
    two_term_boundary_expansion = false
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 0
    solver_sys = v_system
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = 1e-8
    solver_sys = pressure_system
    two_term_boundary_expansion = false
  []
  [TKE]
    type = INSFVEnergyVariable
    solver_sys = TKE_system
    initial_condition = ${k_init}
  []
  [TKED]
    type = INSFVEnergyVariable
    solver_sys = TKED_system
    initial_condition = ${eps_init}
  []
[]

[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
  []

  [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
    k = TKE
    rho = ${rho}
    mu = ${mu}
    mu_t = 'mu_t'
    C1_eps = ${C1_eps}
    C2_eps = ${C2_eps}
    walls = ${walls}
    wall_treatment = ${wall_treatment}
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '${bulk_u}'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = 0
  []
  [walls-u]
    type = FVDirichletBC
    boundary = 'top'
    variable = vel_x
    value = 0
  []
  [walls-v]
    type = FVDirichletBC
    boundary = 'top'
    variable = vel_y
    value = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
  [inlet_TKE]
    type = INSFVInletIntensityTKEBC
    boundary = 'left'
    variable = TKE
    u = vel_x
    v = vel_y
    intensity = ${intensity}
  []
  [inlet_TKED]
    type = INSFVMixingLengthTKEDBC
    boundary = 'left'
    variable = TKED
    k = TKE
    characteristic_length = '${fparse 2*H}'
  []
  [walls_mu_t]
    type = INSFVTurbulentViscosityWallFunction
    boundary = 'top'
    variable = mu_t
    u = vel_x
    v = vel_y
    rho = ${rho}
    mu = ${mu}
    mu_t = 'mu_t'
    k = TKE
    wall_treatment = ${wall_treatment}
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = 'mu_t'
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = 'mu_t'
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [symmetry_TKE]
    type = INSFVSymmetryScalarBC
    boundary = 'bottom'
    variable = TKE
  []
  [symmetry_TKED]
    type = INSFVSymmetryScalarBC
    boundary = 'bottom'
    variable = TKED
  []
[]

[AuxVariables]
  [mu_t]
    type = MooseVariableFVReal
    initial_condition = '${fparse rho * C_mu * ${k_init}^2 / eps_init}'
    two_term_boundary_expansion = false
  []
  [yplus]
    type = MooseVariableFVReal
    two_term_boundary_expansion = false
  []
[]

[AuxKernels]
  [compute_mu_t]
    type = kEpsilonViscosityAux
    variable = mu_t
    C_mu = ${C_mu}
    k = 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'
  []
  [compute_y_plus]
    type = RANSYPlusAux
    variable = yplus
    k = TKE
    mu = ${mu}
    rho = ${rho}
    u = vel_x
    v = vel_y
    walls = ${walls}
    wall_treatment = ${wall_treatment}
    execute_on = 'NONLINEAR'
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  turbulence_systems = 'TKED_system TKE_system'

  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.7
  pressure_variable_relaxation = 0.3
  turbulence_equation_relaxation = '0.25 0.25'
  num_iterations = 1000
  pressure_absolute_tolerance = 1e-12
  momentum_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'

  momentum_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
  pressure_l_tol = 0.0
  turbulence_l_tol = 0.0
  print_fields = false
  continue_on_max_its = true
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/hydraulic-separators/separator-scalar.i)

# This test is designed to check for energy conservation
# in separated channels. The three inlet temperatures should be
# preserved at the outlets.

rho=1.1
mu=0.6
alpha=0.1
advected_interp_method='upwind'
velocity_interp_method='rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1.0'
    dy = '0.25 0.25 0.25'
    ix = '5'
    iy = '2 2 2'
    subdomain_id = '1 2 3'
  []
  [separator-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    primary_block = '1'
    paired_block = '2'
    new_boundary = 'separator-1'
  []
  [separator-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = separator-1
    primary_block = '2'
    paired_block = '3'
    new_boundary = 'separator-2'
  []
  [inlet-1]
    type = ParsedGenerateSideset
    input = separator-2
    combinatorial_geometry = 'y < 0.25 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-1
  []
  [inlet-2]
    type = ParsedGenerateSideset
    input = inlet-1
    combinatorial_geometry = 'y > 0.25 & y < 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-2
  []
  [inlet-3]
    type = ParsedGenerateSideset
    input = inlet-2
    combinatorial_geometry = 'y > 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-3
  []
  [outlet-1]
    type = ParsedGenerateSideset
    input = inlet-3
    combinatorial_geometry = 'y < 0.25 & x > 0.999999'
    replace = false
    new_sideset_name = outlet-1
  []
  [outlet-2]
    type = ParsedGenerateSideset
    input = outlet-1
    combinatorial_geometry = 'y > 0.25 & y < 0.5 & x > 0.999999'
    replace = false
    new_sideset_name = outlet-2
  []
  [outlet-3]
    type = ParsedGenerateSideset
    input = outlet-2
    combinatorial_geometry = 'y > 0.5 & x > 0.999999'
    replace = false
    new_sideset_name = outlet-3
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0.1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
  []
  [pressure]
    type = BernoulliPressureVariable
    u = superficial_vel_x
    v = superficial_vel_y
    rho = ${rho}
  []
  [scalar]
    type = INSFVEnergyVariable
    initial_condition = 50
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    momentum_component = 'x'
    mu = ${mu}
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    pressure = pressure
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    momentum_component = 'y'
    mu = ${mu}
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    pressure = pressure
    momentum_component = 'y'
  []

  [scalar_conduction]
    type = FVDiffusion
    coeff = ${alpha}
    variable = scalar
  []
  [scalar_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar
  []
[]

[FVBCs]
  [inlet-u-1]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1'
    variable = superficial_vel_x
    function = '0.1'
  []
  [inlet-u-2]
    type = INSFVInletVelocityBC
    boundary = 'inlet-2'
    variable = superficial_vel_x
    function = '0.2'
  []
  [inlet-u-3]
    type = INSFVInletVelocityBC
    boundary = 'inlet-3'
    variable = superficial_vel_x
    function = '0.3'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1 inlet-2 inlet-3'
    variable = superficial_vel_y
    function = 0
  []

  [inlet-scalar-1]
    type = FVDirichletBC
    variable = scalar
    boundary = 'inlet-1'
    value = 10
  []
  [inlet-scalar-2]
    type = FVDirichletBC
    variable = scalar
    boundary = 'inlet-2'
    value = 20
  []
  [inlet-scalar-3]
    type = FVDirichletBC
    variable = scalar
    boundary = 'inlet-3'
    value = 30
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-u]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_x
    momentum_component = 'x'
  []

  [separator-v]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-p]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = pressure
  []

  [separator-scalar]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = scalar
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  [porosity-1]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '1.0'
    block = '1 3'
  []
  [porosity-2]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '0.5'
    block = '2'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = ' lu       NONZERO               1e-10'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [outlet_scalar1]
    type = SideAverageValue
    variable = 'scalar'
    boundary = 'outlet-1'
  []
  [outlet_scalar2]
    type = SideAverageValue
    variable = 'scalar'
    boundary = 'outlet-2'
  []
  [outlet_scalar3]
    type = SideAverageValue
    variable = 'scalar'
    boundary = 'outlet-3'
  []
[]

[Outputs]
  csv = true
  execute_on = final
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/1d-average.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 1
    xmin = 0
    xmax = 1
    nx = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = false
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

[FVBCs]
  [inlet_u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = 'exact_u'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*x*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/4)*pi^2*mu*sin((1/2)*x*pi) + pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) - '
            '1/2*pi*sin((1/2)*x*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'cos((1/2)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '(1/2)*pi*rho*cos((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
  exodus = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d-functor-material.i)

rho = 1.1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '3 3'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = BernoulliPressureVariable
    u = u
    porosity = porosity
    rho = ${rho}
  []
[]

[AuxVariables]
  [has_porosity_jump_face]
    type = MooseVariableFVReal
  []
  [porosity_out]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [has_porosity_jump_face]
    type = HasPorosityJumpFace
    porosity = porosity
    execute_on = 'initial timestep_end'
    variable = has_porosity_jump_face
  []
  [porosity_out]
    type = FunctorAux
    variable = porosity_out
    functor = porosity
    execute_on = 'initial timestep_end'
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1
  []
[]

[FunctorMaterials]
  [porosity]
    type = ADPiecewiseByBlockFunctorMaterial
    prop_name = 'porosity'
    subdomain_to_prop_value = '1 1 2 0.5'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  line_search = 'none'
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/solidification/pipe_solidification.i)

mu = 8.8871e-4
rho_solid = 997.561
rho_liquid = 997.561
k_solid = 0.6203
k_liquid = 0.6203
cp_solid = 4181.72
cp_liquid = 4181.72
L = 3e5
T_liquidus = 285
T_solidus = 280

advected_interp_method = 'average'
velocity_interp_method = 'rc'

U_inlet = '${fparse 0.5 * mu / rho_liquid / 0.5}'
T_inlet = 300.0
T_cold = 200.0
Nx = 30
Ny = 5

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  coord_type = 'RZ'
  rz_coord_axis = 'X'
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = 0
    ymax = '${fparse 0.5 * 1.0}'
    nx = ${Nx}
    ny = ${Ny}
    bias_y = '${fparse 1 / 1.2}'
  []
  [rename1]
    type = RenameBoundaryGenerator
    input = gen
    old_boundary = 'left'
    new_boundary = 'inlet'
  []
  [rename2]
    type = RenameBoundaryGenerator
    input = rename1
    old_boundary = 'right'
    new_boundary = 'outlet'
  []
  [rename3]
    type = RenameBoundaryGenerator
    input = rename2
    old_boundary = 'bottom'
    new_boundary = 'symmetry'
  []
  [rename4]
    type = RenameBoundaryGenerator
    input = rename3
    old_boundary = 'top'
    new_boundary = 'wall'
  []
  [rename5]
    type = ParsedGenerateSideset
    input = rename4
    normal = '0 1 0'
    combinatorial_geometry = 'x>2.0 & x<8.0 & y>0.49999'
    new_sideset_name = 'cooled_wall'
  []
[]

[AuxVariables]
  [U]
    type = MooseVariableFVReal
  []
  [fl]
    type = MooseVariableFVReal
    initial_condition = 1.0
  []
  [density]
    type = MooseVariableFVReal
  []
  [th_cond]
    type = MooseVariableFVReal
  []
  [cp_var]
    type = MooseVariableFVReal
  []
  [darcy_coef]
    type = MooseVariableFVReal
  []
  [fch_coef]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [mag]
    type = VectorMagnitudeAux
    variable = U
    x = vel_x
    y = vel_y
  []
  [compute_fl]
    type = NSLiquidFractionAux
    variable = fl
    temperature = T
    T_liquidus = '${T_liquidus}'
    T_solidus = '${T_solidus}'
    execute_on = 'TIMESTEP_END'
  []
  [rho_out]
    type = FunctorAux
    functor = 'rho_mixture'
    variable = 'density'
  []
  [th_cond_out]
    type = FunctorAux
    functor = 'k_mixture'
    variable = 'th_cond'
  []
  [cp_out]
    type = FunctorAux
    functor = 'cp_mixture'
    variable = 'cp_var'
  []
  [darcy_out]
    type = FunctorAux
    functor = 'Darcy_coefficient'
    variable = 'darcy_coef'
  []
  [fch_out]
    type = FunctorAux
    functor = 'Forchheimer_coefficient'
    variable = 'fch_coef'
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 0.0
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 0.0
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T]
    type = INSFVEnergyVariable
    initial_condition = '${T_inlet}'
    scaling = 1.0
  []
[]

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

  [u_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_x
    rho = rho_mixture
    momentum_component = 'x'
  []
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = rho_mixture
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = vel_x
    momentum_component = 'x'
    u = vel_x
    v = vel_y
    Darcy_name = 'Darcy_coeff'
    Forchheimer_name = 'Forchheimer_coeff'
    rho = ${rho_liquid}
    mu = ${mu}
    standard_friction_formulation = false
  []

  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_y
    rho = rho_mixture
    momentum_component = 'y'
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = rho_mixture
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = vel_y
    momentum_component = 'y'
    u = vel_x
    v = vel_y
    Darcy_name = 'Darcy_coeff'
    Forchheimer_name = 'Forchheimer_coeff'
    rho = ${rho_liquid}
    mu = ${mu}
    standard_friction_formulation = false
  []

  [T_time]
    type = INSFVEnergyTimeDerivative
    variable = T
    rho = rho_mixture
    dh_dt = dh_dt
  []
  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = k_mixture
    variable = T
  []
  [energy_source]
    type = NSFVPhaseChangeSource
    variable = T
    L = ${L}
    liquid_fraction = fl
    T_liquidus = ${T_liquidus}
    T_solidus = ${T_solidus}
    rho = 'rho_mixture'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'inlet'
    variable = vel_x
    function = '${U_inlet}'
  []
  [sym_u]
    type = INSFVSymmetryVelocityBC
    boundary = 'symmetry'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'inlet'
    variable = vel_y
    function = 0
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'wall'
    variable = vel_x
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'wall'
    variable = vel_y
    function = 0
  []
  [sym_v]
    type = INSFVSymmetryVelocityBC
    boundary = 'symmetry'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = y
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'outlet'
    variable = pressure
    function = 0
  []
  [sym_p]
    type = INSFVSymmetryPressureBC
    boundary = 'symmetry'
    variable = pressure
  []
  [sym_T]
    type = INSFVSymmetryScalarBC
    variable = T
    boundary = 'symmetry'
  []
  [cooled_wall]
    type = FVFunctorDirichletBC
    variable = T
    functor = '${T_cold}'
    boundary = 'cooled_wall'
  []
[]

[FunctorMaterials]
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = rho_mixture
    cp = cp_mixture
    temperature = 'T'
  []
  [eff_cp]
    type = NSFVMixtureFunctorMaterial
    phase_2_names = '${cp_solid} ${k_solid} ${rho_solid}'
    phase_1_names = '${cp_liquid} ${k_liquid} ${rho_liquid}'
    prop_names = 'cp_mixture k_mixture rho_mixture'
    phase_1_fraction = fl
  []
  [mushy_zone_resistance]
    type = INSFVMushyPorousFrictionFunctorMaterial
    liquid_fraction = 'fl'
    mu = '${mu}'
    rho_l = '${rho_liquid}'
  []
  [friction]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Darcy_coeff Forchheimer_coeff'
    prop_values = 'darcy_coef darcy_coef darcy_coef fch_coef fch_coef fch_coef'
  []
[]

[Executioner]
  type = Transient
  dt = 5e3
  end_time = 1e4
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  nl_abs_tol = 1e-8
  nl_max_its = 12
[]

[Postprocessors]
  [average_T]
    type = ElementAverageValue
    variable = T
    outputs = csv
    execute_on = FINAL
  []
[]

[VectorPostprocessors]
  [sat]
    type = LineValueSampler
    warn_discontinuous_face_values = false
    start_point = '0.0 0 0'
    end_point = '10.0 0 0'
    num_points = '${Nx}'
    sort_by = x
    variable = 'T'
    execute_on = FINAL
  []
[]

[Outputs]
  exodus = true
  [csv]
    type = CSV
    execute_on = 'FINAL'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average-with-temp.i)

mu = 1.1
rho = 1.1
k = 1.1
cp = 1.1
advected_interp_method = 'average'
velocity_interp_method = 'average'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

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

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

  [temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = temperature
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = temperature
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
  []
  [temp_forcing]
    type = FVBodyForce
    variable = temperature
    function = forcing_t
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 'exact_v'
  []
  [inlet-and-walls-t]
    type = FVFunctionDirichletBC
    boundary = 'left top bottom'
    variable = temperature
    function = 'exact_t'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

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

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + '
            '(1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - '
            'pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - '
            '1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - '
            'pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + '
            '(1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + '
            '(3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [exact_t]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_t]
    type = ParsedFunction
    expression = '-pi*cp*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - '
            '1/2*pi*cp*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + '
            '(1/4)*pi*cp*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + '
            '(5/16)*pi^2*k*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
    symbol_names = 'k rho cp'
    symbol_values = '${k} ${rho} ${cp}'
  []
[]

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

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2Error
    variable = u
    function = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2Error
    variable = v
    function = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    variable = pressure
    function = exact_p
    type = ElementL2Error
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2t]
    variable = temperature
    function = exact_t
    type = ElementL2Error
    outputs = 'console csv'
    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'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-average-with-temp.i)

mu=1.1
rho=1.1
k=1.1
cp=1.1
advected_interp_method='average'
velocity_interp_method='average'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1
    ymin = 0
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[Problem]
  coord_type = 'RZ'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

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

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

  [temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = temperature
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = temperature
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
  []
  [temp_forcing]
    type = FVBodyForce
    variable = temperature
    function = forcing_t
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 'exact_v'
  []
  [no-slip-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 'exact_u'
  []
  [no-slip-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 'exact_v'
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 'exact_p'
  []
  [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
  []
  [axis-inlet-wall-t]
    type = FVFunctionDirichletBC
    boundary = 'left bottom right'
    variable = temperature
    function = 'exact_t'
  []
[]

[FunctorMaterials]
  [const_functor]
    type = ADGenericFunctorMaterial
    prop_names = 'cp k'
    prop_values = '${cp} ${k}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'temperature'
    rho = ${rho}
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin(x*pi)^2*sin((1/2)*y*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin(x*pi)^2*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/4)*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) + (4*x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^4*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)^2*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x - (-2*x*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) + 2*x*pi^2*mu*sin((1/2)*y*pi)*cos(x*pi)^2 + 2*pi*mu*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos(y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*cos(x*pi)*cos(y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)*cos(y*pi) + 2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi))/x'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [exact_t]
    type = ParsedFunction
    expression = 'sin(x*pi)*sin((1/2)*y*pi)'
  []
  [forcing_t]
    type = ParsedFunction
    expression = '(1/4)*pi^2*k*sin(x*pi)*sin((1/2)*y*pi) - (-x*pi^2*k*sin(x*pi)*sin((1/2)*y*pi) + pi*k*sin((1/2)*y*pi)*cos(x*pi))/x + (3*x*pi*cp*rho*sin(x*pi)^2*sin((1/2)*y*pi)^2*cos(x*pi) + cp*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2)/x + (-x*pi*cp*rho*sin(x*pi)*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*cp*rho*sin(x*pi)*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x'
    symbol_names = 'k rho cp'
    symbol_values = '${k} ${rho} ${cp}'
  []
[]

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

[Outputs]
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2t]
    approximate = temperature
    exact = exact_t
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/hydraulic-separators/separator-jump.i)

# This test describes a test where three parallel channels are
# separated using flow separators that act as slip boundary conditions.
# The different channels have different pressure discontinuities
# due to Bernoulli pressure jump combined with irreversible form losses.
# Channel 1 expected drop (analytic, Bernoulli plus contraction form loss): 2.079E-01 Pa
# Channel 2 expected drop (analytic, Bernoulli plus contraction form loss): 8.360E-02 Pa
# Channel 3 expected drop (analytic, Bernoulli plus contraction form loss): 1.870E-02 Pa

rho=1.1
advected_interp_method='upwind'
velocity_interp_method='rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '0.2 0.2 0.2 0.2'
    dy = '0.25 0.25 0.25'
    ix = '2 2 2 2'
    iy = '2 2 2'
    subdomain_id = '1 2 2 2 3 3 4 4 5 5 5 6'
  []
  [separator-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    primary_block = '1 2'
    paired_block = '3 4'
    new_boundary = 'separator-1'
  []
  [separator-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = separator-1
    primary_block = '3 4'
    paired_block = '5 6'
    new_boundary = 'separator-2'
  []
  [jump-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = separator-2
    primary_block = '1'
    paired_block = '2'
    new_boundary = 'jump-1'
  []
  [jump-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = jump-1
    primary_block = '3'
    paired_block = '4'
    new_boundary = 'jump-2'
  []
  [jump-3]
    type = SideSetsBetweenSubdomainsGenerator
    input = jump-2
    primary_block = '5'
    paired_block = '6'
    new_boundary = 'jump-3'
  []
  [inlet-1]
    type = ParsedGenerateSideset
    input = jump-3
    combinatorial_geometry = 'y < 0.25 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-1
  []
  [inlet-2]
    type = ParsedGenerateSideset
    input = inlet-1
    combinatorial_geometry = 'y > 0.25 & y < 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-2
  []
  [inlet-3]
    type = ParsedGenerateSideset
    input = inlet-2
    combinatorial_geometry = 'y > 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-3
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0.1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
  []
  [pressure]
    type = BernoulliPressureVariable
    u = superficial_vel_x
    v = superficial_vel_y
    rho = ${rho}
    pressure_drop_sidesets = 'jump-1 jump-2 jump-3'
    pressure_drop_form_factors = '0.1 0.2 0.3 '
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    pressure = pressure
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    pressure = pressure
    momentum_component = 'y'
  []
[]

[FVBCs]
  [inlet-u-1]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1'
    variable = superficial_vel_x
    function = '0.1'
  []
  [inlet-u-2]
    type = INSFVInletVelocityBC
    boundary = 'inlet-2'
    variable = superficial_vel_x
    function = '0.2'
  []
  [inlet-u-3]
    type = INSFVInletVelocityBC
    boundary = 'inlet-3'
    variable = superficial_vel_x
    function = '0.3'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1 inlet-2 inlet-3'
    variable = superficial_vel_y
    function = 0
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-u]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_x
    momentum_component = 'x'
  []

  [separator-v]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-p]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = pressure
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  [porosity-1]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '1.0'
    block = '1 3 5'
  []
  [porosity-2]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '0.5'
    block = '2 4 6'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = ' lu       NONZERO               1e-10'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [inlet_p1]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'inlet-1'
  []
  [inlet_p2]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'inlet-2'
  []
  [inlet_p3]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'inlet-3'
  []
  [drop-1]
    type = ParsedPostprocessor
    expression = 'inlet_p1 - outlet'
    pp_names = 'inlet_p1'
    constant_names = 'outlet'
    constant_expressions = '0.4'
  []
  [drop-2]
    type = ParsedPostprocessor
    expression = 'inlet_p2 - outlet'
    pp_names = 'inlet_p2'
    constant_names = 'outlet'
    constant_expressions = '0.4'
  []
  [drop-3]
    type = ParsedPostprocessor
    expression = 'inlet_p3 - outlet'
    pp_names = 'inlet_p3'
    constant_names = 'outlet'
    constant_expressions = '0.4'
  []
[]

[Outputs]
  csv = true
  execute_on = final
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-average.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = false
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = false
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + '
            '(1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - '
            'pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - '
            '1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - '
            'pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + '
            '(1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + '
            '(3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

(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/pins/channel-flow/hydraulic-separators/separator-energy-nonorthogonal.i)

# This test is designed to check for energy conservation
# in separated channels which are described using a nonorthogonal mesh.
# The two inlet temperatures should be preserved at the outlets.

rho=1.1
mu=0.6
k=2.1
cp=5.5
advected_interp_method='upwind'
velocity_interp_method='rc'

[Mesh]
  [file]
    type = FileMeshGenerator
    file = diverging.msh
  []
  [mirror]
    type = SymmetryTransformGenerator
    input = file
    mirror_point = "0 0 0"
    mirror_normal_vector = "1 0 0"
  []
  [stitch]
    type = StitchedMeshGenerator
    inputs = 'file mirror'
    stitch_boundaries_pairs = 'left left'
  []
  [subdomain1]
    type = ParsedSubdomainMeshGenerator
    input = stitch
    combinatorial_geometry = 'x > 0'
    block_id = 1
  []
  [subdomain2]
    type = ParsedSubdomainMeshGenerator
    input = subdomain1
    combinatorial_geometry = 'x < 0'
    block_id = 2
  []
  [separator]
    type = ParsedGenerateSideset
    input = subdomain2
    combinatorial_geometry = 'x > -0.00001 & x < 0.00001'
    replace = true
    new_sideset_name = separator
  []
  [inlet-1]
    type = ParsedGenerateSideset
    input = separator
    combinatorial_geometry = 'y < 0.00001 & x < 0'
    replace = true
    new_sideset_name = inlet-1
  []
  [inlet-2]
    type = ParsedGenerateSideset
    input = inlet-1
    combinatorial_geometry = 'y < 0.00001 & x > 0'
    replace = true
    new_sideset_name = inlet-2
  []
  [outlet-1]
    type = ParsedGenerateSideset
    input = inlet-2
    combinatorial_geometry = 'y > 20.999999 & x < 0'
    replace = true
    new_sideset_name = outlet-1
  []
  [outlet-2]
    type = ParsedGenerateSideset
    input = outlet-1
    combinatorial_geometry = 'y > 20.999999 & x > 0'
    replace = true
    new_sideset_name = outlet-2
  []
  uniform_refine = 1
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0.1
  []
  [pressure]
    type = BernoulliPressureVariable
    u = superficial_vel_x
    v = superficial_vel_y
    rho = ${rho}
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = 300
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    momentum_component = 'x'
    mu = ${mu}
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    pressure = pressure
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    momentum_component = 'y'
    mu = ${mu}
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    pressure = pressure
    momentum_component = 'y'
  []

  [temp_conduction]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1 inlet-2'
    variable = superficial_vel_x
    function = '0.0'
  []
  [inlet-v-1]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1'
    variable = superficial_vel_y
    function = 0.1
  []
  [inlet-v-2]
    type = INSFVInletVelocityBC
    boundary = 'inlet-2'
    variable = superficial_vel_y
    function = 0.2
  []

  [inlet-T-1]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'inlet-1'
    value = 310
  []
  [inlet-T-2]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'inlet-2'
    value = 350
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-u]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator'
    variable = superficial_vel_x
    momentum_component = 'x'
  []

  [separator-v]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-p]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator'
    variable = pressure
  []

  [separator-T]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator'
    variable = T_fluid
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'outlet-2 outlet-1'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  [porosity-1]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '1.0'
    block = '1'
  []
  [porosity-2]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '0.5'
    block = '2'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T_fluid'
    rho = ${rho}
    cp = ${cp}
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = ' lu       NONZERO               1e-10'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [outlet_T1]
    type = SideAverageValue
    variable = 'T_fluid'
    boundary = 'outlet-1'
  []
  [outlet_T2]
    type = SideAverageValue
    variable = 'T_fluid'
    boundary = 'outlet-2'
  []
[]

[Outputs]
  csv = true
  execute_on = final
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/segregated/2d-momentum.i)

mu = 1.1
rho = 1.1

pressure_tag = "pressure_grad"

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = 0
    ymax = 1
    nx = 40
    ny = 6
  []
[]

[GlobalParams]
  advected_interp_method = 'average'
  velocity_interp_method = 'rc'
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolatorSegregated
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system'
  previous_nl_solution_required = true
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
    solver_sys = u_system
    two_term_boundary_expansion = false
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
    solver_sys = v_system
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = false
    solver_sys = pressure_system
  []
[]

[AuxVariables]
  [porosity]
    type = MooseVariableFVReal
    initial_condition = 0.5
  []
[]

[FVKernels]
  inactive = "u_friction v_friction"
  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
    extra_vector_tags = ${pressure_tag}
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_x
    momentum_component = 'y'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
    extra_vector_tags = ${pressure_tag}
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = superficial_vel_y
    momentum_component = 'y'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []

  [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
  []
[]

[FVBCs]
  inactive = 'slip-u slip-v'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [symmetry-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
  ### Are disabled by default but we switch it on for certain tests ###
  [slip-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = superficial_vel_y
    momentum_component = 'y'
  []
  #####################################################################
[]

[FunctorMaterials]
  [darcy]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Darcy_coefficient Forchheimer_coefficient'
    prop_values = '0.01 0.02 0.03 0.01 0.02 0.03'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.85
  pressure_variable_relaxation = 0.45
  num_iterations = 150
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  print_fields = false
  continue_on_max_its = true
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_interface_area_model/turbulent_driven_growth.i)

###############################################################################
# Validation test based on Hibiki and Ishii experiment [1] reported in Figure 5
# [1] Hibiki, T., & Ishii, M. (2000). One-group interfacial area transport of
# bubbly flows in vertical round tubes.
# International Journal of Heat and Mass Transfer, 43(15), 2711-2726.
###############################################################################

mu = 1.0
rho = 1000.0
mu_d = 1.0
rho_d = 1.0
l = ${fparse 50.8/1000.0}
U = 5.031429
dp = 0.005
inlet_phase_2 = 0.442
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
mass_exchange_coeff = 0.0
inlet_interface_area = ${fparse 6.0*inlet_phase_2/dp}

outlet_pressure = 1e5

[GlobalParams]
  rhie_chow_user_object = 'rc'
  density_interp_method = 'average'
  mu_interp_method = 'average'
[]

[Problem]
  identify_variable_groups_in_nl = false
  previous_nl_solution_required = true
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  coord_type = 'RZ'
  rz_coord_axis = 'X'
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = '${fparse l * 60}'
    ymin = 0
    ymax = '${fparse l / 2}'
    nx = 20
    ny = 5
  []
  uniform_refine = 0
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 0
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 0
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [phase_2]
    type = INSFVScalarFieldVariable
    initial_condition = ${inlet_phase_2}
  []
  [interface_area]
    type = INSFVScalarFieldVariable
    initial_condition = ${inlet_interface_area}
  []
[]

[FVKernels]

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

  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = 'rho_mixture'
    momentum_component = 'x'
  []
  [u_drift]
    type = WCNSFV2PMomentumDriftFlux
    variable = vel_x
    rho_d = ${rho_d}
    fd = 'rho_mixture_var'
    u_slip = 'vel_slip_x'
    v_slip = 'vel_slip_y'
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = 'mu_mixture'
    limit_interpolation = true
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = 'rho_mixture'
    momentum_component = 'y'
  []
  [v_drift]
    type = WCNSFV2PMomentumDriftFlux
    variable = vel_y
    rho_d = ${rho_d}
    fd = 'rho_mixture_var'
    u_slip = 'vel_slip_x'
    v_slip = 'vel_slip_y'
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = 'mu_mixture'
    limit_interpolation = true
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []

  [phase_2_advection]
    type = INSFVScalarFieldAdvection
    variable = phase_2
    u_slip = 'vel_x'
    v_slip = 'vel_y'
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = 'upwind'
  []
  [phase_2_diffusion]
    type = FVDiffusion
    variable = phase_2
    coeff = 1.0
  []
  [phase_2_src]
    type = NSFVMixturePhaseInterface
    variable = phase_2
    phase_coupled = phase_1
    alpha = ${mass_exchange_coeff}
  []

  [interface_area_advection]
    type = INSFVScalarFieldAdvection
    variable = interface_area
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = 'upwind'
  []
  [interface_area_diffusion]
    type = FVDiffusion
    variable = interface_area
    coeff = 0.1
  []
  [interface_area_source_sink]
    type = WCNSFV2PInterfaceAreaSourceSink
    variable = interface_area
    u = 'vel_x'
    v = 'vel_y'
    L = ${fparse l/2}
    rho = 'rho_mixture'
    rho_d = 'rho'
    pressure = 'pressure'
    k_c = '${fparse mass_exchange_coeff}'
    fd = 'phase_2'
    sigma = 1e-3
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    functor = '${U}'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    functor = '0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_x
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = vel_y
    function = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '${outlet_pressure}'
  []
  [inlet_phase_2]
    type = FVDirichletBC
    boundary = 'left'
    variable = phase_2
    value = ${inlet_phase_2}
  []
  [inlet_interface_area]
    type = FVDirichletBC
    boundary = 'left'
    variable = interface_area
    value = ${inlet_interface_area}
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = 'mu_mixture'
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = 'mu_mixture'
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [symmetry-phase-2]
    type = INSFVSymmetryScalarBC
    boundary = 'bottom'
    variable = phase_2
  []
  [symmetry-interface-area]
    type = INSFVSymmetryScalarBC
    boundary = 'bottom'
    variable = interface_area
  []
[]

[AuxVariables]
  [drag_coefficient]
    type = MooseVariableFVReal
  []
  [rho_mixture_var]
    type = MooseVariableFVReal
  []
  [mu_mixture_var]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [populate_cd]
    type = FunctorAux
    variable = drag_coefficient
    functor = 'Darcy_coefficient'
  []
  [populate_rho_mixture_var]
    type = FunctorAux
    variable = rho_mixture_var
    functor = 'rho_mixture'
  []
  [populate_mu_mixture_var]
    type = FunctorAux
    variable = mu_mixture_var
    functor = 'mu_mixture'
  []
[]

[FluidProperties]
  [fp]
    type = IdealGasFluidProperties
  []
[]

[FunctorMaterials]
  [bubble_properties]
    type = GeneralFunctorFluidProps
    fp = 'fp'
    pressure = 'pressure'
    T_fluid = 300.0
    speed = 1.0
    characteristic_length = 1.0
    porosity = 1.0
    output_properties = 'rho'
    outputs = 'out'
  []
  [populate_u_slip]
    type = WCNSFV2PSlipVelocityFunctorMaterial
    slip_velocity_name = 'vel_slip_x'
    momentum_component = 'x'
    u = 'vel_x'
    v = 'vel_y'
    rho = ${rho}
    mu = 'mu_mixture'
    rho_d = ${rho_d}
    particle_diameter = ${dp}
    linear_coef_name = 'Darcy_coefficient'
  []
  [populate_v_slip]
    type = WCNSFV2PSlipVelocityFunctorMaterial
    slip_velocity_name = 'vel_slip_y'
    momentum_component = 'y'
    u = 'vel_x'
    v = 'vel_y'
    rho = ${rho}
    mu = 'mu_mixture'
    rho_d = ${rho_d}
    particle_diameter = ${dp}
    linear_coef_name = 'Darcy_coefficient'
  []
  [compute_phase_1]
    type = ADParsedFunctorMaterial
    property_name = phase_1
    functor_names = 'phase_2'
    expression = '1 - phase_2'
  []
  [CD]
    type = NSFVDispersePhaseDragFunctorMaterial
    rho = 'rho_mixture'
    mu = mu_mixture
    u = 'vel_x'
    v = 'vel_y'
    particle_diameter = ${dp}
  []
  [mixing_material]
    type = NSFVMixtureFunctorMaterial
    phase_2_names = '${rho} ${mu}'
    phase_1_names = 'rho ${mu_d}'
    prop_names = 'rho_mixture mu_mixture'
    phase_1_fraction = 'phase_2'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  nl_rel_tol = 1e-10
  line_search = 'none'
[]

[Debug]
  show_var_residual_norms = true
[]

[Preconditioning]
  [SMP]
    type = SMP
    full = true
    petsc_options_iname = '-pc_type -pc_factor_shift_type'
    petsc_options_value = 'lu       NONZERO'
  []
[]

[Outputs]
  [out]
    type = Exodus
  []
[]

[Postprocessors]
  [Re]
    type = ParsedPostprocessor
    expression = '${rho} * ${l} * ${U}'
    pp_names = ''
  []
  [rho_outlet]
    type = SideAverageValue
    boundary = 'right'
    variable = 'rho_mixture_var'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-extrapolated-outlet-pressure.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [lambda]
    family = SCALAR
    order = FIRST
  []
[]

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

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 0
  []
  [outlet_u]
    type = INSFVMomentumAdvectionOutflowBC
    variable = u
    u = u
    v = v
    boundary = 'right'
    momentum_component = 'x'
    rho = ${rho}
  []
  [outlet_v]
    type = INSFVMomentumAdvectionOutflowBC
    variable = v
    u = u
    v = v
    boundary = 'right'
    momentum_component = 'y'
    rho = ${rho}
  []
  [outlet_p]
    type = INSFVMassAdvectionOutflowBC
    boundary = 'right'
    variable = pressure
    u = u
    v = v
    rho = ${rho}
  []
[]

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

[Outputs]
  exodus = true
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/2d-rc-epsjump.i)

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

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1'
    dy = '0.5'
    ix = '30 30'
    iy = '20'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    porosity = porosity
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [v]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    type = MooseVariableFVReal
  []
[]

[ICs]
  inactive = 'porosity_continuous'
  [porosity_1]
    type = ConstantIC
    variable = porosity
    block = 1
    value = 1
  []
  [porosity_2]
    type = ConstantIC
    variable = porosity
    block = 2
    value = 0.5
  []
  [porosity_continuous]
    type = FunctionIC
    variable = porosity
    block = '1 2'
    function = smooth_jump
  []
[]

[Functions]
  [smooth_jump]
    type = ParsedFunction
    expression = '1 - 0.5 * 1 / (1 + exp(-30*(x-1)))'
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    pressure = pressure
    momentum_component = 'y'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = u
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = v
    momentum_component = 'y'
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  inactive = 'smooth'
  [jump]
    type = ADPiecewiseByBlockFunctorMaterial
    prop_name = 'porosity'
    subdomain_to_prop_value = '1 1
                               2 0.5'
  []
  [smooth]
    type = ADGenericFunctionFunctorMaterial
    prop_names = 'porosity'
    prop_values = 'smooth_jump'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/hydraulic-separators/separator-energy.i)

# This test is designed to check for energy conservation
# in separated channels. The three inlet temperatures should be
# preserved at the outlets.

rho=1.1
mu=0.6
k=2.1
cp=5.5
advected_interp_method='upwind'
velocity_interp_method='rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1.0'
    dy = '0.25 0.25 0.25'
    ix = '5'
    iy = '2 2 2'
    subdomain_id = '1 2 3'
  []
  [separator-1]
    type = SideSetsBetweenSubdomainsGenerator
    input = mesh
    primary_block = '1'
    paired_block = '2'
    new_boundary = 'separator-1'
  []
  [separator-2]
    type = SideSetsBetweenSubdomainsGenerator
    input = separator-1
    primary_block = '2'
    paired_block = '3'
    new_boundary = 'separator-2'
  []
  [inlet-1]
    type = ParsedGenerateSideset
    input = separator-2
    combinatorial_geometry = 'y < 0.25 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-1
  []
  [inlet-2]
    type = ParsedGenerateSideset
    input = inlet-1
    combinatorial_geometry = 'y > 0.25 & y < 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-2
  []
  [inlet-3]
    type = ParsedGenerateSideset
    input = inlet-2
    combinatorial_geometry = 'y > 0.5 & x < 0.00001'
    replace = true
    new_sideset_name = inlet-3
  []
  [outlet-1]
    type = ParsedGenerateSideset
    input = inlet-3
    combinatorial_geometry = 'y < 0.25 & x > 0.999999'
    replace = false
    new_sideset_name = outlet-1
  []
  [outlet-2]
    type = ParsedGenerateSideset
    input = outlet-1
    combinatorial_geometry = 'y > 0.25 & y < 0.5 & x > 0.999999'
    replace = false
    new_sideset_name = outlet-2
  []
  [outlet-3]
    type = ParsedGenerateSideset
    input = outlet-2
    combinatorial_geometry = 'y > 0.5 & x > 0.999999'
    replace = false
    new_sideset_name = outlet-3
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  porosity = porosity
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 0.1
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
  []
  [pressure]
    type = BernoulliPressureVariable
    u = superficial_vel_x
    v = superficial_vel_y
    rho = ${rho}
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = 300
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    momentum_component = 'x'
    mu = ${mu}
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    pressure = pressure
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    momentum_component = 'y'
    mu = ${mu}
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    pressure = pressure
    momentum_component = 'y'
  []

  [temp_conduction]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
  []
[]

[FVBCs]
  [inlet-u-1]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1'
    variable = superficial_vel_x
    function = '0.1'
  []
  [inlet-u-2]
    type = INSFVInletVelocityBC
    boundary = 'inlet-2'
    variable = superficial_vel_x
    function = '0.2'
  []
  [inlet-u-3]
    type = INSFVInletVelocityBC
    boundary = 'inlet-3'
    variable = superficial_vel_x
    function = '0.3'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'inlet-1 inlet-2 inlet-3'
    variable = superficial_vel_y
    function = 0
  []

  [inlet-T-1]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'inlet-1'
    value = 310
  []
  [inlet-T-2]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'inlet-2'
    value = 320
  []
  [inlet-T-3]
    type = FVDirichletBC
    variable = T_fluid
    boundary = 'inlet-3'
    value = 330
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-u]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_x
    momentum_component = 'x'
  []

  [separator-v]
    type = INSFVVelocityHydraulicSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = superficial_vel_y
    momentum_component = 'y'
  []

  [separator-p]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = pressure
  []

  [separator-T]
    type = INSFVScalarFieldSeparatorBC
    boundary = 'separator-1 separator-2'
    variable = T_fluid
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.4
  []
[]

[FunctorMaterials]
  [porosity-1]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '1.0'
    block = '1 3'
  []
  [porosity-2]
    type = ADGenericFunctorMaterial
    prop_names = 'porosity'
    prop_values = '0.5'
    block = '2'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = superficial_vel_x
    superficial_vel_y = superficial_vel_y
    porosity = porosity
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T_fluid'
    rho = ${rho}
    cp = ${cp}
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = ' lu       NONZERO               1e-10'
  line_search = 'none'
  nl_rel_tol = 1e-10
[]

[Postprocessors]
  [outlet_T1]
    type = SideAverageValue
    variable = 'T_fluid'
    boundary = 'outlet-1'
  []
  [outlet_T2]
    type = SideAverageValue
    variable = 'T_fluid'
    boundary = 'outlet-2'
  []
  [outlet_T3]
    type = SideAverageValue
    variable = 'T_fluid'
    boundary = 'outlet-3'
  []
[]

[Outputs]
  csv = true
  execute_on = final
[]

(modules/navier_stokes/test/tests/finite_volume/fviks/convection/convection_channel.i)

mu = 1
rho = 1
k = .01
cp = 1

[Mesh]
  [cmg]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 0.5'
    dy = '1'
    ix = '8 5'
    iy = '8'
    subdomain_id = '0 1'
  []
  [interface]
    type = SideSetsBetweenSubdomainsGenerator
    input = 'cmg'
    primary_block = 0
    paired_block = 1
    new_boundary = 'interface'
  []
  [fluid_side]
    type = BreakBoundaryOnSubdomainGenerator
    input = 'interface'
    boundaries = 'top bottom'
  []
[]

[GlobalParams]
  # retain behavior at time of test creation
  two_term_boundary_expansion = false
  rhie_chow_user_object = 'rc'
  advected_interp_method = 'average'
  velocity_interp_method = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    block = 0
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    block = 0
    initial_condition = 1e-6
  []
  [v]
    type = INSFVVelocityVariable
    block = 0
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
    block = 0
  []
  [T]
    type = INSFVEnergyVariable
    block = 0
    initial_condition = 1
  []
  [Ts]
    type = INSFVEnergyVariable
    block = 1
  []
  [lambda]
    family = SCALAR
    order = FIRST
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    rho = ${rho}
  []
  [mean_zero_pressure]
    type = FVIntegralValueConstraint
    variable = pressure
    lambda = lambda
  []

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

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

  [temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = T
  []
  [temp_advection]
    type = INSFVEnergyAdvection
    variable = T
  []

  [solid_temp_conduction]
    type = FVDiffusion
    coeff = 'k'
    variable = Ts
  []
[]

[FVInterfaceKernels]
  [convection]
    type = FVConvectionCorrelationInterface
    variable1 = T
    variable2 = Ts
    boundary = 'interface'
    h = 5
    T_solid = Ts
    T_fluid = T
    subdomain1 = 0
    subdomain2 = 1
    wall_cell_is_bulk = true
  []
[]

[FVBCs]
  [walls_u]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'interface left'
    function = 0
  []
  [walls_v]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'interface left'
    function = 0
  []

  [inlet_u]
    type = INSFVInletVelocityBC
    variable = u
    boundary = 'bottom_to_0'
    function = 0
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    variable = v
    boundary = 'bottom_to_0'
    function = 1
  []

  [inlet_T]
    type = FVDirichletBC
    variable = T
    boundary = 'bottom_to_0'
    value = 0.5
  []

  [outlet]
    type = INSFVMassAdvectionOutflowBC
    variable = pressure
    boundary = 'top_to_0'
    u = u
    v = v
    rho = ${rho}
  []
  [outlet_u]
    type = INSFVMomentumAdvectionOutflowBC
    variable = u
    boundary = 'top_to_0'
    u = u
    v = v
    momentum_component = 'x'
    rho = ${rho}
  []
  [outlet_v]
    type = INSFVMomentumAdvectionOutflowBC
    variable = v
    boundary = 'top_to_0'
    u = u
    v = v
    momentum_component = 'y'
    rho = ${rho}
  []

  [heater]
    type = FVDirichletBC
    variable = 'Ts'
    boundary = 'right'
    value = 10
  []
[]

[FunctorMaterials]
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp k'
    prop_values = '${cp} ${k}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    temperature = 'T'
    rho = ${rho}
    block = 0
  []
[]

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

  nl_abs_tol = 1e-14
[]

[Postprocessors]
  [max_T]
    type = ADElementExtremeFunctorValue
    functor = T
    block = 0
  []
  [max_Ts]
    type = ADElementExtremeFunctorValue
    functor = Ts
    block = 1
  []
  [mdot_out]
    type = VolumetricFlowRate
    boundary = 'top_to_0'
    vel_x = u
    vel_y = v
    advected_quantity = ${rho}
  []
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/cylindrical/2d-rc.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1
    ymin = 0
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[Problem]
  coord_type = 'RZ'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

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

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 'exact_v'
  []
  [no-slip-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = u
    function = 'exact_u'
  []
  [no-slip-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = v
    function = 'exact_v'
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 'exact_p'
  []
  [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
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin(x*pi)^2*sin((1/2)*y*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin(x*pi)^2*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/4)*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) - pi*sin(x*pi)*cos((1/2)*y*pi) + (4*x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)^2*cos(x*pi) + rho*sin(x*pi)^4*sin((1/2)*y*pi)^2)/x + (-x*pi*rho*sin(x*pi)^2*sin((1/2)*y*pi)*sin(y*pi)*cos(x*pi) + (1/2)*x*pi*rho*sin(x*pi)^2*cos(x*pi)*cos((1/2)*y*pi)*cos(y*pi))/x - (-2*x*pi^2*mu*sin(x*pi)^2*sin((1/2)*y*pi) + 2*x*pi^2*mu*sin((1/2)*y*pi)*cos(x*pi)^2 + 2*pi*mu*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos(y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*cos(x*pi)*cos(y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = 'pi^2*mu*cos(x*pi)*cos(y*pi) - 2*pi*rho*sin(y*pi)*cos(x*pi)^2*cos(y*pi) - 1/2*pi*sin((1/2)*y*pi)*cos(x*pi) - (-x*pi^2*mu*cos(x*pi)*cos(y*pi) - pi*mu*sin(x*pi)*cos(y*pi))/x + (-x*pi*rho*sin(x*pi)^3*sin((1/2)*y*pi)*cos(y*pi) + 2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi)^2*cos(y*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi)*cos(x*pi)*cos(y*pi))/x'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'cos(x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-pi*rho*sin(y*pi)*cos(x*pi) + (2*x*pi*rho*sin(x*pi)*sin((1/2)*y*pi)*cos(x*pi) + rho*sin(x*pi)^2*sin((1/2)*y*pi))/x'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [./L2u]
    type = ElementL2Error
    variable = u
    function = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2v]
    type = ElementL2Error
    variable = v
    function = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
  [./L2p]
    variable = pressure
    function = exact_p
    type = ElementL2Error
    outputs = 'console csv'
    execute_on = 'timestep_end'
  [../]
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/2d-rc.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = -1
    ymax = 1
    nx = 2
    ny = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

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

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = 'rho*sin((1/2)*y*pi)*cos((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '(1/2)*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + '
            '(1/2)*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - '
            'pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - '
            '1/4*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = 'rho*sin((1/4)*x*pi)*cos((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '(5/16)*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - '
            'pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + '
            '(1/4)*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + '
            '(3/2)*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - '
            '1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    type = ElementL2FunctorError
    approximate = pressure
    exact = exact_p
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

(modules/navier_stokes/examples/flow-over-circle/flow_over_circle.i)

velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    two_term_boundary_expansion = true
  []
  [vel_y]
    type = INSFVVelocityVariable
    two_term_boundary_expansion = true
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = true
  []
[]

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

[FVBCs]
  [inlet_x]
    type = INSFVInletVelocityBC
    variable = vel_x
    boundary = 'left_boundary'
    function = 'inlet_function'
  []
  [inlet_y]
    type = INSFVInletVelocityBC
    variable = vel_y
    boundary = 'left_boundary'
    function = 0
  []
  [circle_x]
    type = INSFVNoSlipWallBC
    variable = vel_x
    boundary = 'circle'
    function = 0
  []
  [circle_y]
    type = INSFVNoSlipWallBC
    variable = vel_y
    boundary = 'circle'
    function = 0
  []
  [walls_x]
    type = INSFVNoSlipWallBC
    variable = vel_x
    boundary = 'top_boundary bottom_boundary'
    function = 0
  []
  [walls_y]
    type = INSFVNoSlipWallBC
    variable = vel_y
    boundary = 'top_boundary bottom_boundary'
    function = 0
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    variable = pressure
    boundary = 'right_boundary'
    function = 0
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    zmin = -1
    zmax = 1
    nx = 21
    ny = 7
    nz = 7
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    w = w
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [w]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

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

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

  [w_advection]
    type = INSFVMomentumAdvection
    variable = w
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'z'
  []
  [w_viscosity]
    type = INSFVMomentumDiffusion
    variable = w
    mu = ${mu}
    momentum_component = 'z'
  []
  [w_pressure]
    type = INSFVMomentumPressure
    variable = w
    momentum_component = 'z'
    pressure = pressure
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []
  [inlet-w]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = w
    function = 0
  []

  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom front back'
    variable = u
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom front back'
    variable = v
    momentum_component = 'y'
  []
  [walls-w]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom front back'
    variable = w
    momentum_component = 'z'
  []

  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      100                lu           NONZERO'
  line_search = 'none'
  nl_abs_tol = 1e-13
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/2d-rc-slip.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = 0
    ymax = 10
    nx = 10
    ny = 50
  []
[]

[Problem]
  coord_type = 'RZ'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

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

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

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = u
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = v
    function = 1
  []
  [free-slip-wall-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = u
    momentum_component = 'x'
  []
  [free-slip-wall-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = v
    momentum_component = 'y'
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
  [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
  []
[]

[Postprocessors]
  [in]
    type = SideIntegralVariablePostprocessor
    variable = v
    boundary = 'bottom'
    outputs = 'csv'
  []
  [out]
    type = SideIntegralVariablePostprocessor
    variable = v
    boundary = 'top'
    outputs = 'csv'
  []
[]

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

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/3d/3d-segregated-scalar.i)

mu = 0.002
rho = 1.0
diff = 1.5
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 3
    dx = '0.2'
    dy = '0.2'
    dz = '0.8'
    ix = '3'
    iy = '3'
    iz = '6'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system w_system pressure_system scalar_1_system scalar_2_system'
  previous_nl_solution_required = true
  error_on_jacobian_nonzero_reallocation = true
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    w = vel_z
    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
  []
  [vel_z]
    type = INSFVVelocityVariable
    initial_condition = 0.5
    solver_sys = w_system
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    solver_sys = pressure_system
    initial_condition = 0.2
    two_term_boundary_expansion = false
  []
  [scalar_1]
    type = INSFVScalarFieldVariable
    solver_sys = scalar_1_system
    initial_condition = 1.2
  []
  [scalar_2]
    type = INSFVScalarFieldVariable
    solver_sys = scalar_2_system
    initial_condition = 1.2
  []
[]

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

  [scalar_1_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar_1
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_1_diffusion]
    type = FVDiffusion
    coeff = ${diff}
    variable = scalar_1
  []
  [scalar_1_src]
    type = FVBodyForce
    variable = scalar_1
    value = 1.0
  []
  [scalar_1_coupled_source]
    type = FVCoupledForce
    variable = scalar_1
    v = scalar_2
    coef = 0.1
  []

  [scalar_2_advection]
    type = INSFVScalarFieldAdvection
    variable = scalar_2
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [scalar_2_diffusion]
    type = FVDiffusion
    coeff = '${fparse 2*diff}'
    variable = scalar_2
  []
  [scalar_2_src]
    type = FVBodyForce
    variable = scalar_2
    value = 5.0
  []
  [scalar_2_coupled_source]
    type = FVCoupledForce
    variable = scalar_2
    v = scalar_1
    coef = 0.05
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_x
    function = '0'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_y
    function = '0'
  []
  [inlet-w]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_z
    function = '1.1'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom '
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom'
    variable = vel_y
    function = 0.0
  []
  [walls-w]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom'
    variable = vel_z
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'front'
    variable = pressure
    function = 1.4
  []
  [zero-grad-pressure]
    type = FVFunctionNeumannBC
    variable = pressure
    boundary = 'back left right top bottom'
    function = 0.0
  []
  [inlet_scalar_1]
    type = FVDirichletBC
    boundary = 'back'
    variable = scalar_1
    value = 1
  []
  [inlet_scalar_2]
    type = FVDirichletBC
    boundary = 'back'
    variable = scalar_2
    value = 2
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  passive_scalar_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  passive_scalar_l_tol = 0
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system w_system'
  pressure_system = 'pressure_system'
  passive_scalar_systems = 'scalar_1_system scalar_2_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  passive_scalar_equation_relaxation = '0.98 0.98'
  num_iterations = 150
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  passive_scalar_absolute_tolerance = '1e-13 1e-13'
  print_fields = false
[]

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

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d.i)

rho = 1.1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '3 3'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = BernoulliPressureVariable
    u = u
    porosity = porosity
    rho = ${rho}
  []
[]

[AuxVariables]
  [porosity]
    type = PiecewiseConstantVariable
  []
  [has_porosity_jump_face]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [has_porosity_jump_face]
    type = HasPorosityJumpFace
    porosity = porosity
    execute_on = 'initial timestep_end'
    variable = has_porosity_jump_face
  []
[]

[ICs]
  [porosity_1]
    type = ConstantIC
    variable = porosity
    block = 1
    value = 1
  []
  [porosity_2]
    type = ConstantIC
    variable = porosity
    block = 2
    value = 0.5
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  line_search = 'none'
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/mms/channel-flow/plane-poiseuille-flow.i)

mu = 0.5
rho = 1.1
advected_interp_method = 'average'
velocity_interp_method = 'average'
two_term_boundary_expansion = true

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 10
    ny = 2
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = ${two_term_boundary_expansion}
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1
    two_term_boundary_expansion = ${two_term_boundary_expansion}
  []
  [pressure]
    type = INSFVPressureVariable
    two_term_boundary_expansion = ${two_term_boundary_expansion}
  []
[]

[FVKernels]
  [mass]
    type = INSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    variable = u
    boundary = 'top bottom'
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    variable = v
    boundary = 'top bottom'
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = '0.5*(1.0 - y^2)/mu'
    symbol_names = 'mu'
    symbol_values = '${mu}'
  []
  [exact_rhou]
    type = ParsedFunction
    expression = '0.5*rho*(1.0 - y^2)/mu'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '0'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = '0.0'
  []
  [exact_rhov]
    type = ParsedFunction
    expression = '0'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '0'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = '10.0 - x'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '0'
    symbol_names = 'rho mu'
    symbol_values = '${rho} ${mu}'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu NONZERO                     superlu_dist'
[]

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2Error
    variable = u
    function = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2Error
    variable = v
    function = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    variable = pressure
    function = exact_p
    type = ElementL2Error
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

(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/ins/channel-flow/2d-rc.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = 0
  []
  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = vel_x
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = vel_y
    momentum_component = 'y'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

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

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-disp-system.i)

mu = 1
rho = 1
k = 1e-3
cp = 1
u_inlet = 1
T_inlet = 200
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '5 5'
    dy = '1.0'
    ix = '50 50'
    iy = '20'
    subdomain_id = '1 2'
  []
  displacements = 'disp_x disp_y'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  use_displaced_mesh = true
[]

[AuxVariables]
  [disp_x][]
  [disp_y][]
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
    disp_x = disp_x
    disp_y = disp_y
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
[]

[AuxVariables]
  [T_solid]
    family = 'MONOMIAL'
    order = 'CONSTANT'
    fv = true
    initial_condition = 100
  []
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    k = ${k}
    variable = T_fluid
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVNeumannBC
    variable = T_fluid
    value = '${fparse u_inlet * rho * cp * T_inlet}'
    boundary = 'left'
  []
  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.1
  []
[]

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

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv'
    prop_values = '1'
  []
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '${cp}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideAverageValue
    variable = superficial_vel_x
    boundary = 'right'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'right'
  []
  [solid-temp]
    type = ElementAverageValue
    variable = T_solid
  []
[]

[Outputs]
  hide = 'disp_x disp_y'
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/ins/multiapp-scalar-transport/fluid-flow.i)

mu=1
rho=1

[GlobalParams]
  rhie_chow_user_object = 'rc'
  advected_interp_method='average'
  velocity_interp_method='rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

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

[AuxVariables]
  [ax_out]
    type = MooseVariableFVReal
  []
  [ay_out]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [ax_out]
    type = FunctorAux
    functor = ax
    variable = ax_out
    execute_on = timestep_end
  []
  [ay_out]
    type = FunctorAux
    functor = ay
    variable = ay_out
    execute_on = timestep_end
  []
[]


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

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

[MultiApps]
  [scalar]
    type = FullSolveMultiApp
    execute_on = 'timestep_end'
    input_files = 'scalar-transport.i'
  []
[]

[Transfers]
  [ax]
    type = MultiAppCopyTransfer
    source_variable = ax_out
    variable = ax
    execute_on = 'timestep_end'
    to_multi_app = 'scalar'
  []
  [ay]
    type = MultiAppCopyTransfer
    source_variable = ay_out
    variable = ay
    execute_on = 'timestep_end'
    to_multi_app = 'scalar'
  []
  [u]
    type = MultiAppCopyTransfer
    source_variable = u
    variable = u
    execute_on = 'timestep_end'
    to_multi_app = 'scalar'
  []
  [v]
    type = MultiAppCopyTransfer
    source_variable = v
    variable = v
    execute_on = 'timestep_end'
    to_multi_app = 'scalar'
  []
  [pressure]
    type = MultiAppCopyTransfer
    source_variable = pressure
    variable = pressure
    execute_on = 'timestep_end'
    to_multi_app = 'scalar'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu       NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/porosity_jump/bernoulli-1d-parsed-function.i)

rho = 1.1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '3 3'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = BernoulliPressureVariable
    u = u
    porosity = porosity
    rho = ${rho}
  []
[]

[Functions]
  [porosity]
    type = ParsedFunction
    expression = 'if(x > 1, 0.5, 1)'
  []
[]

[AuxVariables]
  [has_porosity_jump_face]
    type = MooseVariableFVReal
  []
  [porosity_out]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [has_porosity_jump_face]
    type = HasPorosityJumpFace
    porosity = porosity
    execute_on = 'initial timestep_end'
    variable = has_porosity_jump_face
  []
  [porosity_out]
    type = FunctorAux
    variable = porosity_out
    functor = porosity
    execute_on = 'initial timestep_end'
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 1
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  line_search = 'none'
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/mms/2d-rc.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = -1
    ymax = 1
    nx = 8
    ny = 8
  []
[]

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

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.8
  []
[]

[GlobalParams]
  porosity = porosity
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
    porosity = porosity
  []
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
  [v_forcing]
    type = INSFVBodyForce
    variable = v
    functor = forcing_v
    momentum_component = 'y'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    functor = 'exact_u'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    functor = 'exact_v'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = u
    function = 'exact_u'
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = v
    function = 'exact_v'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'sin((1/2)*y*pi)*cos((1/2)*x*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '0.5*pi^2*mu*sin((1/2)*y*pi)*cos((1/2)*x*pi) - 0.625*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) + 0.625*pi*rho*sin((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi)^2 - 1.25*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)^2*cos((1/2)*x*pi) - 0.2*pi*sin((1/4)*x*pi)*sin((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_v]
    type = ParsedFunction
    expression = 'sin((1/4)*x*pi)*cos((1/2)*y*pi)'
  []
  [forcing_v]
    type = ParsedFunction
    expression = '0.3125*pi^2*mu*sin((1/4)*x*pi)*cos((1/2)*y*pi) - 1.25*pi*rho*sin((1/4)*x*pi)^2*sin((1/2)*y*pi)*cos((1/2)*y*pi) - 0.625*pi*rho*sin((1/4)*x*pi)*sin((1/2)*x*pi)*sin((1/2)*y*pi)*cos((1/2)*y*pi) + 0.3125*pi*rho*sin((1/2)*y*pi)*cos((1/4)*x*pi)*cos((1/2)*x*pi)*cos((1/2)*y*pi) + 1.2*pi*cos((1/4)*x*pi)*cos((3/2)*y*pi)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin((3/2)*y*pi)*cos((1/4)*x*pi)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/4)*x*pi)*sin((1/2)*y*pi) - 1/2*pi*rho*sin((1/2)*x*pi)*sin((1/2)*y*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

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

[Outputs]
  csv = true
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2v]
    type = ElementL2FunctorError
    approximate = v
    exact = exact_v
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    type = ElementL2FunctorError
    approximate = pressure
    exact = exact_p
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

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

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

restricted_blocks = '1'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

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

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

[Problem]
  kernel_coverage_check = false
[]

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

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

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

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

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

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

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

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

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

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/one-elem-wide-channel.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 5
    ny = 1
  []
[]

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

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

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

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [walls-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = u
    momentum_component = 'x'
  []
  [walls-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top bottom'
    variable = v
    momentum_component = 'y'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

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

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/examples/pipe_mixing_length/pipe_mixing_length.i)

# This example demonstrates how the mixing length model can be tuned to match an
# established correlation for pressure drop in a smooth circular pipe.

# The primary input parameters for this example are the system Reynolds number
# and the von Karman constant for the mixing length model. These two parameters
# can be changed here:
Re = 1e5
von_karman_const = 0.22

# Note that for this model (using the wall-distance mixing length for the entire
# pipe) different von Karman constants are optimal for different Reynolds
# numbers.

# This model has been non-dimensionalized. The diameter (D), density (rho), and
# bulk velocity (bulk_u) are all considered unity.
D = 1
total_len = ${fparse 40 * D}
rho = 1
bulk_u = 1

# With those parameters set, the viscosity is then computed in order to reach
# the desired Reynolds number.
mu = ${fparse rho * bulk_u * D / Re}

# Here the DeltaP will be evaluated by using a postprocessor to find the pressure
# at a point that is 10 diameters away from the outlet. (The outlet pressure is
# set to zero.)
L = ${fparse 10 * D}

# We will use the McAdams correlation to find the Darcy friction factor. Note
# that this correlation is valid for fully developed flow in smooth circular
# tubes at 3e4 < Re < 1e6.
f = ${fparse 0.316 * Re^(-0.25)}

# The DeltaP can then be computed using this friction factor as,
ref_delta_P = ${fparse f * L / D * rho * bulk_u^2 / 2}

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = ${total_len}
    ymin = 0
    ymax = ${fparse 0.5 * D}
    nx = 200
    ny = 40
    bias_y = ${fparse 1 / 1.2}
  []
  [rename1]
    type = RenameBoundaryGenerator
    input = gen
    old_boundary = 'left'
    new_boundary = 'inlet'
  []
  [rename2]
    type = RenameBoundaryGenerator
    input = rename1
    old_boundary = 'right'
    new_boundary = 'outlet'
  []
  [rename3]
    type = RenameBoundaryGenerator
    input = rename2
    old_boundary = 'bottom'
    new_boundary = 'symmetry'
  []
  [rename4]
    type = RenameBoundaryGenerator
    input = rename3
    old_boundary = 'top'
    new_boundary = 'wall'
  []
[]

[Outputs]
  exodus = true
[]

[Problem]
  kernel_coverage_check = false
  fv_bcs_integrity_check = true
  coord_type = 'RZ'
  rz_coord_axis = 'X'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
  # The upwind and Rhie-Chow interpolation schemes are used here.
  advected_interp_method='upwind'
  velocity_interp_method='rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_len]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

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

  [u_advection]
    type = INSFVMomentumAdvection
    variable = u
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = u
    rho = ${rho}
    mixing_length = mixing_len
    momentum_component = 'x'
    u = u
    v = v
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = u
    momentum_component = 'x'
    pressure = pressure
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = v
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_viscosity_rans]
    type = INSFVMixingLengthReynoldsStress
    variable = v
    rho = ${rho}
    mixing_length = mixing_len
    momentum_component = 'y'
    u = u
    v = v
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
  []
[]

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'wall'
    variable = mixing_len
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
  []
[]

[FVBCs]
  [inlet_u]
    type = INSFVInletVelocityBC
    boundary = 'inlet'
    variable = u
    function = ${bulk_u}
  []
  [inlet_v]
    type = INSFVInletVelocityBC
    boundary = 'inlet'
    variable = v
    function = '0'
  []
  [walls_u]
    type = INSFVNoSlipWallBC
    boundary = 'wall'
    variable = u
    function = 0
  []
  [walls_v]
    type = INSFVNoSlipWallBC
    boundary = 'wall'
    variable = v
    function = 0
  []
  [sym_u]
    type = INSFVSymmetryVelocityBC
    boundary = 'symmetry'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
  []
  [sym_v]
    type = INSFVSymmetryVelocityBC
    boundary = 'symmetry'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = y
  []
  [sym_p]
    type = INSFVSymmetryPressureBC
    boundary = 'symmetry'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'outlet'
    variable = pressure
    function = '0'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'
  line_search = 'none'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-12
[]

[Postprocessors]
  [delta_P]
    type = PointValue
    variable = 'pressure'
    point = '${fparse total_len - L} 0 0'
  []
  [reference_delta_P]
    type = Receiver
    default = ${ref_delta_P}
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/3d/3d-segregated-velocity.i)

mu = 0.002
rho = 1.0
advected_interp_method = 'average'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 3
    dx = '0.2'
    dy = '0.2'
    dz = '0.8'
    ix = '3'
    iy = '3'
    iz = '12'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system w_system pressure_system'
  previous_nl_solution_required = true
  error_on_jacobian_nonzero_reallocation = true
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    w = vel_z
    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
  []
  [vel_z]
    type = INSFVVelocityVariable
    initial_condition = 0.5
    solver_sys = w_system
    two_term_boundary_expansion = false
  []
  [pressure]
    type = INSFVPressureVariable
    solver_sys = pressure_system
    initial_condition = 0.2
    two_term_boundary_expansion = false
  []
[]

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_x
    function = '0'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_y
    function = '0'
  []
  [inlet-w]
    type = INSFVInletVelocityBC
    boundary = 'back'
    variable = vel_z
    function = '1.1'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom '
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom'
    variable = vel_y
    function = 0.0
  []
  [walls-w]
    type = INSFVNoSlipWallBC
    boundary = 'left right top bottom'
    variable = vel_z
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'front'
    variable = pressure
    function = 1.4
  []
  [zero-grad-pressure]
    type = FVFunctionNeumannBC
    variable = pressure
    boundary = 'back left right top bottom'
    function = 0.0
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  rhie_chow_user_object = 'rc'
  momentum_systems = 'u_system v_system w_system'
  pressure_system = 'pressure_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.6
  pressure_variable_relaxation = 0.3
  num_iterations = 100
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13

  momentum_l_abs_tol = 1e-14
  pressure_l_abs_tol = 1e-14
  momentum_l_tol = 0
  pressure_l_tol = 0
  print_fields = false
  continue_on_max_its = true
[]

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

(modules/navier_stokes/test/tests/finite_volume/pwcns/channel-flow/2d-transient.i)

# Fluid properties
mu = 'mu'
rho = 'rho'
cp = 'cp'
k = 'k'

# Solid properties
cp_s = 2
rho_s = 4
k_s = 1e-2
h_fs = 10

# Operating conditions
u_inlet = 1
T_inlet = 200
p_outlet = 10
top_side_temperature = 150

# Numerical scheme
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = 0
    ymax = 1
    nx = 20
    ny = 5
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
    initial_condition = ${p_outlet}
  []
  [T_fluid]
    type = INSFVEnergyVariable
    initial_condition = ${T_inlet}
  []
  [T_solid]
    type = MooseVariableFVReal
    initial_condition = 100
  []
[]

[AuxVariables]
  [porosity]
    type = MooseVariableFVReal
    initial_condition = 0.5
  []
  [velocity_norm]
    type = MooseVariableFVReal
  []
[]

[FVKernels]
  [mass_time]
    type = PWCNSFVMassTimeDerivative
    variable = pressure
    porosity = 'porosity'
    drho_dt = 'drho_dt'
  []
  [mass]
    type = PWCNSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_time]
    type = WCNSFVMomentumTimeDerivative
    variable = superficial_vel_x
    rho = ${rho}
    drho_dt = 'drho_dt'
    momentum_component = 'x'
  []
  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_time]
    type = WCNSFVMomentumTimeDerivative
    variable = superficial_vel_y
    rho = ${rho}
    drho_dt = 'drho_dt'
    momentum_component = 'y'
  []
  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [energy_time]
    type = PINSFVEnergyTimeDerivative
    variable = T_fluid
    cp = ${cp}
    rho = ${rho}
    drho_dt = 'drho_dt'
    is_solid = false
    porosity = porosity
  []
  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    variable = T_fluid
    k = ${k}
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = T_fluid
    T_solid = T_solid
    h_solid_fluid = 'h_cv'
  []

  [solid_energy_time]
    type = PINSFVEnergyTimeDerivative
    variable = T_solid
    cp = ${cp_s}
    rho = ${rho_s}
    is_solid = true
    porosity = porosity
  []
  [solid_energy_diffusion]
    type = FVDiffusion
    variable = T_solid
    coeff = ${k_s}
  []
  [solid_energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_solid
    is_solid = true
    T_fluid = T_fluid
    T_solid = T_solid
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVDirichletBC
    variable = T_fluid
    value = ${T_inlet}
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [heated-side]
    type = FVDirichletBC
    boundary = 'top'
    variable = 'T_solid'
    value = ${top_side_temperature}
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = ${p_outlet}
  []
[]

[FluidProperties]
  [fp]
    type = FlibeFluidProperties
  []
[]

[FunctorMaterials]
  [fluid_props_to_mat_props]
    type = GeneralFunctorFluidProps
    fp = fp
    pressure = 'pressure'
    T_fluid = 'T_fluid'
    speed = 'velocity_norm'

    # To initialize with a high viscosity
    mu_rampdown = 'mu_rampdown'

    # For porous flow
    characteristic_length = 1
    porosity = 'porosity'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv'
    prop_values = '${h_fs}'
  []
[]

[Functions]
  [mu_rampdown]
    type = PiecewiseLinear
    x = '1 2 3 4'
    y = '1e3 1e2 1e1 1'
  []
[]

[AuxKernels]
  [speed]
    type = ParsedAux
    variable = 'velocity_norm'
    coupled_variables = 'superficial_vel_x superficial_vel_y porosity'
    expression = 'sqrt(superficial_vel_x*superficial_vel_x + superficial_vel_y*superficial_vel_y) / '
               'porosity'
  []
[]

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

  end_time = 3.0
[]

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideAverageValue
    variable = superficial_vel_x
    boundary = 'right'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'right'
  []
  [solid-temp]
    type = ElementAverageValue
    variable = T_solid
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-ambient-convection.i)

mu = 1
rho = 1
k = 1e-3
cp = 1
alpha = 1
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = -1
    ymax = 1
    nx = 50
    ny = 16
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
[]

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

  [energy_advection]
    type = INSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = FVDiffusion
    coeff = ${k}
    variable = T_fluid
  []
  [ambient_convection]
    type = NSFVEnergyAmbientConvection
    variable = T_fluid
    T_ambient = 100
    alpha = 'alpha'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = 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_t]
    type = FVDirichletBC
    boundary = 'left'
    variable = T_fluid
    value = 1
  []
[]

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

[Postprocessors]
  [temp]
    type = ElementAverageValue
    variable = T_fluid
  []
[]

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

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated.i)

mu = 1
rho = 1
k = 1e-3
cp = 1
u_inlet = 1
T_inlet = 200
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 2
    dx = '5 5'
    dy = '1.0'
    ix = '50 50'
    iy = '20'
    subdomain_id = '1 2'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  inactive = 'T_solid'
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${u_inlet}
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
  [T_solid]
    family = 'MONOMIAL'
    order = 'CONSTANT'
    fv = true
  []
[]

[AuxVariables]
  [T_solid]
    family = 'MONOMIAL'
    order = 'CONSTANT'
    fv = true
    initial_condition = 100
  []
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []
[]

[FVKernels]
  inactive = 'solid_energy_diffusion solid_energy_convection'
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []

  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    k = ${k}
    variable = T_fluid
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []

  [solid_energy_diffusion]
    type = FVDiffusion
    coeff = ${k}
    variable = T_solid
  []
  [solid_energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_solid
    is_solid = true
    T_fluid = 'T_fluid'
    T_solid = 'T_solid'
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  inactive = 'heated-side'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    function = ${u_inlet}
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    function = 0
  []
  [inlet-T]
    type = FVNeumannBC
    variable = T_fluid
    value = '${fparse u_inlet * rho * cp * T_inlet}'
    boundary = 'left'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = superficial_vel_y
    function = 0
  []
  [heated-side]
    type = FVDirichletBC
    boundary = 'top'
    variable = 'T_solid'
    value = 150
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0.1
  []
[]

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv'
    prop_values = '1'
  []
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '${cp}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  nl_rel_tol = 1e-14
[]

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideAverageValue
    variable = superficial_vel_x
    boundary = 'right'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'right'
  []
  [solid-temp]
    type = ElementAverageValue
    variable = T_solid
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/2d-rc-rz-by-parts.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = 0
    ymax = 1
    nx = 40
    ny = 10
  []
  coord_type = 'RZ'
  rz_coord_axis = 'X'
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [v]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.5
  []
[]

[FVKernels]
  inactive = 'v_pressure_volumetric'
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressureFlux
    variable = u
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []
  [u_friction]
    type = PINSFVMomentumFriction
    variable = u
    momentum_component = 'x'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = v
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = v
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure_volumetric]
    type = PINSFVMomentumPressure
    variable = v
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []
  [v_pressure_by_parts_flux]
    type = PINSFVMomentumPressureFlux
    variable = v
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []
  [v_pressure_by_parts_volume_term]
    type = PNSFVMomentumPressureFluxRZ
    variable = v
    pressure = pressure
    porosity = porosity
    momentum_component = 'y'
  []
  [v_friction]
    type = PINSFVMomentumFriction
    variable = v
    momentum_component = 'y'
    Darcy_name = 'Darcy_coefficient'
    Forchheimer_name = 'Forchheimer_coefficient'
    rho = ${rho}
    speed = speed
    mu = ${mu}
  []
[]

[FVBCs]
  inactive = 'free-slip-u free-slip-v'
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = 0
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = u
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'top'
    variable = v
    function = 0
  []
  [free-slip-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = u
    momentum_component = 'x'
  []
  [free-slip-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'top'
    variable = v
    momentum_component = 'y'
  []
  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 0
  []
[]

[FunctorMaterials]
  [darcy]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'Darcy_coefficient Forchheimer_coefficient'
    prop_values = '0.1 0.1 0.1 0.1 0.1 0.1'
  []
  [speed]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = u
    superficial_vel_y = v
    porosity = porosity
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_shift_type'
  petsc_options_value = 'lu NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-11
  nl_abs_tol = 1e-14
[]

# Some basic Postprocessors to visually examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-outflow-bcs.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '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_u]
    type = INSFVMomentumAdvectionOutflowBC
    variable = vel_x
    u = vel_x
    v = vel_y
    boundary = 'right'
    momentum_component = 'x'
    rho = ${rho}
  []
  [outlet_v]
    type = INSFVMomentumAdvectionOutflowBC
    variable = vel_y
    u = vel_x
    v = vel_y
    boundary = 'right'
    momentum_component = 'y'
    rho = ${rho}
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

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

[Outputs]
  exodus = true
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/pins/mms/porosity_change/1d-rc-continuous.i)

mu = 1.5
rho = 1.1
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = CartesianMeshGenerator
    dim = 1
    dx = '1 1'
    ix = '15 15'
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    porosity = porosity
    pressure = pressure
  []
[]

[Problem]
  error_on_jacobian_nonzero_reallocation = true
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
  []
[]

[ICs]
  [porosity_continuous]
    type = FunctionIC
    variable = porosity
    function = smooth_jump
  []
[]

[Functions]
  [smooth_jump]
    type = ParsedFunction
    expression = '1 - 0.5 * 1 / (1 + exp(-30*(x-1)))'
  []

  # Generated by compute-functions-1d.py
  [exact_u]
    type = ParsedFunction
    expression = 'cos((1/2)*x*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '-mu*(1 - 0.5/(exp(30 - 30*x) + 1))*(-1/4*pi^2*cos((1/2)*x*pi)/(1 - 0.5/(exp(30 - 30*x) + 1)) - 15.0*pi*exp(30 - 30*x)*sin((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2) - 450.0*exp(30 - 30*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2) + 900.0*exp(60 - 60*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^3) + 450.0*exp(60 - 60*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^3*(exp(30 - 30*x) + 1)^4)) + 15.0*mu*(-1/2*pi*sin((1/2)*x*pi)/(1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*exp(30 - 30*x)*cos((1/2)*x*pi)/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2))*exp(30 - 30*x)/(exp(30 - 30*x) + 1)^2 - pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi)/(1 - 0.5/(exp(30 - 30*x) + 1)) + 15.0*rho*exp(30 - 30*x)*cos((1/2)*x*pi)^2/((1 - 0.5/(exp(30 - 30*x) + 1))^2*(exp(30 - 30*x) + 1)^2) + (1 - 0.5/(exp(30 - 30*x) + 1))*cos(x)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin(x)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = u
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []

  [u_pressure]
    type = PINSFVMomentumPressure
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []

  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    functor = 'exact_u'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[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'

  # ksp_gmres_restart bumped to 200 for linear convergence
  nl_max_its = 100
[]

[Postprocessors]
  [inlet_p]
    type = SideAverageValue
    variable = 'pressure'
    boundary = 'left'
  []
  [outlet-u]
    type = SideIntegralVariablePostprocessor
    variable = u
    boundary = 'right'
  []
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

[Outputs]
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/friction/2d-rc-friction.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 5
    ymin = -1
    ymax = 1
    nx = 50
    ny = 10
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[FVKernels]
  inactive = 'u_friction_quad v_friction_quad'
  [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}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
  []
  [u_friction_linear]
    type = PINSFVMomentumFriction
    variable = vel_x
    Darcy_name = friction_coefficient
    momentum_component = 'x'
    rho = ${rho}
    standard_friction_formulation = false
  []
  [u_friction_quad]
    type = PINSFVMomentumFriction
    variable = vel_x
    speed = speed
    Forchheimer_name = friction_coefficient
    momentum_component = 'x'
    rho = ${rho}
    standard_friction_formulation = false
  []

  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []
  [v_friction_linear]
    type = PINSFVMomentumFriction
    variable = vel_y
    Darcy_name = friction_coefficient
    momentum_component = 'y'
    rho = ${rho}
    standard_friction_formulation = false
  []
  [v_friction_quad]
    type = PINSFVMomentumFriction
    variable = vel_y
    speed = speed
    Forchheimer_name = friction_coefficient
    momentum_component = 'y'
    rho = ${rho}
    standard_friction_formulation = false
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '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'
  []
[]

[FunctorMaterials]
  inactive = exponential_friction_coefficient
  [friction_coefficient]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'friction_coefficient'
    prop_values = '25 25 25'
  []
  [speed_material]
    type = PINSFVSpeedFunctorMaterial
    superficial_vel_x = vel_x
    superficial_vel_y = vel_y
    porosity = 1
    vel_x = vel_x_mat
    vel_y = vel_y_mat
  []
  [Re_material]
    type = ReynoldsNumberFunctorMaterial
    speed = speed
    characteristic_length = 2
    rho = ${rho}
    mu = ${mu}
  []
  [exponential_coeff]
    type = ExponentialFrictionMaterial
    friction_factor_name = 'exponential_coeff'
    Re = Re
    c1 = 0.25
    c2 = 0.55
  []
  [exponential_friction_coefficient]
    type = ADGenericVectorFunctorMaterial
    prop_names = 'friction_coefficient'
    prop_values = 'exponential_coeff exponential_coeff exponential_coeff'
  []
[]

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

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/channel-flow/heated/2d-rc-heated-boussinesq.i)

mu = 1
rho = 1
k = 1e-3
cp = 1
v_inlet = 1
T_inlet = 200
advected_interp_method = 'average'
velocity_interp_method = 'rc'

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 2
    ymin = 0
    ymax = 10
    nx = 20
    ny = 100
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = superficial_vel_x
    v = superficial_vel_y
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [superficial_vel_x]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = 1e-6
  []
  [superficial_vel_y]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = ${v_inlet}
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [T_fluid]
    type = INSFVEnergyVariable
  []
[]

[AuxVariables]
  [T_solid]
    family = 'MONOMIAL'
    order = 'CONSTANT'
    fv = true
    initial_condition = 100
  []
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.4
  []
[]

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

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_x
    mu = ${mu}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_x
    momentum_component = 'x'
    pressure = pressure
    porosity = porosity
  []
  [u_gravity]
    type = PINSFVMomentumGravity
    variable = superficial_vel_x
    rho = ${rho}
    gravity = '0 -9.81 0'
    momentum_component = 'x'
    porosity = porosity
  []
  [u_boussinesq]
    type = PINSFVMomentumBoussinesq
    variable = superficial_vel_x
    T_fluid = 'T_fluid'
    rho = ${rho}
    ref_temperature = 150
    gravity = '0 -9.81 0'
    momentum_component = 'x'
    alpha_name = 'alpha_b'
    porosity = porosity
  []

  [v_advection]
    type = PINSFVMomentumAdvection
    variable = superficial_vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_viscosity]
    type = PINSFVMomentumDiffusion
    variable = superficial_vel_y
    mu = ${mu}
    porosity = porosity
    momentum_component = 'y'
  []
  [v_pressure]
    type = PINSFVMomentumPressure
    variable = superficial_vel_y
    momentum_component = 'y'
    pressure = pressure
    porosity = porosity
  []
  [v_gravity]
    type = PINSFVMomentumGravity
    variable = superficial_vel_y
    rho = ${rho}
    gravity = '-0 -9.81 0'
    momentum_component = 'y'
    porosity = porosity
  []
  [v_boussinesq]
    type = PINSFVMomentumBoussinesq
    variable = superficial_vel_y
    T_fluid = 'T_fluid'
    rho = ${rho}
    ref_temperature = 150
    gravity = '0 -9.81 0'
    momentum_component = 'y'
    alpha_name = 'alpha_b'
    porosity = porosity
  []

  [energy_advection]
    type = PINSFVEnergyAdvection
    variable = T_fluid
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = ${advected_interp_method}
  []
  [energy_diffusion]
    type = PINSFVEnergyDiffusion
    k = ${k}
    variable = T_fluid
    porosity = porosity
  []
  [energy_convection]
    type = PINSFVEnergyAmbientConvection
    variable = T_fluid
    is_solid = false
    T_fluid = T_fluid
    T_solid = T_solid
    h_solid_fluid = 'h_cv'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_x
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = superficial_vel_y
    function = ${v_inlet}
  []
  [inlet-T]
    type = FVNeumannBC
    variable = T_fluid
    value = '${fparse v_inlet * rho * cp * T_inlet}'
    boundary = 'bottom'
  []

  [no-slip-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = superficial_vel_x
    function = 0
  []
  [no-slip-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = superficial_vel_y
    function = 0
  []

  [symmetry-u]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = superficial_vel_x
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'x'
  []
  [symmetry-v]
    type = PINSFVSymmetryVelocityBC
    boundary = 'left'
    variable = superficial_vel_y
    u = superficial_vel_x
    v = superficial_vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [symmetry-p]
    type = INSFVSymmetryPressureBC
    boundary = 'left'
    variable = pressure
  []

  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
[]

[FunctorMaterials]
  [constants]
    type = ADGenericFunctorMaterial
    prop_names = 'h_cv alpha_b'
    prop_values = '1e-3 8e-4'
  []
  [functor_constants]
    type = ADGenericFunctorMaterial
    prop_names = 'cp'
    prop_values = '${cp}'
  []

  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    temperature = 'T_fluid'
  []
[]

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

# Some basic Postprocessors to examine the solution
[Postprocessors]
  [inlet-p]
    type = SideAverageValue
    variable = pressure
    boundary = 'top'
  []
  [outlet-v]
    type = SideAverageValue
    variable = superficial_vel_y
    boundary = 'top'
  []
  [outlet-temp]
    type = SideAverageValue
    variable = T_fluid
    boundary = 'top'
  []
[]

[Outputs]
  exodus = true
  csv = false
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/2d-rc-no-slip-average-outlet-pressure-constraint.i)

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

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    nx = 100
    ny = 20
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [lambda]
    family = SCALAR
    order = FIRST
  []
[]

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

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    function = '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 = INSFVAveragePressureValueBC
    variable = pressure
    lambda = lambda
    phi0 = 0
    boundary = 'right'
  []
[]

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

[Outputs]
  [out]
    type = Exodus
    hide = 'lambda'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/3d-rc-no-slip.i)

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

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 10
    ymin = -1
    ymax = 1
    zmin = -1
    zmax = 1
    nx = 20
    ny = 4
    nz = 4
    elem_type = TET4
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    w = w
    pressure = pressure
  []
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1
  []
  [v]
    type = INSFVVelocityVariable
  []
  [w]
    type = INSFVVelocityVariable
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

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

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

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

  [w_advection]
    type = INSFVMomentumAdvection
    variable = w
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'z'
  []
  [w_viscosity]
    type = INSFVMomentumDiffusion
    variable = w
    mu = ${mu}
    momentum_component = 'z'
  []
  [w_pressure]
    type = INSFVMomentumPressure
    variable = w
    momentum_component = 'z'
    pressure = pressure
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [inlet-w]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = w
    function = '0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom front back'
    variable = u
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom front back'
    variable = v
    function = 0
  []
  [walls-w]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom front back'
    variable = w
    function = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -pc_factor_mat_solver_type -pc_factor_shift_type'
  petsc_options_value = 'lu       mumps                      NONZERO'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
  csv = true
  [dof]
    type = DOFMap
    execute_on = 'initial'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/two_phase/mixture_model/channel-drift-flux-w-interface-area.i)

mu = 10.0
rho = 100.0
mu_d = 1.0
rho_d = 1.0
l = 2
U = 1
dp = 0.01
inlet_phase_2 = 0.0
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'
mass_exchange_coeff = 0.01

[GlobalParams]
  rhie_chow_user_object = 'rc'
  density_interp_method = 'average'
  mu_interp_method = 'average'
[]

[Problem]
  identify_variable_groups_in_nl = false
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = '${fparse l * 5}'
    ymin = '${fparse -l / 2}'
    ymax = '${fparse l / 2}'
    nx = 20
    ny = 5
  []
  uniform_refine = 0
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 0
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 0
  []
  [pressure]
    type = INSFVPressureVariable
  []
  [phase_2]
    type = INSFVScalarFieldVariable
  []
  [interface_area]
    type = INSFVScalarFieldVariable
  []
[]

[FVKernels]

  inactive = 'u_time v_time phase_2_time interface_area_time'

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

  [u_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_x
    rho = 'rho_mixture'
    momentum_component = 'x'
  []
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = 'rho_mixture'
    momentum_component = 'x'
  []
  [u_drift]
    type = WCNSFV2PMomentumDriftFlux
    variable = vel_x
    rho_d = ${rho_d}
    fd = 'rho_mixture_var'
    u_slip = 'vel_slip_x'
    v_slip = 'vel_slip_y'
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = 'mu_mixture'
    limit_interpolation = true
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
  []

  [v_time]
    type = INSFVMomentumTimeDerivative
    variable = vel_y
    rho = 'rho_mixture'
    momentum_component = 'y'
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = 'rho_mixture'
    momentum_component = 'y'
  []
  [v_drift]
    type = WCNSFV2PMomentumDriftFlux
    variable = vel_y
    rho_d = ${rho_d}
    fd = 'rho_mixture_var'
    u_slip = 'vel_slip_x'
    v_slip = 'vel_slip_y'
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = 'mu_mixture'
    limit_interpolation = true
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []

  [phase_2_time]
    type = FVFunctorTimeKernel
    variable = phase_2
    functor = phase_2
  []
  [phase_2_advection]
    type = INSFVScalarFieldAdvection
    variable = phase_2
    u_slip = 'vel_slip_x'
    v_slip = 'vel_slip_y'
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = 'upwind'
  []
  [phase_2_diffusion]
    type = FVDiffusion
    variable = phase_2
    coeff = 1.0
  []
  [phase_2_src]
    type = NSFVMixturePhaseInterface
    variable = phase_2
    phase_coupled = phase_1
    alpha = ${mass_exchange_coeff}
  []

  [interface_area_time]
    type = FVFunctorTimeKernel
    variable = interface_area
    functor = interface_area
  []
  [interface_area_advection]
    type = INSFVScalarFieldAdvection
    variable = interface_area
    velocity_interp_method = ${velocity_interp_method}
    advected_interp_method = 'upwind'
  []
  [interface_area_diffusion]
    type = FVDiffusion
    variable = interface_area
    coeff = 0.1
  []
  [interface_area_source_sink]
    type = WCNSFV2PInterfaceAreaSourceSink
    variable = interface_area
    u = 'vel_x'
    v = 'vel_y'
    L = 1.0
    rho = 'rho_mixture'
    rho_d = ${rho_d}
    pressure = 'pressure'
    k_c = ${fparse mass_exchange_coeff * 100.0}
    fd = 'phase_2'
    sigma = 1e-3
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_x
    functor = '${U}'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = vel_y
    functor = '0'
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_x
    function = 0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_y
    function = 0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
  [inlet_phase_2]
    type = FVDirichletBC
    boundary = 'left'
    variable = phase_2
    value = ${inlet_phase_2}
  []
  [inlet_interface_area]
    type = FVDirichletBC
    boundary = 'left'
    variable = interface_area
    value = 0.0
  []
[]

[AuxVariables]
  [drag_coefficient]
    type = MooseVariableFVReal
  []
  [rho_mixture_var]
    type = MooseVariableFVReal
  []
  [mu_mixture_var]
    type = MooseVariableFVReal
  []
[]

[AuxKernels]
  [populate_cd]
    type = FunctorAux
    variable = drag_coefficient
    functor = 'Darcy_coefficient'
  []
  [populate_rho_mixture_var]
    type = FunctorAux
    variable = rho_mixture_var
    functor = 'rho_mixture'
  []
  [populate_mu_mixture_var]
    type = FunctorAux
    variable = mu_mixture_var
    functor = 'mu_mixture'
  []
[]

[FunctorMaterials]
  [populate_u_slip]
    type = WCNSFV2PSlipVelocityFunctorMaterial
    slip_velocity_name = 'vel_slip_x'
    momentum_component = 'x'
    u = 'vel_x'
    v = 'vel_y'
    rho = ${rho}
    mu = 'mu_mixture'
    rho_d = ${rho_d}
    particle_diameter = ${dp}
    linear_coef_name = 'Darcy_coefficient'
  []
  [populate_v_slip]
    type = WCNSFV2PSlipVelocityFunctorMaterial
    slip_velocity_name = 'vel_slip_y'
    momentum_component = 'y'
    u = 'vel_x'
    v = 'vel_y'
    rho = ${rho}
    mu = 'mu_mixture'
    rho_d = ${rho_d}
    particle_diameter = ${dp}
    linear_coef_name = 'Darcy_coefficient'
  []
  [compute_phase_1]
    type = ADParsedFunctorMaterial
    property_name = phase_1
    functor_names = 'phase_2'
    expression = '1 - phase_2'
  []
  [CD]
    type = NSFVDispersePhaseDragFunctorMaterial
    rho = 'rho_mixture'
    mu = mu_mixture
    u = 'vel_x'
    v = 'vel_y'
    particle_diameter = ${dp}
  []
  [mixing_material]
    type = NSFVMixtureFunctorMaterial
    phase_2_names = '${rho} ${mu}'
    phase_1_names = '${rho_d} ${mu_d}'
    prop_names = 'rho_mixture mu_mixture'
    phase_1_fraction = 'phase_2'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  nl_rel_tol = 1e-10
  # dt = 0.1
  # end_time = 1.0
  # nl_max_its = 10
[]

[Debug]
  show_var_residual_norms = true
[]

[Preconditioning]
  [SMP]
    type = SMP
    full = true
    petsc_options_iname = '-pc_type -pc_factor_shift_type'
    petsc_options_value = 'lu       NONZERO'
  []
[]

[Outputs]
  exodus = true
[]

[Postprocessors]
  [Re]
    type = ParsedPostprocessor
    function = '${rho} * ${l} * ${U}'
    pp_names = ''
  []
  [rho_outlet]
    type = SideAverageValue
    boundary = 'right'
    variable = 'rho_mixture_var'
  []
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/segregated/diverger/diverger.i)

mu = 2.6
rho = 1.0
cp = 700
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

pressure_tag = "pressure_grad"

[Mesh]
  # uniform_refine = 1
  [fmg]
    type = FileMeshGenerator
    file = "diverger-2d.msh"
  []
[]

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[Problem]
  nl_sys_names = 'u_system v_system pressure_system energy_system'
  previous_nl_solution_required = true
  error_on_jacobian_nonzero_reallocation = true
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolatorSegregated
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 0.5
    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]
    type = INSFVEnergyVariable
    two_term_boundary_expansion = false
    solver_sys = energy_system
    initial_condition = 700
  []
[]

[FVKernels]
  [u_advection]
    type = INSFVMomentumAdvection
    variable = vel_x
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'x'
  []
  [u_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_x
    mu = ${mu}
    momentum_component = 'x'
  []
  [u_pressure]
    type = INSFVMomentumPressure
    variable = vel_x
    momentum_component = 'x'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [v_advection]
    type = INSFVMomentumAdvection
    variable = vel_y
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
    extra_vector_tags = ${pressure_tag}
  []
  [p_diffusion]
    type = FVAnisotropicDiffusion
    variable = pressure
    coeff = "Ainv"
    coeff_interp_method = 'average'
  []
  [p_source]
    type = FVDivergence
    variable = pressure
    vector_field = "HbyA"
    force_boundary_execution = true
  []

  [heat_advection]
    type = INSFVEnergyAdvection
    variable = T
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
  []
  [heat_diffusion]
    type = FVDiffusion
    variable = T
    coeff = '10'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'inlet'
    variable = vel_x
    function = '1.1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'inlet'
    variable = vel_y
    function = '0.0'
  []
  [inlet-T]
    type = FVDirichletBC
    boundary = 'inlet'
    value = 700
    variable = T
  []
  [walls-u]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_x
    function = 0.0
  []
  [walls-v]
    type = INSFVNoSlipWallBC
    boundary = 'top bottom'
    variable = vel_y
    function = 0.0
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'outlet'
    variable = pressure
    function = 1.4
  []
  [zerograd-p]
    type = FVNeumannBC
    boundary = 'top bottom inlet'
    variable = pressure
    value = 0
  []
[]
[FunctorMaterials]
  [mu]
    type = ADGenericFunctorMaterial #defines mu artificially for numerical convergence
    prop_names = 'mu rho cp' #it converges to the real mu eventually.
    prop_values = '${mu} ${rho} ${cp}'
  []
  [ins_fv]
    type = INSFVEnthalpyFunctorMaterial
    rho = ${rho}
    cp = ${cp}
    temperature = 'T'
  []
[]

[Executioner]
  type = SIMPLENonlinearAssembly
  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 v_system'
  pressure_system = 'pressure_system'
  energy_system = 'energy_system'
  pressure_gradient_tag = ${pressure_tag}
  momentum_equation_relaxation = 0.8
  pressure_variable_relaxation = 0.3
  num_iterations = 100
  pressure_absolute_tolerance = 1e-13
  momentum_absolute_tolerance = 1e-13
  energy_absolute_tolerance = 1e-13
  print_fields = false
  continue_on_max_its = true
[]

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

(modules/navier_stokes/test/tests/finite_volume/ins/mixing_length_eddy_viscosity_aux/steady.i)

von_karman_const = 0.41

H = 1 #halfwidth of the channel
L = 150

Re = 100

rho = 1
bulk_u = 1
mu = '${fparse rho * bulk_u * 2 * H / Re}'

advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[GlobalParams]
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = u
    v = v
    pressure = pressure
  []
[]

[Mesh]
  [gen]
    type = CartesianMeshGenerator
    dim = 2
    dx = '${L}'
    dy = '0.667 0.333'
    ix = '200'
    iy = '10  1'
  []
[]

[Problem]
  fv_bcs_integrity_check = false
[]

[Variables]
  [u]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [v]
    type = INSFVVelocityVariable
    initial_condition = 1e-6
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [mixing_len]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_shear_stress]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [wall_yplus]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
  [eddy_viscosity]
    order = CONSTANT
    family = MONOMIAL
    fv = true
  []
[]

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

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

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

[AuxKernels]
  [mixing_len]
    type = WallDistanceMixingLengthAux
    walls = 'top'
    variable = mixing_len
    execute_on = 'initial'
    von_karman_const = ${von_karman_const}
    delta = 0.5
  []
  [turbulent_viscosity]
    type = INSFVMixingLengthTurbulentViscosityAux
    variable = eddy_viscosity
    mixing_length = mixing_len
    u = u
    v = v
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    function = '1'
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = v
    function = '0'
  []
  [wall-u]
    type = INSFVWallFunctionBC
    variable = u
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = x
  []
  [wall-v]
    type = INSFVWallFunctionBC
    variable = v
    boundary = 'top'
    u = u
    v = v
    mu = ${mu}
    rho = ${rho}
    momentum_component = y
  []
  [sym-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = u
    u = u
    v = v
    mu = ${mu}
    momentum_component = x
  []
  [sym-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'bottom'
    variable = v
    u = u
    v = v
    mu = ${mu}
    momentum_component = y
  []
  [symmetry_pressure]
    type = INSFVSymmetryPressureBC
    boundary = 'bottom'
    variable = pressure
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = '0'
  []
[]

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

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_volume/ins/channel-flow/cylindrical/no-slip-tris.i)

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

[GlobalParams]
  two_term_boundary_expansion = true
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = INSFVRhieChowInterpolator
    u = vel_x
    v = vel_y
    pressure = pressure
  []
[]

[Mesh]
  type = GeneratedMesh
  nx = 4
  ny = 4
  xmax = 3.9
  ymax = 4.1
  elem_type = TRI3
  dim = 2
[]

[Problem]
  coord_type = 'RZ'
[]

[Variables]
  [vel_x]
    type = INSFVVelocityVariable
    initial_condition = 1e-15
  []
  [vel_y]
    type = INSFVVelocityVariable
    initial_condition = 1e-15
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[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}
    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
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    momentum_component = 'y'
    # we can think of the axis as a slip wall boundary, no normal velocity and no viscous shear
  []
  [v_viscosity]
    type = INSFVMomentumDiffusion
    variable = vel_y
    mu = ${mu}
    momentum_component = 'y'
  []
  [v_pressure]
    type = INSFVMomentumPressure
    variable = vel_y
    momentum_component = 'y'
    pressure = pressure
  []
[]

[FVBCs]
  active = 'inlet-u inlet-v free-slip-wall-u free-slip-wall-v outlet-p axis-u axis-v'

  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = vel_x
    function = 0
  []
  [inlet-v]
    type = INSFVInletVelocityBC
    boundary = 'bottom'
    variable = vel_y
    function = 1
  []
  [free-slip-wall-u]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = vel_x
    momentum_component = 'x'
  []
  [free-slip-wall-v]
    type = INSFVNaturalFreeSlipBC
    boundary = 'right'
    variable = vel_y
    momentum_component = 'y'
  []
  [no-slip-wall-u]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = vel_x
    function = 0
  []
  [no-slip-wall-v]
    type = INSFVNoSlipWallBC
    boundary = 'right'
    variable = vel_y
    function = 0
  []
  [outlet-p]
    type = INSFVOutletPressureBC
    boundary = 'top'
    variable = pressure
    function = 0
  []
  [axis-u]
    type = INSFVSymmetryVelocityBC
    boundary = 'left'
    variable = vel_x
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = x
  []
  [axis-v]
    type = INSFVSymmetryVelocityBC
    boundary = 'left'
    variable = vel_y
    u = vel_x
    v = vel_y
    mu = ${mu}
    momentum_component = y
  []
  [axis-p]
    type = INSFVSymmetryPressureBC
    boundary = 'left'
    variable = pressure
  []
[]

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

[Debug]
  show_var_residual_norms = true
[]

[Postprocessors]
  [in]
    type = SideIntegralVariablePostprocessor
    variable = vel_y
    boundary = 'bottom'
  []
  [out]
    type = SideIntegralVariablePostprocessor
    variable = vel_y
    boundary = 'top'
  []
  [num_lin]
    type = NumLinearIterations
    outputs = 'console'
  []
  [num_nl]
    type = NumNonlinearIterations
    outputs = 'console'
  []
  [cum_lin]
    type = CumulativeValuePostprocessor
    outputs = 'console'
    postprocessor = 'num_lin'
  []
  [cum_nl]
    type = CumulativeValuePostprocessor
    outputs = 'console'
    postprocessor = 'num_nl'
  []
[]

[Outputs]
  exodus = true
  csv = true
[]

(modules/navier_stokes/test/tests/finite_volume/pins/mms/1d-rc-no-diffusion.i)

mu = 1e-15
rho = 1.1
advected_interp_method = 'upwind'
velocity_interp_method = 'rc'

[Mesh]
  [mesh]
    type = GeneratedMeshGenerator
    dim = 1
    nx = 2
    xmax = 0.5
  []
[]

[GlobalParams]
  two_term_boundary_expansion = true
  rhie_chow_user_object = 'rc'
[]

[UserObjects]
  [rc]
    type = PINSFVRhieChowInterpolator
    u = u
    pressure = pressure
    porosity = porosity
  []
[]

[Variables]
  [u]
    type = PINSFVSuperficialVelocityVariable
    initial_condition = .1
  []
  [pressure]
    type = INSFVPressureVariable
  []
[]

[AuxVariables]
  [porosity]
    family = MONOMIAL
    order = CONSTANT
    fv = true
    initial_condition = 0.8
  []
[]

[Problem]
  error_on_jacobian_nonzero_reallocation = true
[]

[Functions]
  [exact_u]
    type = ParsedFunction
    expression = 'cos((1/2)*x*pi)'
  []
  [forcing_u]
    type = ParsedFunction
    expression = '-1.25*pi*rho*sin((1/2)*x*pi)*cos((1/2)*x*pi) + 0.8*cos(x)'
    symbol_names = 'mu rho'
    symbol_values = '${mu} ${rho}'
  []
  [exact_p]
    type = ParsedFunction
    expression = 'sin(x)'
  []
  [forcing_p]
    type = ParsedFunction
    expression = '-1/2*pi*rho*sin((1/2)*x*pi)'
    symbol_names = 'rho'
    symbol_values = '${rho}'
  []
[]

[FVKernels]
  [mass]
    type = PINSFVMassAdvection
    variable = pressure
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
  []
  [mass_forcing]
    type = FVBodyForce
    variable = pressure
    function = forcing_p
  []

  [u_advection]
    type = PINSFVMomentumAdvection
    variable = u
    advected_interp_method = ${advected_interp_method}
    velocity_interp_method = ${velocity_interp_method}
    rho = ${rho}
    porosity = porosity
    momentum_component = 'x'
  []
  [u_pressure]
    type = PINSFVMomentumPressureFlux
    variable = u
    pressure = pressure
    porosity = porosity
    momentum_component = 'x'
  []
  [u_forcing]
    type = INSFVBodyForce
    variable = u
    functor = forcing_u
    momentum_component = 'x'
  []
[]

[FVBCs]
  [inlet-u]
    type = INSFVInletVelocityBC
    boundary = 'left'
    variable = u
    functor = 'exact_u'
  []
  [outlet_p]
    type = INSFVOutletPressureBC
    boundary = 'right'
    variable = pressure
    function = 'exact_p'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type -ksp_gmres_restart -sub_pc_type -sub_pc_factor_shift_type'
  petsc_options_value = 'asm      100                lu           NONZERO'
  line_search = 'bt'
[]

[Postprocessors]
  [h]
    type = AverageElementSize
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2u]
    type = ElementL2FunctorError
    approximate = u
    exact = exact_u
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
  [L2p]
    approximate = pressure
    exact = exact_p
    type = ElementL2FunctorError
    outputs = 'console csv'
    execute_on = 'timestep_end'
  []
[]

[Outputs]
  csv = true
[]