- functionThe function to use for controlling the specified parameter.
C++ Type:FunctionName
Unit:(no unit assumed)
Controllable:No
Description:The function to use for controlling the specified parameter.
- parameterThe input parameter(s) to control. Specify a single parameter name and all parameters in all objects matching the name will be updated
C++ Type:std::string
Controllable:No
Description:The input parameter(s) to control. Specify a single parameter name and all parameters in all objects matching the name will be updated
RealFunctionControl
The RealFunctionControl object is designed to control a "Real" parameter with a function rather than use the value specified in the input file. This object is mainly a demonstration of how to create a Control object and modify a parameter.
Example
Consider a simulation that solves the diffusion equation, where the Laplacian term has a coefficient, but the coefficient is defined as a constant input parameter ("coef"). For some reason, it is desired to control this coefficient and replace the constant value with a function that varies with space and time; this function is defined in the Functions block.
The RealFunctionControl object is designed for this purpose as shown in Listing 1.
Listing 1: Control block demonstrating the use of the RealFunctionControl object.
[Controls<<<{"href": "../../syntax/Controls/index.html"}>>>]
[./func_control]
type = RealFunctionControl<<<{"description": "Sets the value of a 'Real' input parameters to the value of a provided function.", "href": "RealFunctionControl.html"}>>>
parameter<<<{"description": "The input parameter(s) to control. Specify a single parameter name and all parameters in all objects matching the name will be updated"}>>> = '*/*/coef'
function<<<{"description": "The function to use for controlling the specified parameter."}>>> = 'func_coef'
execute_on<<<{"description": "The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html."}>>> = 'initial timestep_begin'
[../]
[]Notice that the "parameter" input parameter is expecting a parameter name which can be defined in various forms.
For a discussion on the naming of objects and parameters see Object and Parameter Names section.
Input Parameters
- depends_onThe Controls that this control relies upon (i.e. must execute before this one)
C++ Type:std::vector<std::string>
Controllable:No
Description:The Controls that this control relies upon (i.e. must execute before this one)
- execute_onINITIAL TIMESTEP_ENDThe list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
Default:INITIAL TIMESTEP_END
C++ Type:ExecFlagEnum
Options:XFEM_MARK, FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, LINEAR_CONVERGENCE, NONLINEAR, NONLINEAR_CONVERGENCE, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, MULTIAPP_FIXED_POINT_CONVERGENCE, FINAL, CUSTOM, PRE_MULTIAPP_SETUP
Controllable:No
Description:The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
Optional Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:No
Description:Set the enabled status of the MooseObject.
- implicitTrueDetermines whether this object is calculated using an implicit or explicit form
Default:True
C++ Type:bool
Controllable:No
Description:Determines whether this object is calculated using an implicit or explicit form
Advanced Parameters
Input Files
- (modules/subchannel/validation/EBR-II/XX09_SCM_TR45R.i)
- (modules/navier_stokes/test/tests/finite_volume/controls/switch-pressure-bc/switch_vel_pres_bc.i)
- (modules/solid_mechanics/examples/wave_propagation/cantilever_sweep.i)
- (test/tests/controls/dependency/test.i)
- (test/tests/controls/real_function_control/real_function_control.i)
- (test/tests/controls/real_function_control/multi_real_function_control.i)
- (modules/subchannel/validation/EBR-II/XX09_SCM_TR17.i)
- (test/tests/controls/control_piecewise/controlled_piecewise.i)
- (test/tests/postprocessors/constant/receiver.i)
(test/tests/controls/real_function_control/real_function_control.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 10
dt = 0.1
dtmin = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
[Functions]
[./func_coef]
type = ParsedFunction
expression = '2*t + 0.1'
[../]
[]
[Postprocessors]
[./coef]
type = RealControlParameterReporter
parameter = 'Kernels/diff/coef'
[../]
[]
[Controls]
[./func_control]
type = RealFunctionControl
parameter = '*/*/coef'
function = 'func_coef'
execute_on = 'initial timestep_begin'
[../]
[]
(modules/subchannel/validation/EBR-II/XX09_SCM_TR45R.i)
# Following Benchmark Specifications and Data Requirements for EBR-II Shutdown Heat Removal Tests SHRT-17 and SHRT-45R
# Available at: https://publications.anl.gov/anlpubs/2012/06/73647.pdf
# Transient Subchannel calculation
###################################################
# Thermal-hydraulics parameters
###################################################
T_in = 616.4 #Kelvin
Total_Surface_Area = 0.000854322 #m3
mass_flux_in = '${fparse 2.427 / Total_Surface_Area}'
P_out = 2.0e5
Power_initial = 379800 #W (Page 26,35 of ANL document)
###################################################
# Geometric parameters
###################################################
scale_factor = 0.01
fuel_pin_pitch = '${fparse 0.5664*scale_factor}'
fuel_pin_diameter = '${fparse 0.4419*scale_factor}'
wire_z_spacing = '${fparse 15.24*scale_factor}'
wire_diameter = '${fparse 0.1244*scale_factor}'
inner_duct_in = '${fparse 4.64*scale_factor}'
n_rings = 5
heated_length = '${fparse 34.3*scale_factor}'
unheated_length_exit = '${fparse 26.9*scale_factor}'
###################################################
[TriSubChannelMesh]
[subchannel]
type = SCMTriSubChannelMeshGenerator
nrings = ${n_rings}
n_cells = 50
flat_to_flat = ${inner_duct_in}
unheated_length_exit = ${unheated_length_exit}
heated_length = ${heated_length}
pin_diameter = ${fuel_pin_diameter}
pitch = ${fuel_pin_pitch}
dwire = ${wire_diameter}
hwire = ${wire_z_spacing}
spacer_z = '0.0'
spacer_k = '0.0'
[]
[fuel_pins]
type = SCMTriPinMeshGenerator
input = subchannel
nrings = ${n_rings}
n_cells = 50
unheated_length_exit = ${unheated_length_exit}
heated_length = ${heated_length}
pitch = ${fuel_pin_pitch}
[]
[]
[AuxVariables]
[mdot]
block = subchannel
[]
[SumWij]
block = subchannel
[]
[P]
block = subchannel
[]
[DP]
block = subchannel
[]
[h]
block = subchannel
[]
[T]
block = subchannel
[]
[rho]
block = subchannel
[]
[S]
block = subchannel
[]
[w_perim]
block = subchannel
[]
[mu]
block = subchannel
[]
[q_prime_init]
block = fuel_pins
[]
[power_history_field]
block = fuel_pins
[]
[q_prime]
block = fuel_pins
[]
[Tpin]
block = fuel_pins
[]
[Dpin]
block = fuel_pins
[]
[displacement]
block = subchannel
[]
[]
[FluidProperties]
[sodium]
type = PBSodiumFluidProperties
[]
[]
[Problem]
type = TriSubChannel1PhaseProblem
fp = sodium
n_blocks = 1
P_out = ${P_out}
CT = 2.6
compute_density = true
compute_viscosity = true
compute_power = true
P_tol = 1.0e-6
T_tol = 1.0e-5
implicit = true
segregated = false
interpolation_scheme = 'upwind'
[]
[ICs]
[S_IC]
type = SCMTriFlowAreaIC
variable = S
[]
[w_perim_IC]
type = SCMTriWettedPerimIC
variable = w_perim
[]
[q_prime_IC]
type = SCMTriPowerIC
variable = q_prime_init
power = ${Power_initial}
filename = "pin_power_profile61_uniform.txt"
[]
[T_ic]
type = ConstantIC
variable = T
value = ${T_in}
[]
[Dpin_ic]
type = ConstantIC
variable = Dpin
value = ${fuel_pin_diameter}
[]
[P_ic]
type = ConstantIC
variable = P
value = 0.0
[]
[DP_ic]
type = ConstantIC
variable = DP
value = 0.0
[]
[Viscosity_ic]
type = ViscosityIC
variable = mu
p = ${P_out}
T = T
fp = sodium
[]
[rho_ic]
type = RhoFromPressureTemperatureIC
variable = rho
p = ${P_out}
T = T
fp = sodium
[]
[h_ic]
type = SpecificEnthalpyFromPressureTemperatureIC
variable = h
p = ${P_out}
T = T
fp = sodium
[]
[mdot_ic]
type = ConstantIC
variable = mdot
value = 0.0
[]
[]
[Functions]
[power_func]
type = PiecewiseLinear
data_file = 'power_history_SHRT45.csv'
format = "columns"
scale_factor = 1.0
[]
[mass_flux_in]
type = PiecewiseLinear
data_file = 'massflow_SHRT45.csv'
format = "columns"
scale_factor = '${fparse mass_flux_in / 2.427}'
[]
[dts]
type = PiecewiseLinear
xy_data = '0.0 0.1
5.0 2.0
100 2.0
110 20.0
900 20.0'
[]
[]
[Controls]
[mass_flux_ctrl]
type = RealFunctionControl
parameter = 'Postprocessors/mass_flux_PP/value'
function = 'mass_flux_in'
execute_on = 'initial timestep_begin'
[]
[]
[AuxKernels]
[T_in_bc]
type = ConstantAux
variable = T
boundary = inlet
value = ${T_in}
execute_on = 'timestep_begin'
block = subchannel
[]
[mdot_in_bc]
type = SCMMassFlowRateAux
variable = mdot
boundary = inlet
area = S
mass_flux = mass_flux_PP
execute_on = 'timestep_begin'
[]
[populate_power_history]
type = FunctionAux
variable = power_history_field
function = 'power_func'
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[change_q_prime]
type = ParsedAux
variable = q_prime
args = 'q_prime_init power_history_field'
function = 'q_prime_init*power_history_field'
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[report_pressure_outlet]
type = Receiver
default = ${P_out}
[]
[TTC-31]
type = SubChannelPointValue
variable = T
index = 0
execute_on = 'initial timestep_end'
height = 0.322
[]
[post_func]
type = ElementIntegralVariablePostprocessor
block = fuel_pins
variable = q_prime
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[mass_flux_PP]
type = ConstantPostprocessor
value = ${mass_flux_in}
[]
[mass_flow_PP]
type = ParsedPostprocessor
expression = '${Total_Surface_Area} * mass_flux_PP'
pp_names = 'mass_flux_PP'
[]
[]
[Executioner]
type = Transient
start_time = -1
end_time = 900.0
[TimeStepper]
type = FunctionDT
function = dts
min_dt = 0.1
growth_factor = 2.0
[]
dtmax = 20
num_steps = 15
[]
################################################################################
# A multiapp that projects data to a detailed mesh
################################################################################
[MultiApps]
[viz]
type = TransientMultiApp
input_files = '3d_SCM_TR.i'
execute_on = 'INITIAL TIMESTEP_END'
catch_up = true
[]
[]
[Transfers]
[subchannel_transfer]
type = SCMSolutionTransfer
to_multi_app = viz
variable = 'mdot SumWij P DP h T rho mu S'
[]
[pin_transfer]
type = SCMPinSolutionTransfer
to_multi_app = viz
variable = 'Tpin q_prime'
[]
[]
(modules/navier_stokes/test/tests/finite_volume/controls/switch-pressure-bc/switch_vel_pres_bc.i)
rho = 'rho'
l = 10
inlet_area = 1
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_velocity = 0.001
end_time = 3.0
switch_time = 1.0
[Mesh]
[gen]
type = GeneratedMeshGenerator
dim = 2
xmin = 0
xmax = ${l}
ymin = 0
ymax = 1
nx = 10
ny = 5
[]
[]
[GlobalParams]
rhie_chow_user_object = 'rc'
[]
[UserObjects]
[rc]
type = INSFVRhieChowInterpolator
u = u
v = v
pressure = pressure
[]
[]
[Variables]
[u]
type = INSFVVelocityVariable
initial_condition = ${inlet_velocity}
[]
[v]
type = INSFVVelocityVariable
[]
[pressure]
type = INSFVPressureVariable
initial_condition = ${outlet_pressure}
[]
[T]
type = INSFVEnergyVariable
initial_condition = ${inlet_temp}
[]
[]
[AuxVariables]
[power_density]
type = MooseVariableFVReal
initial_condition = 1e4
[]
[]
[FVKernels]
[mass_time]
type = WCNSFVMassTimeDerivative
variable = pressure
drho_dt = drho_dt
[]
[mass]
type = INSFVMassAdvection
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
[]
[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]
# Inlet
[inlet_u]
type = WCNSFVSwitchableInletVelocityBC
variable = u
boundary = 'left'
mdot_pp = 'inlet_mdot'
area_pp = 'surface_inlet'
rho = 'rho'
switch_bc = true
face_limiter = 1.0
[]
[outlet_u]
type = WCNSFVSwitchableInletVelocityBC
variable = u
boundary = 'right'
mdot_pp = 'inlet_mdot'
area_pp = 'surface_inlet'
rho = 'rho'
switch_bc = false
scaling_factor = -1.0
face_limiter = 1.0
[]
[inlet_v]
type = WCNSFVInletVelocityBC
variable = v
boundary = 'left'
mdot_pp = 0
area_pp = 'surface_inlet'
rho = 'rho'
[]
[inlet_T]
type = WCNSFVInletTemperatureBC
variable = T
boundary = 'left'
temperature_pp = 'inlet_T'
[]
[outlet_T]
type = NSFVOutflowTemperatureBC
variable = T
boundary = 'right'
u = u
v = v
rho = 'rho'
cp = 'cp'
backflow_T = ${inlet_temp}
[]
[outlet_p]
type = INSFVSwitchableOutletPressureBC
variable = pressure
boundary = 'right'
function = ${outlet_pressure}
switch_bc = true
face_limiter = 1.0
[]
[inlet_p]
type = INSFVSwitchableOutletPressureBC
variable = pressure
boundary = 'left'
function = ${outlet_pressure}
switch_bc = false
face_limiter = 1.0
[]
# Walls
[no_slip_x]
type = INSFVNoSlipWallBC
variable = u
boundary = 'top bottom'
function = 0
[]
[no_slip_y]
type = INSFVNoSlipWallBC
variable = v
boundary = 'top bottom'
function = 0
[]
[]
[Functions]
[func_coef]
type = ParsedFunction
expression = 'if(t<${switch_time} | t>2.0*${switch_time}, 1, 0)'
[]
[func_coef_comp]
type = ParsedFunction
expression = 'if(t<${switch_time} | t>2.0*${switch_time}, 0, 1)'
[]
[mass_flux_and_pressure_test_scaling]
type = ParsedFunction
expression = 'if(t<${switch_time} | t>2.0*${switch_time}, 0.1, 0.2)'
[]
[]
[Controls]
[func_control_u_inlet]
type = BoolFunctionControl
parameter = 'FVBCs/inlet_u/switch_bc'
function = 'func_coef'
execute_on = 'initial timestep_begin'
[]
[func_control_u_outlet]
type = BoolFunctionControl
parameter = 'FVBCs/outlet_u/switch_bc'
function = 'func_coef_comp'
execute_on = 'initial timestep_begin'
[]
[func_control_p_outlet]
type = BoolFunctionControl
parameter = 'FVBCs/outlet_p/switch_bc'
function = 'func_coef'
execute_on = 'initial timestep_begin'
[]
[func_control_p_inlet]
type = BoolFunctionControl
parameter = 'FVBCs/inlet_p/switch_bc'
function = 'func_coef_comp'
execute_on = 'initial timestep_begin'
[]
[func_control_limiter_u_inlet]
type = RealFunctionControl
parameter = 'FVBCs/inlet_u/face_limiter'
function = 'mass_flux_and_pressure_test_scaling'
execute_on = 'initial timestep_begin'
[]
[func_control_limiter_u_outlet]
type = RealFunctionControl
parameter = 'FVBCs/outlet_u/face_limiter'
function = 'mass_flux_and_pressure_test_scaling'
execute_on = 'initial timestep_begin'
[]
[func_control_limiter_p_outlet]
type = RealFunctionControl
parameter = 'FVBCs/outlet_p/face_limiter'
function = 'mass_flux_and_pressure_test_scaling'
execute_on = 'initial timestep_begin'
[]
[func_control_limiter_p_inlet]
type = RealFunctionControl
parameter = 'FVBCs/inlet_p/face_limiter'
function = 'mass_flux_and_pressure_test_scaling'
execute_on = 'initial timestep_begin'
[]
[]
# used for the boundary conditions in this example
[Postprocessors]
[inlet_mdot]
type = Receiver
default = '${fparse 1980 * inlet_velocity * inlet_area}'
[]
[surface_inlet]
type = AreaPostprocessor
boundary = 'left'
execute_on = 'INITIAL'
[]
[inlet_T]
type = Receiver
default = ${inlet_temp}
[]
[outlet_mfr]
type = VolumetricFlowRate
boundary = 'right'
advected_quantity = 1.0
vel_x = u
vel_y = v
[]
[]
[FluidProperties]
[fp]
type = FlibeFluidProperties
[]
[]
[FunctorMaterials]
[const_functor]
type = ADGenericFunctorMaterial
prop_names = 'cp k'
prop_values = '${cp} ${k}'
[]
[rho]
type = RhoFromPTFunctorMaterial
fp = fp
temperature = T
pressure = pressure
[]
[ins_fv]
type = INSFVEnthalpyFunctorMaterial
temperature = 'T'
rho = ${rho}
[]
[]
[Executioner]
type = Transient
solve_type = 'NEWTON'
petsc_options_iname = '-pc_type -pc_factor_shift_type'
petsc_options_value = 'lu NONZERO'
dt = 0.1
end_time = ${end_time}
nl_abs_tol = 1e-12
nl_max_its = 50
line_search = 'none'
automatic_scaling = true
[]
[Outputs]
csv = true
execute_on = 'TIMESTEP_END'
[]
(modules/solid_mechanics/examples/wave_propagation/cantilever_sweep.i)
# Frequency Response function for cantilever beam:
# Analytic results: 509Hz and 763Hz
# Simulation results with coarse mesh: 600Hz and 800Hz
[Mesh]
type = GeneratedMesh
elem_type = HEX8
dim = 3
xmin=0
xmax=1
nx=10
ymin=0
ymax=0.1
ny = 1
zmin=0
zmax=0.15
nz = 2
[]
[GlobalParams]
order = FIRST
family = LAGRANGE
displacements = 'disp_x disp_y disp_z'
[]
[Problem]
type = ReferenceResidualProblem
reference_vector = 'ref'
extra_tag_vectors = 'ref'
group_variables = 'disp_x disp_y disp_z'
[]
[Physics]
[SolidMechanics]
[QuasiStatic]
[all]
strain = SMALL
add_variables = true
new_system = true
formulation = TOTAL
[]
[]
[]
[]
[Kernels]
#reaction terms
[reaction_realx]
type = Reaction
variable = disp_x
rate = 0# filled by controller
extra_vector_tags = 'ref'
[]
[reaction_realy]
type = Reaction
variable = disp_y
rate = 0# filled by controller
extra_vector_tags = 'ref'
[]
[reaction_realz]
type = Reaction
variable = disp_z
rate = 0# filled by controller
extra_vector_tags = 'ref'
[]
[]
[AuxVariables]
[disp_mag]
[]
[]
[AuxKernels]
[disp_mag]
type = ParsedAux
variable = disp_mag
coupled_variables = 'disp_x disp_y disp_z'
expression = 'sqrt(disp_x^2+disp_y^2+disp_z^2)'
[]
[]
[BCs]
#Left
[disp_x_left]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0.0
[]
[disp_y_left]
type = DirichletBC
variable = disp_y
boundary = 'left'
value = 0.0
[]
[disp_z_left]
type = DirichletBC
variable = disp_z
boundary = 'left'
value = 0.0
[]
#Right
[BC_right_yreal]
type = NeumannBC
variable = disp_y
boundary = 'right'
value = 1000
[]
[BC_right_zreal]
type = NeumannBC
variable = disp_z
boundary = 'right'
value = 1000
[]
[]
[Materials]
[elastic_tensor_Al]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 68e9
poissons_ratio = 0.36
[]
[compute_stress]
type = ComputeLagrangianLinearElasticStress
[]
[]
[Postprocessors]
[dispMag]
type = NodalExtremeValue
value_type = max
variable = disp_mag
[]
[]
[Functions]
[./freq2]
type = ParsedFunction
symbol_names = density
symbol_values = 2.7e3 #Al kg/m3
expression = '-t*t*density'
[../]
[]
[Controls]
[./func_control]
type = RealFunctionControl
parameter = 'Kernels/*/rate'
function = 'freq2'
execute_on = 'initial timestep_begin'
[../]
[]
[Executioner]
type = Transient
solve_type=LINEAR
petsc_options_iname = ' -pc_type'
petsc_options_value = 'lu'
start_time = 300 #starting frequency
end_time = 1200 #ending frequency
nl_abs_tol = 1e-6
[TimeStepper]
type = ConstantDT
dt = 50 #frequency stepsize
[]
[]
[Outputs]
csv=true
exodus=false
console = false
[]
(test/tests/controls/dependency/test.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[AuxVariables]
[./a]
family = SCALAR
order = FIRST
[../]
[]
[AuxScalarKernels]
[./a_sk]
type = ConstantScalarAux
variable = a
value = 0
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
[Functions]
[./func_coef]
type = ParsedFunction
expression = 1
[../]
[]
[Controls]
# We start with a = 0, control2 sets its value to 1 and then control1 will multiply it by 3,
# so the end value has to be 3. If dependecy is broken, we multiply by 3 and then set to 1,
# which is wrong
[./control1]
type = TestControl
parameter = 'AuxScalarKernels/a_sk/value'
test_type = MULT
execute_on = 'initial timestep_begin'
depends_on = control2
[../]
[./control2]
type = RealFunctionControl
parameter = 'AuxScalarKernels/a_sk/value'
function = 'func_coef'
execute_on = 'initial timestep_begin'
[../]
[]
(test/tests/controls/real_function_control/real_function_control.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[]
[Kernels]
[./diff]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time]
type = TimeDerivative
variable = u
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 10
dt = 0.1
dtmin = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
[Functions]
[./func_coef]
type = ParsedFunction
expression = '2*t + 0.1'
[../]
[]
[Postprocessors]
[./coef]
type = RealControlParameterReporter
parameter = 'Kernels/diff/coef'
[../]
[]
[Controls]
[./func_control]
type = RealFunctionControl
parameter = '*/*/coef'
function = 'func_coef'
execute_on = 'initial timestep_begin'
[../]
[]
(test/tests/controls/real_function_control/multi_real_function_control.i)
###########################################################
# This is a test of the Control Logic System. This test
# uses the RealFunctionControl to change a multiple Kernel
# coefficients based on an analytical function at the end
# of each timestep.
#
# @Requirement F8.10
###########################################################
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
[]
[Variables]
[./u]
[../]
[./v]
[../]
[]
[Kernels]
[./diff_u]
type = CoefDiffusion
variable = u
coef = 0.1
[../]
[./time_u]
type = TimeDerivative
variable = u
[../]
[./diff_v]
type = CoefDiffusion
variable = v
coef = 0.2
[../]
[./time_v]
type = TimeDerivative
variable = v
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = left
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = right
value = 1
[../]
[]
[Executioner]
type = Transient
num_steps = 5
dt = 0.1
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type'
petsc_options_value = 'hypre boomeramg'
[]
[Outputs]
csv = true
[]
[Functions]
[./func_coef]
type = ParsedFunction
expression = '2*t + 0.1'
[../]
[]
[Postprocessors]
[./u_coef]
type = RealControlParameterReporter
parameter = 'Kernels/diff_u/coef'
[../]
[./v_coef]
type = RealControlParameterReporter
parameter = 'Kernels/diff_v/coef'
[../]
[]
[Controls]
[./func_control]
type = RealFunctionControl
parameter = '*/*/coef'
function = 'func_coef'
execute_on = 'timestep_begin'
[../]
[]
(modules/subchannel/validation/EBR-II/XX09_SCM_TR17.i)
# Following Benchmark Specifications and Data Requirements for EBR-II Shutdown Heat Removal Tests SHRT-17 and SHRT-45R
# Available at: https://publications.anl.gov/anlpubs/2012/06/73647.pdf
# Transient Subchannel calculation
###################################################
# Thermal-hydraulics parameters
###################################################
T_in = 624.7 #Kelvin
Total_Surface_Area = 0.000854322 #m3
mass_flux_in = '${fparse 2.45 / Total_Surface_Area}'
P_out = 2.0e5
Power_initial = 486200 #W (Page 26,35 of ANL document)
###################################################
# Geometric parameters
###################################################
scale_factor = 0.01
fuel_pin_pitch = '${fparse 0.5664*scale_factor}'
fuel_pin_diameter = '${fparse 0.4419*scale_factor}'
wire_z_spacing = '${fparse 15.24*scale_factor}'
wire_diameter = '${fparse 0.1244*scale_factor}'
inner_duct_in = '${fparse 4.64*scale_factor}'
n_rings = 5
heated_length = '${fparse 34.3*scale_factor}'
unheated_length_exit = '${fparse 26.9*scale_factor}'
###################################################
[TriSubChannelMesh]
[subchannel]
type = SCMTriSubChannelMeshGenerator
nrings = ${n_rings}
n_cells = 50
flat_to_flat = ${inner_duct_in}
unheated_length_exit = ${unheated_length_exit}
heated_length = ${heated_length}
pin_diameter = ${fuel_pin_diameter}
pitch = ${fuel_pin_pitch}
dwire = ${wire_diameter}
hwire = ${wire_z_spacing}
spacer_z = '0.0'
spacer_k = '0.0'
[]
[fuel_pins]
type = SCMTriPinMeshGenerator
input = subchannel
nrings = ${n_rings}
n_cells = 50
unheated_length_exit = ${unheated_length_exit}
heated_length = ${heated_length}
pitch = ${fuel_pin_pitch}
[]
[]
[AuxVariables]
[mdot]
block = subchannel
[]
[SumWij]
block = subchannel
[]
[P]
block = subchannel
[]
[DP]
block = subchannel
[]
[h]
block = subchannel
[]
[T]
block = subchannel
[]
[rho]
block = subchannel
[]
[S]
block = subchannel
[]
[w_perim]
block = subchannel
[]
[mu]
block = subchannel
[]
[q_prime_init]
block = fuel_pins
[]
[power_history_field]
block = fuel_pins
[]
[q_prime]
block = fuel_pins
[]
[Tpin]
block = fuel_pins
[]
[Dpin]
block = fuel_pins
[]
[displacement]
block = subchannel
[]
[]
[FluidProperties]
[sodium]
type = PBSodiumFluidProperties
[]
[]
[Problem]
type = TriSubChannel1PhaseProblem
fp = sodium
n_blocks = 1
P_out = ${P_out}
CT = 2.6
compute_density = true
compute_viscosity = true
compute_power = true
P_tol = 1.0e-6
T_tol = 1.0e-5
implicit = true
segregated = false
interpolation_scheme = 'upwind'
[]
[ICs]
[S_IC]
type = SCMTriFlowAreaIC
variable = S
[]
[w_perim_IC]
type = SCMTriWettedPerimIC
variable = w_perim
[]
[q_prime_IC]
type = SCMTriPowerIC
variable = q_prime_init
power = ${Power_initial}
filename = "pin_power_profile61_uniform.txt"
[]
[T_ic]
type = ConstantIC
variable = T
value = ${T_in}
[]
[Dpin_ic]
type = ConstantIC
variable = Dpin
value = ${fuel_pin_diameter}
[]
[P_ic]
type = ConstantIC
variable = P
value = 0.0
[]
[DP_ic]
type = ConstantIC
variable = DP
value = 0.0
[]
[Viscosity_ic]
type = ViscosityIC
variable = mu
p = ${P_out}
T = T
fp = sodium
[]
[rho_ic]
type = RhoFromPressureTemperatureIC
variable = rho
p = ${P_out}
T = T
fp = sodium
[]
[h_ic]
type = SpecificEnthalpyFromPressureTemperatureIC
variable = h
p = ${P_out}
T = T
fp = sodium
[]
[mdot_ic]
type = ConstantIC
variable = mdot
value = 0.0
[]
[]
[Functions]
[power_func]
type = PiecewiseLinear
data_file = 'power_history_SHRT17.csv'
format = "columns"
scale_factor = 1.0
[]
[mass_flux_in]
type = PiecewiseLinear
data_file = 'massflow_SHRT17.csv'
format = "columns"
scale_factor = '${fparse mass_flux_in / 2.45}'
[]
[time_step_limiting]
type = PiecewiseLinear
xy_data = '0.1 0.1
10.0 10.0'
[]
[]
[Controls]
[mass_flux_ctrl]
type = RealFunctionControl
parameter = 'Postprocessors/mass_flux_PP/value'
function = 'mass_flux_in'
execute_on = 'initial timestep_begin'
[]
[]
[AuxKernels]
[T_in_bc]
type = ConstantAux
variable = T
boundary = inlet
value = ${T_in}
execute_on = 'timestep_begin'
block = subchannel
[]
[mdot_in_bc]
type = SCMMassFlowRateAux
variable = mdot
boundary = inlet
area = S
mass_flux = mass_flux_PP
execute_on = 'timestep_begin'
[]
[populate_power_history]
type = FunctionAux
variable = power_history_field
function = 'power_func'
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[change_q_prime]
type = ParsedAux
variable = q_prime
args = 'q_prime_init power_history_field'
function = 'q_prime_init*power_history_field'
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[]
[Outputs]
exodus = true
csv = true
[]
[Postprocessors]
[report_pressure_outlet]
type = Receiver
default = ${P_out}
[]
[TTC-31]
type = SubChannelPointValue
variable = T
index = 0
execute_on = 'initial timestep_end'
height = 0.322
[]
[post_func]
type = ElementIntegralVariablePostprocessor
block = fuel_pins
variable = q_prime
execute_on = 'INITIAL TIMESTEP_BEGIN'
[]
[mass_flux_PP]
type = ConstantPostprocessor
value = ${mass_flux_in}
[]
[mass_flow_PP]
type = ParsedPostprocessor
expression = '${Total_Surface_Area} * mass_flux_PP'
pp_names = 'mass_flux_PP'
[]
[]
[Executioner]
type = Transient
start_time = -1.0
end_time = 900.0
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.1
iteration_window = 5
optimal_iterations = 6
growth_factor = 1.1
cutback_factor = 0.8
timestep_limiting_function = 'time_step_limiting'
[]
dtmax = 20
num_steps = 15
[]
################################################################################
# A multiapp that projects data to a detailed mesh
################################################################################
[MultiApps]
[viz]
type = TransientMultiApp
input_files = '3d_SCM_TR.i'
execute_on = 'INITIAL TIMESTEP_END'
catch_up = true
[]
[]
[Transfers]
[subchannel_transfer]
type = SCMSolutionTransfer
to_multi_app = viz
variable = 'mdot SumWij P DP h T rho mu S'
[]
[pin_transfer]
type = SCMPinSolutionTransfer
to_multi_app = viz
variable = 'Tpin q_prime'
[]
[]
(test/tests/controls/control_piecewise/controlled_piecewise.i)
[Mesh]
[./generated]
type = GeneratedMeshGenerator
dim = 1
xmin = 0
xmax = 1
nx = 10
[../]
[]
[Problem]
kernel_coverage_check = false
[]
[Variables]
[./u]
initial_condition = 0.1
[../]
[]
[AuxVariables]
[./v]
[../]
[./x]
[../]
[]
[ICs]
[./x_ic]
type = FunctionIC
variable = x
function = 'x'
[../]
[]
[AuxKernels]
[./v_aux]
type = FunctionAux
variable = v
function = func
[../]
[]
[Controls]
[./func_control]
type = RealFunctionControl
parameter = '*/*/scale_factor'
function = '2'
execute_on = 'initial'
[../]
[]
[Materials]
[./mat]
type = PiecewiseLinearInterpolationMaterial
property = matprop
variable = x
x = '0 1'
y = '0 10'
outputs = all
[../]
[]
[Functions]
[./func]
type = PiecewiseLinear
x = '0 1'
y = '0 10'
axis = x
[../]
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(test/tests/postprocessors/constant/receiver.i)
[Mesh]
[mesh]
type = GeneratedMeshGenerator
dim = 1
nx = 1
[]
[]
[Problem]
type = FEProblem
solve = false
[]
[Executioner]
type = Transient
num_steps = 3
dt = 1
[]
[Controls]
[func_control]
type = RealFunctionControl
parameter = 'Postprocessors/recv/value'
function = 'val'
execute_on = 'timestep_begin'
[]
[]
[Functions]
[val]
type = ParsedFunction
expression = '1 + 2*t'
[]
[]
[Postprocessors]
[recv]
type = ConstantPostprocessor
[]
[]
[Outputs]
csv = true
[]