- componentThe name of the component to be controlled.
C++ Type:std::string
Controllable:No
Description:The name of the component to be controlled.
- parameterThe name of the parameter in the component to be controlled.
C++ Type:std::string
Controllable:No
Description:The name of the parameter in the component to be controlled.
- valueThe name of control data to be set in the component.
C++ Type:std::string
Controllable:No
Description:The name of control data to be set in the component.
SetComponentRealValueControl
commentnote
ControlData is only defined by the thermal hydraulics module control logic.
Example input syntax
In this example, the T0 parameter of the inlet component using the value ControlData of the T_inlet_fn ControlLogic.
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 100.e3
T0 = 350.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[ControlLogic]
[T_inlet_fn]
type = GetFunctionValueControl
function = T0_fn
[]
[set_inlet_value]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = T_inlet_fn:value
[]
[]
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)
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/thermal_hydraulics/tutorials/single_phase_flow/04_loop.i)
- (modules/thermal_hydraulics/test/tests/controls/set_component_real_value_control/test.i)
- (modules/thermal_hydraulics/test/tests/misc/coupling_mD_flow/thm_non_overlapping.i)
- (modules/thermal_hydraulics/test/tests/postprocessors/real_component_parameter_value/non_existent_par_name.i)
- (modules/thermal_hydraulics/tutorials/single_phase_flow/06_custom_closures.i)
- (modules/thermal_hydraulics/test/tests/controls/pid_control/test.i)
- (modules/thermal_hydraulics/test/tests/controls/dependency/test.i)
- (modules/thermal_hydraulics/test/tests/problems/brayton_cycle/recuperated_brayton_cycle.i)
- (modules/thermal_hydraulics/tutorials/single_phase_flow/05_secondary_side.i)
- (modules/thermal_hydraulics/test/tests/controls/error_checking/non_existent_control_data.i)
- (modules/thermal_hydraulics/test/tests/components/shaft_connected_turbine_1phase/turbine_startup.i)
(modules/thermal_hydraulics/test/tests/controls/set_component_real_value_control/test.i)
# This is testing that the values set by SetComponentRealValueControl are used.
# Function T0_fn prescribes values for T0 at inlet. We output the function
# values via a postprocessor `T_fn` and the inlet values via another
# postprocessor `T_ctrl`. Those two values have to be equal.
[GlobalParams]
initial_p = 100.e3
initial_vel = 1.0
initial_T = 350.
scaling_factor_1phase = '1 1e-2 1e-4'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 100.e3
T0 = 350.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[Functions]
[T0_fn]
type = PiecewiseLinear
x = '0 1'
y = '350 345'
[]
[]
[ControlLogic]
[T_inlet_fn]
type = GetFunctionValueControl
function = T0_fn
[]
[set_inlet_value]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = T_inlet_fn:value
[]
[]
[Postprocessors]
[T_fn]
type = FunctionValuePostprocessor
function = T0_fn
[]
[T_ctrl]
type = RealComponentParameterValuePostprocessor
component = inlet
parameter = T0
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
dt = 0.1
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 20
l_tol = 1e-3
l_max_its = 5
start_time = 0.0
end_time = 1
[]
[Outputs]
csv = true
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/04_loop.i)
T_in = 300. # K
m_dot_in = 1e-4 # kg/s
press = 1e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 10
core_dia = ${units 2. cm -> m}
core_pitch = ${units 8.7 cm -> m}
# pipe parameters
pipe_dia = ${units 10. cm -> m}
tot_power = 100 # W
[GlobalParams]
initial_p = ${press}
initial_vel = 0
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
rdg_slope_reconstruction = full
closures = simple_closures
fp = he
f = 0.4
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[HeatStructureMaterials]
[steel]
type = SolidMaterialProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
A = ${fparse core_pitch * core_pitch - pi * core_dia * core_dia / 4.}
D_h = ${core_dia}
f = 1.6
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
materials = 'steel'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = ${fparse pi * core_dia}
Hw = 1.36
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 1'
connections = 'core_chan:out up_pipe:in'
volume = 1e-3
[]
[up_pipe]
type = FlowChannel1Phase
position = '0 0 1'
orientation = '0 0 1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct2]
type = VolumeJunction1Phase
position = '0 0 2'
connections = 'up_pipe:out top_pipe:in'
volume = 1e-3
[]
[top_pipe]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct3]
type = VolumeJunction1Phase
position = '1 0 2'
connections = 'top_pipe:out cooling_pipe:in'
volume = 1e-3
[]
[cooling_pipe]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[cold_wall]
type = HeatTransferFromSpecifiedTemperature1Phase
flow_channel = cooling_pipe
T_wall = 300
Hw = 0.97
[]
[jct4]
type = VolumeJunction1Phase
position = '1 0 1'
connections = 'cooling_pipe:out down_pipe:in'
volume = 1e-3
[]
[down_pipe]
type = FlowChannel1Phase
position = '1 0 1'
orientation = '0 0 -1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct5]
type = VolumeJunction1Phase
position = '1 0 0'
connections = 'down_pipe:out bottom_b:in'
volume = 1e-3
[]
[bottom_b]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[pump]
type = Pump1Phase
position = '0.5 0 0'
connections = 'bottom_b:out bottom_a:in'
volume = 1e-3
A_ref = ${fparse pi * pipe_dia * pipe_dia / 4.}
head = 0
[]
[bottom_a]
type = FlowChannel1Phase
position = '0.5 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct6]
type = VolumeJunction1Phase
position = '0 0 0'
connections = 'bottom_a:out core_chan:in'
volume = 1e-3
[]
[]
[ControlLogic]
[set_point]
type = GetFunctionValueControl
function = ${m_dot_in}
[]
[pid]
type = PIDControl
initial_value = 0
set_point = set_point:value
input = m_dot_pump
K_p = 250
K_i = 0.5
K_d = 0
[]
[set_pump_head]
type = SetComponentRealValueControl
component = pump
parameter = head
value = pid:output
[]
[]
[Postprocessors]
[m_dot_pump]
type = ADFlowJunctionFlux1Phase
boundary = core_chan:in
connection_index = 1
equation = mass
junction = jct6
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = cooling_pipe:out
variable = T
[]
[]
[Executioner]
type = Transient
start_time = 0
end_time = 1000
dt = 10
line_search = basic
solve_type = NEWTON
nl_rel_tol = 1e-5
nl_abs_tol = 1e-5
nl_max_its = 5
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/test/tests/controls/set_component_real_value_control/test.i)
# This is testing that the values set by SetComponentRealValueControl are used.
# Function T0_fn prescribes values for T0 at inlet. We output the function
# values via a postprocessor `T_fn` and the inlet values via another
# postprocessor `T_ctrl`. Those two values have to be equal.
[GlobalParams]
initial_p = 100.e3
initial_vel = 1.0
initial_T = 350.
scaling_factor_1phase = '1 1e-2 1e-4'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 100.e3
T0 = 350.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[Functions]
[T0_fn]
type = PiecewiseLinear
x = '0 1'
y = '350 345'
[]
[]
[ControlLogic]
[T_inlet_fn]
type = GetFunctionValueControl
function = T0_fn
[]
[set_inlet_value]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = T_inlet_fn:value
[]
[]
[Postprocessors]
[T_fn]
type = FunctionValuePostprocessor
function = T0_fn
[]
[T_ctrl]
type = RealComponentParameterValuePostprocessor
component = inlet
parameter = T0
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
dt = 0.1
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 20
l_tol = 1e-3
l_max_its = 5
start_time = 0.0
end_time = 1
[]
[Outputs]
csv = true
[]
(modules/thermal_hydraulics/test/tests/misc/coupling_mD_flow/thm_non_overlapping.i)
T_in = 523.0
mdot = 10
pout = 7e6
[GlobalParams]
initial_p = ${pout}
initial_vel = 1
initial_T = ${T_in}
gravity_vector = '0 0 0'
closures = simple_closures
n_elems = 5
scaling_factor_1phase = '1 1e-2 1e-5'
f = 1
[]
[FluidProperties]
[fp]
type = IdealGasFluidProperties
gamma = 1.66
molar_mass = 0.004
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[inlet_bc]
type = InletMassFlowRateTemperature1Phase
input = 'inlet:in'
m_dot = ${mdot}
T = ${T_in}
[]
[inlet]
type = FlowChannel1Phase
fp = fp
position = '0 0 11'
orientation = '0 0 -1'
length = 1
A = 1
[]
[inlet_plenum]
type = VolumeJunction1Phase
position = '0 0 10'
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 1
connections = 'inlet:out bypass:in core_top:in'
volume = 1
[]
[bypass]
type = FlowChannel1Phase
fp = fp
position = '2 0 10'
orientation = '0 0 -1'
length = 10
A = 0.01
[]
[core_top]
type = FlowChannel1Phase
fp = fp
position = '0 0 10'
orientation = '0 0 -1'
length = 0.1
A = 9
[]
[core_top_bc]
type = Outlet1Phase
p = ${pout}
input = 'core_top:out'
[]
[core_bottom_bc]
type = InletMassFlowRateTemperature1Phase
input = 'core_bottom:in'
m_dot = ${mdot}
T = ${T_in}
[]
[core_bottom]
type = FlowChannel1Phase
fp = fp
position = '0 0 0.1'
orientation = '0 0 -1'
length = 0.1
A = 9
[]
[outlet_plenum]
type = VolumeJunction1Phase
position = '0 0 0'
initial_vel_x = 1
initial_vel_y = 0
initial_vel_z = 1
connections = 'bypass:out core_bottom:out outlet:in'
volume = 1
[]
[outlet]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '0 0 -1'
length = 1
A = 1
[]
[outlet_bc]
type = Outlet1Phase
p = ${pout}
input = 'outlet:out'
[]
[]
[ControlLogic]
[set_core_inlet_pressure]
type = SetComponentRealValueControl
component = core_top_bc
parameter = p
value = core_inlet_pressure
[]
[set_core_outlet_mdot]
type = SetComponentRealValueControl
component = core_bottom_bc
parameter = m_dot
value = core_outlet_mdot
[]
[set_core_outlet_temperature]
type = SetComponentRealValueControl
component = core_bottom_bc
parameter = T
value = core_outlet_temperature
[]
[]
[Postprocessors]
[core_inlet_pressure]
type = Receiver
default = ${pout}
[]
[core_outlet_mdot]
type = Receiver
default = ${mdot}
[]
[core_outlet_temperature]
type = Receiver
default = ${T_in}
[]
[core_outlet_pressure]
type = SideAverageValue
variable = p
boundary = 'core_bottom:in'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[]
[core_inlet_mdot]
type = SideAverageValue
variable = rhouA
boundary = 'core_top:out'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[]
[core_inlet_temperature]
type = SideAverageValue
variable = T
boundary = 'core_top:out'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[]
[bypass_inlet_pressure]
type = SideAverageValue
variable = p
boundary = 'bypass:in'
[]
[bypass_outlet_pressure]
type = SideAverageValue
variable = p
boundary = 'bypass:out'
[]
[bypass_pressure_drop]
type = DifferencePostprocessor
value1 = bypass_inlet_pressure
value2 = bypass_outlet_pressure
[]
[bypass_mdot]
type = SideAverageValue
variable = rhouA
boundary = 'bypass:out'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[]
[inlet_mdot]
type = SideAverageValue
variable = rhouA
boundary = 'inlet:in'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[]
[outlet_mdot]
type = SideAverageValue
variable = rhouA
boundary = 'outlet:out'
execute_on = 'INITIAL LINEAR TIMESTEP_END'
[]
[]
[Preconditioning]
[smp]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
timestep_tolerance = 1e-6
start_time = 0
end_time = 100
dt = 0.01
line_search = l2
nl_rel_tol = 1e-6
nl_abs_tol = 1e-4
nl_max_its = 25
l_tol = 1e-3
l_max_its = 20
petsc_options = '-snes_converged_reason'
petsc_options_iname = '-pc_type'
petsc_options_value = ' lu '
[]
[Outputs]
exodus = true
[]
(modules/thermal_hydraulics/test/tests/postprocessors/real_component_parameter_value/non_existent_par_name.i)
[GlobalParams]
gravity_vector = '0 0 0'
initial_p = 1e5
initial_T = 300
initial_vel = 0.0
scaling_factor_1phase = '1 1 1e-5'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
k = 0.5
mu = 281.8e-6
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
n_elems = 50
A = 1.0000000000e-04
D_h = 1.1283791671e-02
f = 0.0
fp = fp
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe:in'
p0 = 1e5
T0 = 300
[]
[outlet]
type = Outlet1Phase
input = 'pipe:out'
p = 1e5
[]
[]
[Functions]
[p_fn]
type = PiecewiseLinear
x = '0 1'
y = '1e5 1.001e5'
[]
[]
[ControlLogic]
[outlet_p_fn]
type = GetFunctionValueControl
function = p_fn
[]
[set_outlet_value]
type = SetComponentRealValueControl
component = outlet
parameter = p
value = outlet_p_fn:value
[]
[]
[Postprocessors]
[outlet_p]
type = RealComponentParameterValuePostprocessor
component = inlet
parameter = p
[]
[]
[Preconditioning]
[pc]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
start_time = 0.0
dt = 0.25
num_steps = 5
abort_on_solve_fail = true
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-5
nl_abs_tol = 1e-6
nl_max_its = 30
l_tol = 1e-3
l_max_its = 100
[Quadrature]
type = GAUSS
order = SECOND
[]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/06_custom_closures.i)
T_in = 300. # K
m_dot_in = 1e-4 # kg/s
press = 1e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 10
core_dia = ${units 2. cm -> m}
core_pitch = ${units 8.7 cm -> m}
# pipe parameters
pipe_dia = ${units 10. cm -> m}
tot_power = 100 # W
# heat exchanger parameters
hx_dia_inner = ${units 10. cm -> m}
hx_wall_thickness = ${units 5. mm -> m}
hx_dia_outer = ${units 50. cm -> m}
hx_radius_wall = ${fparse hx_dia_inner / 2. + hx_wall_thickness}
hx_length = 1 # m
hx_n_elems = 10
m_dot_sec_in = 1 # kg/s
flow_blocks = 'core_chan up_pipe top_pipe hx/pri hx/sec down_pipe bottom_b bottom_a'
ht_blocks = 'core_chan hx/pri hx/sec'
[GlobalParams]
initial_p = ${press}
initial_vel = 0
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
rdg_slope_reconstruction = full
closures = no_closures
fp = he
[]
[Functions]
[m_dot_sec_fn]
type = PiecewiseLinear
xy_data = '
0 0
100 ${m_dot_sec_in}'
[]
[]
[Materials]
[f_mat]
type = ADWallFrictionChurchillMaterial
block = ${flow_blocks}
D_h = D_h
f_D = f_D
mu = mu
rho = rho
vel = vel
[]
[Hw_mat]
type = ADWallHeatTransferCoefficient3EqnDittusBoelterMaterial
block = ${ht_blocks}
D_h = D_h
rho = rho
vel = vel
T = T
T_wall = T_wall
cp = cp
mu = mu
k = k
[]
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[water]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[no_closures]
type = Closures1PhaseNone
[]
[]
[HeatStructureMaterials]
[steel]
type = SolidMaterialProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
A = ${fparse core_pitch * core_pitch - pi * core_dia * core_dia / 4.}
D_h = ${core_dia}
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
materials = 'steel'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = ${fparse pi * core_dia}
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 1'
connections = 'core_chan:out up_pipe:in'
volume = 1e-3
[]
[up_pipe]
type = FlowChannel1Phase
position = '0 0 1'
orientation = '0 0 1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct2]
type = VolumeJunction1Phase
position = '0 0 2'
connections = 'up_pipe:out top_pipe:in'
volume = 1e-3
[]
[top_pipe]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct3]
type = VolumeJunction1Phase
position = '1 0 2'
connections = 'top_pipe:out hx/pri:in'
volume = 1e-3
[]
[hx]
[pri]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
A = ${fparse pi * hx_dia_inner * hx_dia_inner / 4.}
D_h = ${hx_dia_inner}
[]
[ht_pri]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = inner
flow_channel = hx/pri
[]
[wall]
type = HeatStructureCylindrical
position = '1 0 2'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
widths = '${hx_wall_thickness}'
n_part_elems = '3'
materials = 'steel'
names = '0'
inner_radius = ${fparse hx_dia_inner / 2.}
offset_mesh_by_inner_radius = true
[]
[ht_sec]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = outer
flow_channel = hx/sec
P_hf = ${fparse 2 * pi * hx_radius_wall}
[]
[sec]
type = FlowChannel1Phase
position = '${fparse 1 + hx_wall_thickness} 0 2'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
A = ${fparse pi * (hx_dia_outer * hx_dia_outer / 4. - hx_radius_wall * hx_radius_wall)}
D_h = ${fparse hx_dia_outer - (2 * hx_radius_wall)}
fp = water
[]
[]
[jct4]
type = VolumeJunction1Phase
position = '1 0 1'
connections = 'hx/pri:out down_pipe:in'
volume = 1e-3
[]
[down_pipe]
type = FlowChannel1Phase
position = '1 0 1'
orientation = '0 0 -1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct5]
type = VolumeJunction1Phase
position = '1 0 0'
connections = 'down_pipe:out bottom_b:in'
volume = 1e-3
[]
[bottom_b]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[pump]
type = Pump1Phase
position = '0.5 0 0'
connections = 'bottom_b:out bottom_a:in'
volume = 1e-3
A_ref = ${fparse pi * pipe_dia * pipe_dia / 4.}
head = 0
[]
[bottom_a]
type = FlowChannel1Phase
position = '0.5 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct6]
type = VolumeJunction1Phase
position = '0 0 0'
connections = 'bottom_a:out core_chan:in'
volume = 1e-3
[]
[inlet_sec]
type = InletMassFlowRateTemperature1Phase
input = 'hx/sec:out'
m_dot = 0
T = 300
[]
[outlet_sec]
type = Outlet1Phase
input = 'hx/sec:in'
p = ${press}
[]
[]
[ControlLogic]
[set_point]
type = GetFunctionValueControl
function = ${m_dot_in}
[]
[pid]
type = PIDControl
initial_value = 0
set_point = set_point:value
input = m_dot_pump
K_p = 250
K_i = 0.5
K_d = 0
[]
[set_pump_head]
type = SetComponentRealValueControl
component = pump
parameter = head
value = pid:output
[]
[m_dot_sec_inlet_ctrl]
type = GetFunctionValueControl
function = m_dot_sec_fn
[]
[set_m_dot_sec_ctrl]
type = SetComponentRealValueControl
component = inlet_sec
parameter = m_dot
value = m_dot_sec_inlet_ctrl:value
[]
[]
[Postprocessors]
[m_dot_pump]
type = ADFlowJunctionFlux1Phase
boundary = core_chan:in
connection_index = 1
equation = mass
junction = jct6
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = hx/pri:out
variable = T
[]
[hx_sec_T_in]
type = SideAverageValue
boundary = inlet_sec
variable = T
[]
[hx_sec_T_out]
type = SideAverageValue
boundary = outlet_sec
variable = T
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = SolutionTimeAdaptiveDT
dt = 1
[]
dtmax = 100
end_time = 50000
line_search = basic
solve_type = NEWTON
nl_rel_tol = 1e-5
nl_abs_tol = 1e-5
nl_max_its = 5
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/test/tests/controls/pid_control/test.i)
# This test "measures" the liquid temperature at location (10, 0, 0) on a 15 meters
# long pipe and adjusts the inlet stagnation temperature using a PID controller with
# set point at 340 K. The pipe is filled with water at T = 350 K. The purpose is to
# make sure that the channel fills with colder liquid and levels at the set point
# value. In steady state there should be a flat temperature profile at ~340 K.
[GlobalParams]
initial_p = 100.e3
initial_vel = 1.0
initial_T = 350.
scaling_factor_1phase = '1 1e-2 1e-4'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 105.e3
T0 = 300.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[ControlLogic]
[T_set_point]
type = GetFunctionValueControl
function = 340
[]
[pid_ctrl]
type = PIDControl
input = T_reading
set_point = T_set_point:value
K_i = 0.05
K_p = 0.2
K_d = 0.1
initial_value = 340
[]
[set_inlet_value]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = pid_ctrl:output
[]
[]
[Postprocessors]
[T_reading]
type = PointValue
point = '10 0 0'
variable = T
execute_on = timestep_begin
[]
[T_inlet]
type = PointValue
point = '0 0 0'
variable = T
execute_on = timestep_begin
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
dt = 5
abort_on_solve_fail = true
solve_type = 'NEWTON'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 20
l_tol = 1e-3
l_max_its = 5
start_time = 0.0
end_time = 300.0
[]
[Outputs]
[out]
type = CSV
execute_on = 'final'
[]
[console]
type = Console
max_rows = 1
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/test/tests/controls/dependency/test.i)
# This is testing that controls are executed in the correct order
#
# If controls are executed in the right order, then T_inlet_ctrl
# reads the value of temperature (T = 345 K) from a function. Then
# this value is set into the BC and then is it sampled by a
# postprocessor whose value is then written into a CSV file.
#
# If controls were executed in the wrong order, we would sample the
# stagnation temperature function at time t = 0, which would give
# T = 360 K back, and we would see this value in the CSV file instead.
[GlobalParams]
initial_p = 100.e3
initial_vel = 1.0
initial_T = 350.
scaling_factor_1phase = '1 1e-2 1e-4'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 100.e3
T0 = 355.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[Functions]
# Stagnation temperature in time
[T0_fn]
type = PiecewiseLinear
x = '0 1e-5'
y = '360 345'
[]
[]
[ControlLogic]
[set_inlet_value_ctrl]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = T_inlet_ctrl:value
[]
[T_inlet_ctrl]
type = GetFunctionValueControl
function = T0_fn
[]
[]
[Postprocessors]
[T_ctrl]
type = RealComponentParameterValuePostprocessor
component = inlet
parameter = T0
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
dt = 1e-5
num_steps = 1
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 20
l_tol = 1e-3
l_max_its = 5
[]
[Outputs]
csv = true
[]
(modules/thermal_hydraulics/test/tests/problems/brayton_cycle/recuperated_brayton_cycle.i)
# This input file models an open, recuperated Brayton cycle with a PID
# controlled start up using a coupled motor.
#
# Heat is supplied to the system by a volumetric heat source, and a second heat
# source is used to model a recuperator. The recuperator transfers heat from the
# turbine exhaust gas to the compressor outlet gas.
#
# Initially the fluid and heat structures are at rest at ambient conditions,
# and the shaft speed is zero.
# The transient is controlled as follows:
# * 0 - 2000 s: Motor increases shaft speed to approx. 85,000 RPM by PID control
# * 1000 - 8600 s: Power in main heat source increases from 0 - 104 kW
# * 2000 - 200000 s: Torque supplied by turbine increases to steady state level
# as working fluid temperature increases. Torque supplied by
# the motor is ramped down to 0 N-m transitioning shaft control
# to the turbine at its rated speed of 96,000 RPM.
I_motor = 1.0
I_generator = 1.0
generator_torque_per_shaft_speed = -0.00025
motor_ramp_up_duration = 3605
motor_ramp_down_duration = 1800
post_motor_time = 2160000
t1 = ${motor_ramp_up_duration}
t2 = ${fparse t1 + motor_ramp_down_duration}
t3 = ${fparse t2 + post_motor_time}
D1 = 0.15
D2 = ${D1}
D3 = ${D1}
D4 = ${D1}
D5 = ${D1}
D6 = ${D1}
D7 = ${D1}
D8 = ${D1}
A1 = ${fparse 0.25 * pi * D1^2}
A2 = ${fparse 0.25 * pi * D2^2}
A3 = ${fparse 0.25 * pi * D3^2}
A4 = ${fparse 0.25 * pi * D4^2}
A5 = ${fparse 0.25 * pi * D5^2}
A6 = ${fparse 0.25 * pi * D6^2}
A7 = ${fparse 0.25 * pi * D7^2}
A8 = ${fparse 0.25 * pi * D8^2}
recuperator_width = 0.15
L1 = 5.0
L2 = ${L1}
L3 = ${fparse 2 * L1}
L4 = ${fparse 2 * L1}
L5 = ${L1}
L6 = ${L1}
L7 = ${fparse L1 + recuperator_width}
L8 = ${L1}
x1 = 0.0
x2 = ${fparse x1 + L1}
x3 = ${fparse x2 + L2}
x4 = ${x3}
x5 = ${fparse x4 - L4}
x6 = ${x5}
x7 = ${fparse x6 + L6}
x8 = ${fparse x7 + L7}
y1 = 0
y2 = ${y1}
y3 = ${y2}
y4 = ${fparse y3 - L3}
y5 = ${y4}
y6 = ${fparse y5 + L5}
y7 = ${y6}
y8 = ${y7}
x1_out = ${fparse x1 + L1 - 0.001}
x2_in = ${fparse x2 + 0.001}
y5_in = ${fparse y5 + 0.001}
x6_out = ${fparse x6 + L6 - 0.001}
x7_in = ${fparse x7 + 0.001}
y8_in = ${fparse y8 + 0.001}
y8_out = ${fparse y8 + L8 - 0.001}
hot_leg_in = ${y8_in}
hot_leg_out = ${y8_out}
cold_leg_in = ${fparse y3 - 0.001}
cold_leg_out = ${fparse y3 - (L3/2) - 0.001}
n_elems1 = 5
n_elems2 = ${n_elems1}
n_elems3 = ${fparse 2 * n_elems1}
n_elems4 = ${fparse 2 * n_elems1}
n_elems5 = ${n_elems1}
n_elems6 = ${n_elems1}
n_elems7 = ${n_elems1}
n_elems8 = ${n_elems1}
A_ref_comp = ${fparse 0.5 * (A1 + A2)}
V_comp = ${fparse A_ref_comp * 1.0}
I_comp = 1.0
A_ref_turb = ${fparse 0.5 * (A4 + A5)}
V_turb = ${fparse A_ref_turb * 1.0}
I_turb = 1.0
c0_rated_comp = 351.6925137
rho0_rated_comp = 1.146881112
rated_mfr = 0.25
speed_rated_rpm = 96000
speed_rated = ${fparse speed_rated_rpm * 2 * pi / 60.0}
speed_initial = 0
eff_comp = 0.79
eff_turb = 0.843
T_ambient = 300
p_ambient = 1e5
hs_power = 105750
[GlobalParams]
gravity_vector = '0 0 0'
initial_p = ${p_ambient}
initial_T = ${T_ambient}
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
fp = fp_air
closures = closures
f = 0
scaling_factor_1phase = '1 1 1e-5'
scaling_factor_rhoV = 1
scaling_factor_rhouV = 1e-2
scaling_factor_rhovV = 1e-2
scaling_factor_rhowV = 1e-2
scaling_factor_rhoEV = 1e-5
scaling_factor_temperature = 1e-2
rdg_slope_reconstruction = none
[]
[FluidProperties]
[fp_air]
type = IdealGasFluidProperties
emit_on_nan = none
[]
[]
[HeatStructureMaterials]
[steel]
type = SolidMaterialProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Closures]
[closures]
type = Closures1PhaseSimple
[]
[]
[Functions]
##########################
# Motor
##########################
# Functions for control logic that determines when to shut off the PID system
[is_tripped_fn]
type = ParsedFunction
symbol_names = 'motor_torque turbine_torque'
symbol_values = 'motor_torque turbine_torque'
expression = 'turbine_torque > motor_torque'
[]
[PID_tripped_constant_value]
type = ConstantFunction
value = 1
[]
[PID_tripped_status_fn]
type = ParsedFunction
symbol_values = 'PID_trip_status'
symbol_names = 'PID_trip_status'
expression = 'PID_trip_status'
[]
[time_fn]
type = ParsedFunction
expression = t
[]
# Shutdown function which ramps down the motor once told by the control logic
[motor_torque_fn_shutdown]
type = ParsedFunction
symbol_values = 'PID_trip_status time_trip'
symbol_names = 'PID_trip_status time_trip'
expression = 'if(PID_trip_status = 1, max(2.4 - (2.4 * ((t - time_trip) / 35000)),0.0), 1)'
[]
# Generates motor power curve
[motor_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'motor_torque shaft:omega'
[]
##########################
# Generator
##########################
# Generates generator torque curve
[generator_torque_fn]
type = ParsedFunction
expression = 'slope * t'
symbol_names = 'slope'
symbol_values = '${generator_torque_per_shaft_speed}'
[]
# Generates generator power curve
[generator_power_fn]
type = ParsedFunction
expression = 'torque * speed'
symbol_names = 'torque speed'
symbol_values = 'generator_torque shaft:omega'
[]
##########################
# Reactor
##########################
# Ramps up reactor power when activated by control logic
[power_fn]
type = PiecewiseLinear
x = '0 1000 8600'
y = '0 0 ${hs_power}'
[]
##########################
# Compressor
##########################
# compressor pressure ratios
[rp_comp1]
type = PiecewiseLinear
data_file = 'rp_comp1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp2]
type = PiecewiseLinear
data_file = 'rp_comp2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp3]
type = PiecewiseLinear
data_file = 'rp_comp3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp4]
type = PiecewiseLinear
data_file = 'rp_comp4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_comp5]
type = PiecewiseLinear
data_file = 'rp_comp5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# compressor efficiencies
[eff_comp1]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp2]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp3]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp4]
type = ConstantFunction
value = ${eff_comp}
[]
[eff_comp5]
type = ConstantFunction
value = ${eff_comp}
[]
##########################
# Turbine
##########################
# turbine pressure ratios
[rp_turb0]
type = ConstantFunction
value = 1
[]
[rp_turb1]
type = PiecewiseLinear
data_file = 'rp_turb1.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb2]
type = PiecewiseLinear
data_file = 'rp_turb2.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb3]
type = PiecewiseLinear
data_file = 'rp_turb3.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb4]
type = PiecewiseLinear
data_file = 'rp_turb4.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
[rp_turb5]
type = PiecewiseLinear
data_file = 'rp_turb5.csv'
x_index_in_file = 0
y_index_in_file = 1
format = columns
extrap = true
[]
# turbine efficiency
[eff_turb1]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb2]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb3]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb4]
type = ConstantFunction
value = ${eff_turb}
[]
[eff_turb5]
type = ConstantFunction
value = ${eff_turb}
[]
[]
[Components]
# system inlet pulling air from the open atmosphere
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = ${p_ambient}
T0 = ${T_ambient}
[]
# Inlet pipe
[pipe1]
type = FlowChannel1Phase
position = '${x1} ${y1} 0'
orientation = '1 0 0'
length = ${L1}
n_elems = ${n_elems1}
A = ${A1}
[]
# Compressor as defined in MAGNET PCU document (Guillen 2020)
[compressor]
type = ShaftConnectedCompressor1Phase
position = '${x2} ${y2} 0'
inlet = 'pipe1:out'
outlet = 'pipe2:in'
A_ref = ${A_ref_comp}
volume = ${V_comp}
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
# Determines which compression ratio curve and efficiency curve to use depending on ratio of speed/rated_speed
speeds = '0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_comp1 rp_comp2 rp_comp3 rp_comp4 rp_comp5'
eff_functions = 'eff_comp1 eff_comp2 eff_comp3 eff_comp4 eff_comp5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_comp}
inertia_coeff = '${I_comp} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
# Outlet pipe from the compressor
[pipe2]
type = FlowChannel1Phase
position = '${x2} ${y2} 0'
orientation = '1 0 0'
length = ${L2}
n_elems = ${n_elems2}
A = ${A2}
[]
# 90 degree connection between pipe 2 and 3
[junction2_cold_leg]
type = VolumeJunction1Phase
connections = 'pipe2:out cold_leg:in'
position = '${x3} ${y3} 0'
volume = ${fparse A2*0.1}
[]
# Cold leg of the recuperator
[cold_leg]
type = FlowChannel1Phase
position = '${x3} ${y3} 0'
orientation = '0 -1 0'
length = ${fparse L3/2}
n_elems = ${fparse n_elems3/2}
A = ${A3}
[]
# Recuperator which transfers heat from exhaust gas to reactor inlet gas to improve thermal efficency
[recuperator]
type = HeatStructureCylindrical
orientation = '0 -1 0'
position = '${x3} ${y3} 0'
length = ${fparse L3/2}
widths = ${recuperator_width}
n_elems = ${fparse n_elems3/2}
n_part_elems = 2
names = recuperator
materials = steel
inner_radius = ${D1}
offset_mesh_by_inner_radius = true
[]
# heat transfer from recuperator to cold leg
[heat_transfer_cold_leg]
type = HeatTransferFromHeatStructure1Phase
flow_channel = cold_leg
hs = recuperator
hs_side = OUTER
Hw = 10000
[]
# heat transfer from hot leg to recuperator
[heat_transfer_hot_leg]
type = HeatTransferFromHeatStructure1Phase
flow_channel = hot_leg
hs = recuperator
hs_side = INNER
Hw = 10000
[]
[junction_cold_leg_3]
type = JunctionOneToOne1Phase
connections = 'cold_leg:out pipe3:in'
[]
[pipe3]
type = FlowChannel1Phase
position = '${x3} ${fparse y3 - (L3/2)} 0'
orientation = '0 -1 0'
length = ${fparse L3/2}
n_elems = ${fparse n_elems3/2}
A = ${A3}
[]
# 90 degree connection between pipe 3 and 4
[junction3_4]
type = VolumeJunction1Phase
connections = 'pipe3:out pipe4:in'
position = '${x4} ${y4} 0'
volume = ${fparse A3*0.1}
[]
# Pipe through the "reactor core"
[pipe4]
type = FlowChannel1Phase
position = '${x4} ${y4} 0'
orientation = '-1 0 0'
length = ${L4}
n_elems = ${n_elems4}
A = ${A4}
[]
# "Reactor Core" and it's associated heat transfer to pipe 4
[reactor]
type = HeatStructureCylindrical
orientation = '-1 0 0'
position = '${x4} ${y4} 0'
length = ${L4}
widths = 0.15
n_elems = ${n_elems4}
n_part_elems = 2
names = core
materials = steel
[]
[total_power]
type = TotalPower
power = 0
[]
[heat_generation]
type = HeatSourceFromTotalPower
power = total_power
hs = reactor
regions = core
[]
[heat_transfer]
type = HeatTransferFromHeatStructure1Phase
flow_channel = pipe4
hs = reactor
hs_side = OUTER
Hw = 10000
[]
# 90 degree connection between pipe 4 and 5
[junction4_5]
type = VolumeJunction1Phase
connections = 'pipe4:out pipe5:in'
position = '${x5} ${y5} 0'
volume = ${fparse A4*0.1}
[]
# Pipe carrying hot gas back to the PCU
[pipe5]
type = FlowChannel1Phase
position = '${x5} ${y5} 0'
orientation = '0 1 0'
length = ${L5}
n_elems = ${n_elems5}
A = ${A5}
[]
# 90 degree connection between pipe 5 and 6
[junction5_6]
type = VolumeJunction1Phase
connections = 'pipe5:out pipe6:in'
position = '${x6} ${y6} 0'
volume = ${fparse A5*0.1}
[]
# Inlet pipe to the turbine
[pipe6]
type = FlowChannel1Phase
position = '${x6} ${y6} 0'
orientation = '1 0 0'
length = ${L6}
n_elems = ${n_elems6}
A = ${A6}
[]
# Turbine as defined in MAGNET PCU document (Guillen 2020) and (Wright 2006)
[turbine]
type = ShaftConnectedCompressor1Phase
position = '${x7} ${y7} 0'
inlet = 'pipe6:out'
outlet = 'pipe7:in'
A_ref = ${A_ref_turb}
volume = ${V_turb}
# A turbine is treated as an "inverse" compressor, this value determines if component is to be treated as turbine or compressor
# If treat_as_turbine is omitted, code automatically assumes it is a compressor
treat_as_turbine = true
omega_rated = ${speed_rated}
mdot_rated = ${rated_mfr}
c0_rated = ${c0_rated_comp}
rho0_rated = ${rho0_rated_comp}
# Determines which compression ratio curve and efficiency curve to use depending on ratio of speed/rated_speed
speeds = '0 0.5208 0.6250 0.7292 0.8333 0.9375'
Rp_functions = 'rp_turb0 rp_turb1 rp_turb2 rp_turb3 rp_turb4 rp_turb5'
eff_functions = 'eff_turb1 eff_turb1 eff_turb2 eff_turb3 eff_turb4 eff_turb5'
min_pressure_ratio = 1.0
speed_cr_I = 0
inertia_const = ${I_turb}
inertia_coeff = '${I_turb} 0 0 0'
# assume no shaft friction
speed_cr_fr = 0
tau_fr_const = 0
tau_fr_coeff = '0 0 0 0'
[]
# Outlet pipe from turbine
[pipe7]
type = FlowChannel1Phase
position = '${x7} ${y7} 0'
orientation = '1 0 0'
length = ${L7}
n_elems = ${n_elems7}
A = ${A7}
[]
# 90 degree connection between pipe 7 and 8
[junction7_hot_leg]
type = VolumeJunction1Phase
connections = 'pipe7:out hot_leg:in'
position = '${x8} ${y8} 0'
volume = ${fparse A7*0.1}
[]
# Hot leg of the recuperator
[hot_leg]
type = FlowChannel1Phase
position = '${x8} ${y8} 0'
orientation = '0 1 0'
length = ${L8}
n_elems = ${n_elems8}
A = ${A8}
[]
# System outlet dumping exhaust gas to the atmosphere
[outlet]
type = Outlet1Phase
input = 'hot_leg:out'
p = ${p_ambient}
[]
# Roatating shaft connecting motor, compressor, turbine, and generator
[shaft]
type = Shaft
connected_components = 'motor compressor turbine generator'
initial_speed = ${speed_initial}
[]
# 3-Phase electircal motor used for system start-up, controlled by PID
[motor]
type = ShaftConnectedMotor
inertia = ${I_motor}
torque = 0 # controlled
[]
# Electric generator supplying power to the grid
[generator]
type = ShaftConnectedMotor
inertia = ${I_generator}
torque = generator_torque_fn
[]
[]
# Control logics which govern startup of the motor, startup of the "reactor core", and shutdown of the motor
[ControlLogic]
# Sets desired shaft speed to be reached by motor NOTE: SHOULD BE SET LOWER THAN RATED TURBINE RPM
[set_point]
type = GetFunctionValueControl
function = ${fparse speed_rated_rpm - 9000}
[]
# PID with gains determined by iterative process NOTE: Gain values are system specific
[initial_motor_PID]
type = PIDControl
set_point = set_point:value
input = shaft_RPM
initial_value = 0
K_p = 0.0011
K_i = 0.00000004
K_d = 0
[]
# Determines when the PID system should be running and when it should begin the shutdown cycle. If needed: PID output, else: shutdown function
[logic]
type = ParsedFunctionControl
function = 'if(motor+0.5 > turb, PID, shutdown_fn)'
symbol_names = 'motor turb PID shutdown_fn'
symbol_values = 'motor_torque turbine_torque initial_motor_PID:output motor_torque_fn_shutdown'
[]
# Takes the output generated in [logic] and applies it to the motor torque
[motor_PID]
type = SetComponentRealValueControl
component = motor
parameter = torque
value = logic:value
[]
# Determines when to turn on heat source
[power_logic]
type = ParsedFunctionControl
function = 'power_fn'
symbol_names = 'power_fn'
symbol_values = 'power_fn'
[]
# Applies heat source to the total_power block
[power_applied]
type = SetComponentRealValueControl
component = total_power
parameter = power
value = power_logic:value
[]
[]
[Controls]
# Enables set_PID_tripped
[PID_trip_status]
type = ConditionalFunctionEnableControl
conditional_function = is_tripped_fn
enable_objects = 'AuxScalarKernels::PID_trip_status_aux'
execute_on = 'TIMESTEP_END'
[]
# Enables set_time_PID
[time_PID]
type = ConditionalFunctionEnableControl
conditional_function = PID_tripped_status_fn
disable_objects = 'AuxScalarKernels::time_trip_aux'
execute_on = 'TIMESTEP_END'
[]
[]
[AuxVariables]
# Creates a variable that will later be set to the time when tau_turbine > tau_motor
[time_trip]
order = FIRST
family = SCALAR
[]
# Creates variable which indicates if tau_turbine > tau_motor....... If tau_motor > tau_turbine, 0, else 1
[PID_trip_status]
order = FIRST
family = SCALAR
initial_condition = 0
[]
[]
[AuxScalarKernels]
# Creates variable from time_fn which indicates when tau_turbine > tau_motor
[time_trip_aux]
type = FunctionScalarAux
function = time_fn
variable = time_trip
execute_on = 'TIMESTEP_END'
[]
# Overwrites variable PID_trip_status to the value from PID_tripped_constant_value (changes 0 to 1)
[PID_trip_status_aux]
type = FunctionScalarAux
function = PID_tripped_constant_value
variable = PID_trip_status
execute_on = 'TIMESTEP_END'
enable = false
[]
[]
[Postprocessors]
# Indicates when tau_turbine > tau_motor
[trip_time]
type = ScalarVariable
variable = time_trip
execute_on = 'TIMESTEP_END'
[]
##########################
# Motor
##########################
[motor_torque]
type = RealComponentParameterValuePostprocessor
component = motor
parameter = torque
execute_on = 'INITIAL TIMESTEP_END'
[]
[motor_power]
type = FunctionValuePostprocessor
function = motor_power_fn
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# generator
##########################
[generator_torque]
type = ShaftConnectedComponentPostprocessor
quantity = torque
shaft_connected_component_uo = generator:shaftconnected_uo
execute_on = 'INITIAL TIMESTEP_END'
[]
[generator_power]
type = FunctionValuePostprocessor
function = generator_power_fn
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# Shaft
##########################
# Speed in rad/s
[shaft_speed]
type = ScalarVariable
variable = 'shaft:omega'
execute_on = 'INITIAL TIMESTEP_END'
[]
# speed in RPM
[shaft_RPM]
type = ParsedPostprocessor
pp_names = 'shaft_speed'
function = '(shaft_speed * 60) /( 2 * ${fparse pi})'
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# Compressor
##########################
[comp_dissipation_torque]
type = ScalarVariable
variable = 'compressor:dissipation_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[comp_isentropic_torque]
type = ScalarVariable
variable = 'compressor:isentropic_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[comp_friction_torque]
type = ScalarVariable
variable = 'compressor:friction_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[compressor_torque]
type = ParsedPostprocessor
pp_names = 'comp_dissipation_torque comp_isentropic_torque comp_friction_torque'
function = 'comp_dissipation_torque + comp_isentropic_torque + comp_friction_torque'
[]
[p_in_comp]
type = PointValue
variable = p
point = '${x1_out} ${y1} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_comp]
type = PointValue
variable = p
point = '${x2_in} ${y2} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_comp]
type = ParsedPostprocessor
pp_names = 'p_in_comp p_out_comp'
function = 'p_out_comp / p_in_comp'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_in_comp]
type = PointValue
variable = T
point = '${x1_out} ${y1} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_out_comp]
type = PointValue
variable = T
point = '${x2_in} ${y2} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_ratio_comp]
type = ParsedPostprocessor
pp_names = 'T_in_comp T_out_comp'
function = '(T_out_comp - T_in_comp) / T_out_comp'
execute_on = 'INITIAL TIMESTEP_END'
[]
[mfr_comp]
type = ADFlowJunctionFlux1Phase
boundary = pipe1:out
connection_index = 0
equation = mass
junction = compressor
[]
##########################
# turbine
##########################
[turb_dissipation_torque]
type = ScalarVariable
variable = 'turbine:dissipation_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[turb_isentropic_torque]
type = ScalarVariable
variable = 'turbine:isentropic_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[turb_friction_torque]
type = ScalarVariable
variable = 'turbine:friction_torque'
execute_on = 'INITIAL TIMESTEP_END'
[]
[turbine_torque]
type = ParsedPostprocessor
pp_names = 'turb_dissipation_torque turb_isentropic_torque turb_friction_torque'
function = 'turb_dissipation_torque + turb_isentropic_torque + turb_friction_torque'
[]
[p_in_turb]
type = PointValue
variable = p
point = '${x6_out} ${y6} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_out_turb]
type = PointValue
variable = p
point = '${x7_in} ${y7} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[p_ratio_turb]
type = ParsedPostprocessor
pp_names = 'p_in_turb p_out_turb'
function = 'p_in_turb / p_out_turb'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_in_turb]
type = PointValue
variable = T
point = '${x6_out} ${y6} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[T_out_turb]
type = PointValue
variable = T
point = '${x7_in} ${y7} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[mfr_turb]
type = ADFlowJunctionFlux1Phase
boundary = pipe6:out
connection_index = 0
equation = mass
junction = turbine
[]
##########################
# Recuperator
##########################
[cold_leg_in]
type = PointValue
variable = T
point = '${x3} ${cold_leg_in} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[cold_leg_out]
type = PointValue
variable = T
point = '${x3} ${cold_leg_out} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[hot_leg_in]
type = PointValue
variable = T
point = '${x8} ${hot_leg_in} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[hot_leg_out]
type = PointValue
variable = T
point = '${x8} ${hot_leg_out} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
##########################
# Reactor
##########################
[reactor_inlet]
type = PointValue
variable = T
point = '${x4} ${y4} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[reactor_outlet]
type = PointValue
variable = T
point = '${x5} ${y5_in} 0'
execute_on = 'INITIAL TIMESTEP_END'
[]
[]
[Executioner]
type = Transient
scheme = 'bdf2'
end_time = ${t3}
[TimeStepper]
type = IterationAdaptiveDT
dt = 0.01
growth_factor = 1.1
cutback_factor = 0.9
[]
dtmin = 1e-5
dtmax = 1000
steady_state_detection = true
steady_state_start_time = 200000
solve_type = NEWTON
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
nl_max_its = 15
l_tol = 1e-4
l_max_its = 10
petsc_options_iname = '-pc_type'
petsc_options_value = ' lu '
[]
[Outputs]
[e]
type = Exodus
file_base = 'recuperated_brayton_cycle_out'
[]
[csv]
type = CSV
file_base = 'recuperated_brayton_cycle'
execute_vector_postprocessors_on = 'INITIAL'
[]
[console]
type = Console
show = 'shaft_speed p_ratio_comp p_ratio_turb compressor:pressure_ratio turbine:pressure_ratio'
[]
[]
(modules/thermal_hydraulics/tutorials/single_phase_flow/05_secondary_side.i)
T_in = 300. # K
m_dot_in = 1e-4 # kg/s
press = 1e5 # Pa
# core parameters
core_length = 1. # m
core_n_elems = 10
core_dia = ${units 2. cm -> m}
core_pitch = ${units 8.7 cm -> m}
# pipe parameters
pipe_dia = ${units 10. cm -> m}
tot_power = 100 # W
# heat exchanger parameters
hx_dia_inner = ${units 10. cm -> m}
hx_wall_thickness = ${units 5. mm -> m}
hx_dia_outer = ${units 50. cm -> m}
hx_radius_wall = ${fparse hx_dia_inner / 2. + hx_wall_thickness}
hx_length = 1 # m
hx_n_elems = 10
m_dot_sec_in = 1 # kg/s
[GlobalParams]
initial_p = ${press}
initial_vel = 0
initial_T = ${T_in}
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
rdg_slope_reconstruction = full
closures = simple_closures
fp = he
f = 0.4
[]
[Functions]
[m_dot_sec_fn]
type = PiecewiseLinear
xy_data = '
0 0
100 ${m_dot_sec_in}'
[]
[]
[FluidProperties]
[he]
type = IdealGasFluidProperties
molar_mass = 4e-3
gamma = 1.67
k = 0.2556
mu = 3.22639e-5
[]
[water]
type = StiffenedGasFluidProperties
gamma = 2.35
cv = 1816.0
q = -1.167e6
p_inf = 1.0e9
q_prime = 0
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[HeatStructureMaterials]
[steel]
type = SolidMaterialProperties
rho = 8050
k = 45
cp = 466
[]
[]
[Components]
[total_power]
type = TotalPower
power = ${tot_power}
[]
[core_chan]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
A = ${fparse core_pitch * core_pitch - pi * core_dia * core_dia / 4.}
D_h = ${core_dia}
f = 1.6
[]
[core_hs]
type = HeatStructureCylindrical
position = '0 0 0'
orientation = '0 0 1'
length = ${core_length}
n_elems = ${core_n_elems}
names = 'block'
widths = '${fparse core_dia / 2.}'
materials = 'steel'
n_part_elems = 3
[]
[core_heating]
type = HeatSourceFromTotalPower
hs = core_hs
regions = block
power = total_power
[]
[core_ht]
type = HeatTransferFromHeatStructure1Phase
flow_channel = core_chan
hs = core_hs
hs_side = outer
P_hf = ${fparse pi * core_dia}
Hw = 1.36
[]
[jct1]
type = JunctionParallelChannels1Phase
position = '0 0 1'
connections = 'core_chan:out up_pipe:in'
volume = 1e-3
[]
[up_pipe]
type = FlowChannel1Phase
position = '0 0 1'
orientation = '0 0 1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct2]
type = VolumeJunction1Phase
position = '0 0 2'
connections = 'up_pipe:out top_pipe:in'
volume = 1e-3
[]
[top_pipe]
type = FlowChannel1Phase
position = '0 0 2'
orientation = '1 0 0'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct3]
type = VolumeJunction1Phase
position = '1 0 2'
connections = 'top_pipe:out hx/pri:in'
volume = 1e-3
[]
[hx]
[pri]
type = FlowChannel1Phase
position = '1 0 2'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
A = ${fparse pi * hx_dia_inner * hx_dia_inner / 4.}
D_h = ${hx_dia_inner}
[]
[ht_pri]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = inner
flow_channel = hx/pri
Hw = 0.97
[]
[wall]
type = HeatStructureCylindrical
position = '1 0 2'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
widths = '${hx_wall_thickness}'
n_part_elems = '3'
materials = 'steel'
names = '0'
inner_radius = ${fparse hx_dia_inner / 2.}
offset_mesh_by_inner_radius = true
[]
[ht_sec]
type = HeatTransferFromHeatStructure1Phase
hs = hx/wall
hs_side = outer
flow_channel = hx/sec
P_hf = ${fparse 2 * pi * hx_radius_wall}
Hw = 36
[]
[sec]
type = FlowChannel1Phase
position = '${fparse 1 + hx_wall_thickness} 0 2'
orientation = '0 0 -1'
length = ${hx_length}
n_elems = ${hx_n_elems}
A = ${fparse pi * (hx_dia_outer * hx_dia_outer / 4. - hx_radius_wall * hx_radius_wall)}
D_h = ${fparse hx_dia_outer - (2 * hx_radius_wall)}
fp = water
f = 0.075
[]
[]
[jct4]
type = VolumeJunction1Phase
position = '1 0 1'
connections = 'hx/pri:out down_pipe:in'
volume = 1e-3
[]
[down_pipe]
type = FlowChannel1Phase
position = '1 0 1'
orientation = '0 0 -1'
length = 1
n_elems = 10
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct5]
type = VolumeJunction1Phase
position = '1 0 0'
connections = 'down_pipe:out bottom_b:in'
volume = 1e-3
[]
[bottom_b]
type = FlowChannel1Phase
position = '1 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[pump]
type = Pump1Phase
position = '0.5 0 0'
connections = 'bottom_b:out bottom_a:in'
volume = 1e-3
A_ref = ${fparse pi * pipe_dia * pipe_dia / 4.}
head = 0
[]
[bottom_a]
type = FlowChannel1Phase
position = '0.5 0 0'
orientation = '-1 0 0'
length = 0.5
n_elems = 5
A = ${fparse pi * pipe_dia * pipe_dia / 4.}
D_h = ${pipe_dia}
[]
[jct6]
type = VolumeJunction1Phase
position = '0 0 0'
connections = 'bottom_a:out core_chan:in'
volume = 1e-3
[]
[inlet_sec]
type = InletMassFlowRateTemperature1Phase
input = 'hx/sec:out'
m_dot = 0
T = 300
[]
[outlet_sec]
type = Outlet1Phase
input = 'hx/sec:in'
p = ${press}
[]
[]
[ControlLogic]
[set_point]
type = GetFunctionValueControl
function = ${m_dot_in}
[]
[pid]
type = PIDControl
initial_value = 0
set_point = set_point:value
input = m_dot_pump
K_p = 250
K_i = 0.5
K_d = 0
[]
[set_pump_head]
type = SetComponentRealValueControl
component = pump
parameter = head
value = pid:output
[]
[m_dot_sec_inlet_ctrl]
type = GetFunctionValueControl
function = m_dot_sec_fn
[]
[set_m_dot_sec_ctrl]
type = SetComponentRealValueControl
component = inlet_sec
parameter = m_dot
value = m_dot_sec_inlet_ctrl:value
[]
[]
[Postprocessors]
[m_dot_pump]
type = ADFlowJunctionFlux1Phase
boundary = core_chan:in
connection_index = 1
equation = mass
junction = jct6
[]
[core_T_out]
type = SideAverageValue
boundary = core_chan:out
variable = T
[]
[hx_pri_T_out]
type = SideAverageValue
boundary = hx/pri:out
variable = T
[]
[hx_sec_T_in]
type = SideAverageValue
boundary = inlet_sec
variable = T
[]
[hx_sec_T_out]
type = SideAverageValue
boundary = outlet_sec
variable = T
[]
[]
[Executioner]
type = Transient
start_time = 0
[TimeStepper]
type = SolutionTimeAdaptiveDT
dt = 1
[]
dtmax = 100
end_time = 50000
line_search = basic
solve_type = NEWTON
nl_rel_tol = 1e-5
nl_abs_tol = 1e-5
nl_max_its = 5
[]
[Outputs]
exodus = true
[console]
type = Console
max_rows = 1
outlier_variable_norms = false
[]
print_linear_residuals = false
[]
(modules/thermal_hydraulics/test/tests/controls/error_checking/non_existent_control_data.i)
# This test makes sure that we error out when a control object requests a data
# that were not declared
[GlobalParams]
initial_p = 100.e3
initial_vel = 1.0
initial_T = 350.
scaling_factor_1phase = '1 1e-2 1e-4'
closures = simple_closures
[]
[FluidProperties]
[fp]
type = StiffenedGasFluidProperties
gamma = 2.35
q = -1167e3
q_prime = 0
p_inf = 1.e9
cv = 1816
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[pipe1]
type = FlowChannel1Phase
fp = fp
position = '0 0 0'
orientation = '1 0 0'
length = 15.0
n_elems = 10
A = 0.01
D_h = 0.1
f = 0.01
[]
[inlet]
type = InletStagnationPressureTemperature1Phase
input = 'pipe1:in'
p0 = 105.e3
T0 = 300.
[]
[outlet]
type = Outlet1Phase
input = 'pipe1:out'
p = 100.0e3
[]
[]
[ControlLogic]
[set_inlet_value]
type = SetComponentRealValueControl
component = inlet
parameter = T0
value = wrong # this does not exist
[]
[]
[Preconditioning]
[SMP_PJFNK]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
start_time = 0
dt = 0.5
num_steps = 1
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-6
nl_max_its = 20
l_tol = 1e-3
l_max_its = 5
[]
(modules/thermal_hydraulics/test/tests/components/shaft_connected_turbine_1phase/turbine_startup.i)
# This test tests that the turbine can startup from rest and reach full power.
# The mass flow rate for the inlet component is ramped up over 10s. The dyno
# component and pid_ctrl controler are used to maintain the turbine's rated shaft
# speed. The turbine should supply ~1e6 W of power to the shaft by the end of the test.
omega_rated = 450
mdot = 5.0
T_in = 1000.0
p_out = 1e6
[GlobalParams]
f = 1
scaling_factor_1phase = '0.04 0.04 0.04e-5'
closures = simple_closures
n_elems = 20
initial_T = ${T_in}
initial_p = ${p_out}
initial_vel = 0
initial_vel_x = 0
initial_vel_y = 0
initial_vel_z = 0
[]
[FluidProperties]
[eos]
type = IdealGasFluidProperties
[]
[]
[Closures]
[simple_closures]
type = Closures1PhaseSimple
[]
[]
[Components]
[ch_in]
type = FlowChannel1Phase
position = '-1 0 0'
orientation = '1 0 0'
length = 1
A = 0.1
D_h = 1
fp = eos
[]
[inlet]
type = InletMassFlowRateTemperature1Phase
input = 'ch_in:in'
m_dot = 0
T = ${T_in}
[]
[turbine]
type = ShaftConnectedTurbine1Phase
inlet = 'ch_in:out'
outlet = 'ch_out:in'
position = '0 0 0'
scaling_factor_rhoEV = 1e-5
A_ref = 0.1
volume = 0.0002
inertia_coeff = '1 1 1 1'
inertia_const = 1.61397
speed_cr_I = 1e12
speed_cr_fr = 0
tau_fr_coeff = '0 0 0 0'
tau_fr_const = 0
omega_rated = ${omega_rated}
D_wheel = 0.4
head_coefficient = head
power_coefficient = power
[]
[ch_out]
type = FlowChannel1Phase
position = '0 0 0'
orientation = '1 0 0'
length = 1
A = 0.1
D_h = 1
fp = eos
[]
[outlet]
type = Outlet1Phase
input = 'ch_out:out'
p = ${p_out}
[]
[dyno]
type = ShaftConnectedMotor
inertia = 10
torque = -450
[]
[shaft]
type = Shaft
connected_components = 'turbine dyno'
initial_speed = ${omega_rated}
[]
[]
[Functions]
[head]
type = PiecewiseLinear
x = '0 7e-3 1e-2'
y = '0 15 20'
[]
[power]
type = PiecewiseLinear
x = '0 6e-3 1e-2'
y = '0 0.05 0.18'
[]
[mfr_fn]
type = PiecewiseLinear
x = '0 10'
y = '1e-6 ${mdot}'
[]
[dts]
type = PiecewiseConstant
y = '5e-3 1e-2 5e-2 5e-1'
x = '0 0.5 1 10'
[]
[]
[ControlLogic]
[mfr_cntrl]
type = TimeFunctionComponentControl
component = inlet
parameter = m_dot
function = mfr_fn
[]
[speed_set_point]
type = GetFunctionValueControl
function = ${omega_rated}
[]
[pid_ctrl]
type = PIDControl
input = omega
set_point = speed_set_point:value
K_i = 2
K_p = 5
K_d = 5
initial_value = -450
[]
[set_torque_value]
type = SetComponentRealValueControl
component = dyno
parameter = torque
value = pid_ctrl:output
[]
[]
[Postprocessors]
[omega]
type = ScalarVariable
variable = shaft:omega
execute_on = 'initial timestep_end'
[]
[flow_coefficient]
type = ScalarVariable
variable = turbine:flow_coeff
execute_on = 'initial timestep_end'
[]
[delta_p]
type = ScalarVariable
variable = turbine:delta_p
execute_on = 'initial timestep_end'
[]
[power]
type = ScalarVariable
variable = turbine:power
execute_on = 'initial timestep_end'
[]
[]
[Preconditioning]
[SMP]
type = SMP
full = true
[]
[]
[Executioner]
type = Transient
scheme = 'implicit-euler'
start_time = 0
[TimeStepper]
type = FunctionDT
function = dts
[]
end_time = 20
abort_on_solve_fail = true
solve_type = 'PJFNK'
line_search = 'basic'
nl_rel_tol = 1e-6
nl_abs_tol = 1e-4
nl_max_its = 30
l_tol = 1e-4
l_max_its = 20
[Quadrature]
type = GAUSS
order = SECOND
[]
[]
[Outputs]
[console]
type = Console
max_rows = 1
[]
print_linear_residuals = false
[]