实现test_mql PNL0003与PNL00R管路

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huojiarong committed 2026-07-17 08:54:38 +00:00
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@@ -8,7 +8,7 @@ from PythonModels.components.amesim_pneumatic import (
AmesimPneumaticGas,
diameter_mm_to_area_m2,
)
from PythonModels.core.base import DynamicComponent
from PythonModels.core.base import AlgebraicComponent, DynamicComponent
from PythonModels.core.medium import ThermodynamicProperties
from PythonModels.core.ports import PortState
from PythonModels.core.state import VolumeState
@@ -23,7 +23,89 @@ class AmesimPnl0001Diagnostics:
pressure_drop_pa: float
class AmesimPnl0001Pipe(DynamicComponent):
class _DarcyPipeResistanceMixin:
diameter: float
length: float
relative_roughness: float
area: float
def _mass_flow_for_pressure_drop(
self,
pressure_drop_pa: float,
*,
density: float,
temperature: float,
) -> float:
if pressure_drop_pa <= 0.0:
return 0.0
upper = 1.0e-9
while self._darcy_pressure_drop(
upper,
density=density,
temperature=temperature,
) < pressure_drop_pa:
upper *= 10.0
if upper > 1.0e3:
raise ValueError("unable to bracket pneumatic pipe resistance flow")
lower = 0.0
for _ in range(80):
middle = 0.5 * (lower + upper)
if self._darcy_pressure_drop(
middle,
density=density,
temperature=temperature,
) < pressure_drop_pa:
lower = middle
else:
upper = middle
return 0.5 * (lower + upper)
def _darcy_pressure_drop(
self,
mass_flow_kg_s: float,
*,
density: float,
temperature: float,
) -> float:
if mass_flow_kg_s == 0.0:
return 0.0
reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (density * self.area)
magnitude = (
friction_factor
* (self.length / self.diameter)
* density
* velocity
* velocity
/ 2.0
)
return magnitude if mass_flow_kg_s > 0.0 else -magnitude
def _reynolds_number(self, mass_flow_kg_s: float, temperature: float) -> float:
viscosity = helium_dynamic_viscosity(temperature)
return 4.0 * abs(mass_flow_kg_s) / (pi * self.diameter * viscosity)
def _friction_factor(self, reynolds_number: float) -> float:
if reynolds_number <= 0.0:
return 64_000_000.0
laminar = 64.0 / reynolds_number
if reynolds_number <= 2_300.0:
return laminar
turbulent = 1.0 / (
-1.8
* log10(
(self.relative_roughness / 3.7) ** 1.11
+ 6.9 / reynolds_number
)
) ** 2
if reynolds_number >= 4_000.0:
return turbulent
fraction = (reynolds_number - 2_300.0) / 1_700.0
return laminar + fraction * (turbulent - laminar)
class AmesimPnl0001Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
"""Physical first-pass implementation of AMESim ``PNL0001`` (C-R).
Port 2 owns the lumped gas storage. Port 1 is connected through a Darcy
@@ -193,80 +275,289 @@ class AmesimPnl0001Pipe(DynamicComponent):
U=port_1_m_flow * inlet_h_1 + port_2_m_flow * inlet_h_2 + heat_flow,
)
def _mass_flow_for_pressure_drop(
self,
pressure_drop_pa: float,
*,
density: float,
temperature: float,
) -> float:
if pressure_drop_pa <= 0.0:
return 0.0
upper = 1.0e-9
while self._darcy_pressure_drop(
upper,
density=density,
temperature=temperature,
) < pressure_drop_pa:
upper *= 10.0
if upper > 1.0e3:
raise ValueError("unable to bracket PNL0001 resistance flow")
lower = 0.0
for _ in range(80):
middle = 0.5 * (lower + upper)
if self._darcy_pressure_drop(
middle,
density=density,
temperature=temperature,
) < pressure_drop_pa:
lower = middle
else:
upper = middle
return 0.5 * (lower + upper)
def _darcy_pressure_drop(
class AmesimPnl0003Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
"""First-pass AMESim ``PNL0003`` (C-R-C) pipe.
The two pipe-end compliances are represented as equal half-volume gas
stores connected by the same auditable Darcy resistance used for PNL0001.
Center flow is positive from port 1 storage to port 2 storage.
"""
state_size = 4
def __init__(
self,
mass_flow_kg_s: float,
name: str,
*,
density: float,
temperature: float,
) -> float:
if mass_flow_kg_s == 0.0:
diameter_mm: float,
length_m: float,
relative_roughness: float,
polytropic_constant: float = 1.35,
heat_transfer_coefficient: float = 0.0,
external_temperature_k: float = 293.15,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
p1_0: float = 101_325.0,
T1_0: float = 293.15,
p2_0: float = 101_325.0,
T2_0: float = 293.15,
) -> None:
if diameter_mm <= 0.0:
raise ValueError("diameter_mm must be positive")
if length_m <= 0.0:
raise ValueError("length_m must be positive")
if relative_roughness < 0.0:
raise ValueError("relative_roughness must be non-negative")
if polytropic_constant <= 0.0:
raise ValueError("polytropic_constant must be positive")
if heat_transfer_coefficient < 0.0:
raise ValueError("heat_transfer_coefficient must be non-negative")
if external_temperature_k <= 0.0:
raise ValueError("external_temperature_k must be positive")
super().__init__(name=name)
self.diameter = diameter_mm * 1.0e-3
self.length = length_m
self.relative_roughness = relative_roughness
self.polytropic_constant = polytropic_constant
self.heat_transfer_coefficient = heat_transfer_coefficient
self.external_temperature = external_temperature_k
self.gas = gas
self.area = diameter_mm_to_area_m2(diameter_mm)
self.volume = self.area * self.length
self.compliance_volume = self.volume / 2.0
self.heat_transfer_area = pi * self.diameter * self.length
self.state_1 = self._initial_state(p1_0, T1_0)
self.state_2 = self._initial_state(p2_0, T2_0)
self.port_1 = PortState()
self.port_2 = PortState()
def _initial_state(self, pressure: float, temperature: float) -> VolumeState:
rho = self.gas.density(pressure, temperature)
mass = rho * self.compliance_volume
return VolumeState(
m=mass,
U=mass * self.gas.specific_internal_energy(temperature),
)
def get_state_vector(self) -> list[float]:
return [*self.state_1.as_vector(), *self.state_2.as_vector()]
def set_state_vector(self, values: list[float]) -> None:
if len(values) != 4:
raise ValueError("PNL0003 state vector requires four values")
self.state_1 = VolumeState.from_vector(values[:2])
self.state_2 = VolumeState.from_vector(values[2:])
def properties_1(self) -> ThermodynamicProperties:
properties = self._properties(self.state_1)
self.port_1.p = properties.p
self.port_1.h_outflow = properties.h
return properties
def properties_2(self) -> ThermodynamicProperties:
properties = self._properties(self.state_2)
self.port_2.p = properties.p
self.port_2.h_outflow = properties.h
return properties
def _properties(self, state: VolumeState) -> ThermodynamicProperties:
if state.m <= 0.0:
raise ValueError("pipe mass must stay positive")
temperature = self.gas.temperature_from_internal_energy(state.U / state.m)
density = state.m / self.compliance_volume
pressure = self.gas.pressure(density, temperature)
return ThermodynamicProperties(
p=pressure,
T=temperature,
rho=density,
u=state.U / state.m,
h=self.gas.specific_enthalpy(temperature),
)
def gas_mass_g(self) -> float:
return (self.state_1.m + self.state_2.m) * 1.0e3
def resistance_mass_flow(self) -> float:
"""Return center mass flow from port 1 storage to port 2 storage."""
port_1 = self.properties_1()
port_2 = self.properties_2()
pressure_difference = port_1.p - port_2.p
if pressure_difference == 0.0:
return 0.0
upstream = port_1 if pressure_difference > 0.0 else port_2
magnitude = self._mass_flow_for_pressure_drop(
abs(pressure_difference),
density=upstream.rho,
temperature=upstream.T,
)
return magnitude if pressure_difference > 0.0 else -magnitude
def diagnostics(
self,
*,
mass_flow_kg_s: float,
temperature_k: float | None = None,
) -> AmesimPnl0001Diagnostics:
port_1 = self.properties_1()
port_2 = self.properties_2()
temperature = temperature_k or (port_1.T if mass_flow_kg_s >= 0.0 else port_2.T)
density = port_1.rho if mass_flow_kg_s >= 0.0 else port_2.rho
reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (density * self.area)
magnitude = (
friction_factor
* (self.length / self.diameter)
* density
* velocity
* velocity
pressure_drop = self._darcy_pressure_drop(
mass_flow_kg_s,
density=density,
temperature=temperature,
)
return AmesimPnl0001Diagnostics(
mass_flow_kg_s=mass_flow_kg_s,
reynolds_number=reynolds,
gas_velocity_m_s=velocity,
friction_factor=friction_factor,
pressure_drop_pa=pressure_drop,
)
def derivatives_from_connections(
self,
*,
port_1_m_flow: float,
connected_h_1: float,
port_2_m_flow: float,
connected_h_2: float,
) -> tuple[VolumeState, VolumeState]:
port_1 = self.properties_1()
port_2 = self.properties_2()
center_flow = self.resistance_mass_flow()
heat_flow_each = (
self.heat_transfer_coefficient
* self.heat_transfer_area
* (self.external_temperature - 0.5 * (port_1.T + port_2.T))
/ 2.0
)
return magnitude if mass_flow_kg_s > 0.0 else -magnitude
port_1_external_h = self.connection_inlet_enthalpy(
port_m_flow=port_1_m_flow,
connected_h=connected_h_1,
internal_h=port_1.h,
)
port_2_external_h = self.connection_inlet_enthalpy(
port_m_flow=port_2_m_flow,
connected_h=connected_h_2,
internal_h=port_2.h,
)
port_1_center_h = self.connection_inlet_enthalpy(
port_m_flow=-center_flow,
connected_h=port_2.h,
internal_h=port_1.h,
)
port_2_center_h = self.connection_inlet_enthalpy(
port_m_flow=center_flow,
connected_h=port_1.h,
internal_h=port_2.h,
)
return (
VolumeState(
m=port_1_m_flow - center_flow,
U=(
port_1_m_flow * port_1_external_h
- center_flow * port_1_center_h
+ heat_flow_each
),
),
VolumeState(
m=port_2_m_flow + center_flow,
U=(
port_2_m_flow * port_2_external_h
+ center_flow * port_2_center_h
+ heat_flow_each
),
),
)
def _reynolds_number(self, mass_flow_kg_s: float, temperature: float) -> float:
viscosity = helium_dynamic_viscosity(temperature)
return 4.0 * abs(mass_flow_kg_s) / (pi * self.diameter * viscosity)
def _friction_factor(self, reynolds_number: float) -> float:
if reynolds_number <= 0.0:
return 64_000_000.0
laminar = 64.0 / reynolds_number
if reynolds_number <= 2_300.0:
return laminar
turbulent = 1.0 / (
-1.8
* log10(
(self.relative_roughness / 3.7) ** 1.11
+ 6.9 / reynolds_number
)
) ** 2
if reynolds_number >= 4_000.0:
return turbulent
fraction = (reynolds_number - 2_300.0) / 1_700.0
return laminar + fraction * (turbulent - laminar)
class AmesimPnl00rPipe(_DarcyPipeResistanceMixin, AlgebraicComponent):
"""First-pass AMESim ``PNL00R`` (R) pipe resistance."""
def __init__(
self,
name: str,
*,
diameter_mm: float,
length_m: float,
relative_roughness: float,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> None:
if diameter_mm <= 0.0:
raise ValueError("diameter_mm must be positive")
if length_m <= 0.0:
raise ValueError("length_m must be positive")
if relative_roughness < 0.0:
raise ValueError("relative_roughness must be non-negative")
super().__init__(name=name)
self.diameter = diameter_mm * 1.0e-3
self.length = length_m
self.relative_roughness = relative_roughness
self.gas = gas
self.area = diameter_mm_to_area_m2(diameter_mm)
self.port_1 = PortState()
self.port_2 = PortState()
def mass_flow(
self,
*,
port_1_pressure_pa: float,
port_1_temperature_k: float,
port_2_pressure_pa: float,
port_2_temperature_k: float,
) -> float:
"""Return mass flow from port 1 to port 2 in kg/s."""
if port_1_pressure_pa <= 0.0 or port_2_pressure_pa <= 0.0:
raise ValueError("port pressures must be positive")
if port_1_temperature_k <= 0.0 or port_2_temperature_k <= 0.0:
raise ValueError("port temperatures must be positive")
pressure_difference = port_1_pressure_pa - port_2_pressure_pa
if pressure_difference == 0.0:
return 0.0
upstream_pressure = max(port_1_pressure_pa, port_2_pressure_pa)
upstream_temperature = (
port_1_temperature_k
if pressure_difference > 0.0
else port_2_temperature_k
)
density = self.gas.density(upstream_pressure, upstream_temperature)
magnitude = self._mass_flow_for_pressure_drop(
abs(pressure_difference),
density=density,
temperature=upstream_temperature,
)
return magnitude if pressure_difference > 0.0 else -magnitude
def diagnostics(
self,
*,
mass_flow_kg_s: float,
pressure_pa: float,
temperature_k: float,
) -> AmesimPnl0001Diagnostics:
density = self.gas.density(pressure_pa, temperature_k)
reynolds = self._reynolds_number(mass_flow_kg_s, temperature_k)
friction_factor = self._friction_factor(reynolds)
velocity = mass_flow_kg_s / (density * self.area)
pressure_drop = self._darcy_pressure_drop(
mass_flow_kg_s,
density=density,
temperature=temperature_k,
)
return AmesimPnl0001Diagnostics(
mass_flow_kg_s=mass_flow_kg_s,
reynolds_number=reynolds,
gas_velocity_m_s=velocity,
friction_factor=friction_factor,
pressure_drop_pa=pressure_drop,
)
def helium_dynamic_viscosity(temperature_k: float) -> float:
+24
View File
@@ -3860,6 +3860,8 @@ class TestMqlSystem:
self.archive_path = archive_path or Path(__file__).resolve().parents[2] / AMESIM_ARCHIVE_RELATIVE_PATH
self.network = SimulationNetwork(name=MODEL_NAME)
self.pnl0001_assembly = self._build_pnl0001_assembly()
self.pnl0003_assembly = self._build_pnl0003_assembly()
self.pnl00r_assembly = self._build_pnl00r_assembly()
self.node3_assembly = self._build_node3_assembly()
self.pneumatic_assembly = self._build_pneumatic_assembly()
pneumatic_components = self._pneumatic_components_by_alias()
@@ -3890,6 +3892,20 @@ class TestMqlSystem:
return build_test_mql_pnl0001_assembly(self.archive_path)
def _build_pnl0003_assembly(self):
from PythonModels.systems.test_mql_pneumatic_lines import (
build_test_mql_pnl0003_assembly,
)
return build_test_mql_pnl0003_assembly(self.archive_path)
def _build_pnl00r_assembly(self):
from PythonModels.systems.test_mql_pneumatic_lines import (
build_test_mql_pnl00r_assembly,
)
return build_test_mql_pnl00r_assembly(self.archive_path)
@staticmethod
def _build_node3_assembly():
from PythonModels.systems.test_mql_nodes import build_test_mql_node3_assembly
@@ -3912,6 +3928,14 @@ class TestMqlSystem:
def typed_pnl0001_line_count(self) -> int:
return len(self.pnl0001_assembly.lines)
@property
def typed_pnl0003_line_count(self) -> int:
return len(self.pnl0003_assembly.lines)
@property
def typed_pnl00r_line_count(self) -> int:
return len(self.pnl00r_assembly.lines)
@property
def typed_node3_count(self) -> int:
return len(self.node3_assembly)
@@ -35,6 +35,48 @@ class TestMqlPnl0001Spec:
return self.initial_gauge_pressure_pa + AMESIM_REFERENCE_PRESSURE_PA
@dataclass(frozen=True)
class TestMqlPnl0003Spec:
alias: str
source_component: str
source_port: str
target_component: str
target_port: str
diameter_mm: float
length_m: float
relative_roughness: float
polytropic_constant: float
heat_transfer_coefficient: float
external_temperature_k: float
gas_type_index: int
mode: int
initial_temperature_1_k: float
initial_gauge_pressure_1_pa: float
initial_temperature_2_k: float
initial_gauge_pressure_2_pa: float
@property
def initial_absolute_pressure_1_pa(self) -> float:
return self.initial_gauge_pressure_1_pa + AMESIM_REFERENCE_PRESSURE_PA
@property
def initial_absolute_pressure_2_pa(self) -> float:
return self.initial_gauge_pressure_2_pa + AMESIM_REFERENCE_PRESSURE_PA
@dataclass(frozen=True)
class TestMqlPnl00rSpec:
alias: str
source_component: str
source_port: str
target_component: str
target_port: str
diameter_mm: float
length_m: float
relative_roughness: float
gas_type_index: int
def load_test_mql_pnl0001_specs(
archive_path: str | Path,
*,
@@ -111,6 +153,145 @@ def load_test_mql_pnl0001_specs(
return tuple(specs)
def load_test_mql_pnl0003_specs(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> tuple[TestMqlPnl0003Spec, ...]:
"""Load resolved PNL0003 geometry and both compliance initial states."""
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
numeric_globals = {
name: value
for name, expression in GLOBAL_PARAMETERS.items()
if (value := resolve_numeric_expression(expression, {})) is not None
}
connections = {
str(connection["alias"]): connection
for connection in CONNECTION_SPECS
if connection["submodel"] == "PNL0003"
}
specs = []
for block in re.findall(r"<LINE>.*?</LINE>", cir_text, flags=re.DOTALL):
if _optional_text(block, "SUB_NAME") != "PNL0003":
continue
alias = _required_text(block, "ALIAS")
connection = connections.get(alias)
if connection is None:
raise ValueError(f"PNL0003 line {alias!r} is absent from CONNECTION_SPECS")
real_parameters = _parameter_expressions(block, "RPARAM")
integer_parameters = _parameter_expressions(block, "IPARAM")
state_values = _evar_values(block)
specs.append(
TestMqlPnl0003Spec(
alias=alias,
source_component=str(connection["source_component"]),
source_port=str(connection["source_port"]),
target_component=str(connection["target_component"]),
target_port=str(connection["target_port"]),
diameter_mm=_required_numeric(
alias, "diam", real_parameters, numeric_globals
),
length_m=_required_numeric(alias, "le", real_parameters, numeric_globals),
relative_roughness=_required_numeric(
alias, "rr", real_parameters, numeric_globals
),
polytropic_constant=_required_numeric(
alias, "k", real_parameters, numeric_globals
),
heat_transfer_coefficient=_required_numeric(
alias, "kth", real_parameters, numeric_globals
),
external_temperature_k=_required_numeric(
alias, "extemp", real_parameters, numeric_globals
),
gas_type_index=int(
_required_numeric(alias, "gi", integer_parameters, numeric_globals)
),
mode=int(
_required_numeric(alias, "mode", integer_parameters, numeric_globals)
),
initial_temperature_1_k=_required_numeric(
alias, "t1", state_values, numeric_globals
),
initial_gauge_pressure_1_pa=_required_numeric(
alias, "p1", state_values, numeric_globals
),
initial_temperature_2_k=_required_numeric(
alias, "t2", state_values, numeric_globals
),
initial_gauge_pressure_2_pa=_required_numeric(
alias, "p2", state_values, numeric_globals
),
)
)
if set(connections) != {spec.alias for spec in specs}:
missing = sorted(set(connections) - {spec.alias for spec in specs})
raise ValueError(f"Missing PNL0003 parameter blocks: {missing}")
return tuple(specs)
def load_test_mql_pnl00r_specs(
archive_path: str | Path,
*,
cir_member: str = "test_mql_.cir",
) -> tuple[TestMqlPnl00rSpec, ...]:
"""Load resolved PNL00R geometry from the AMESim source."""
with tarfile.open(archive_path) as archive:
cir_file = archive.extractfile(cir_member)
if cir_file is None:
raise ValueError(f"Missing AMESim circuit member: {cir_member}")
cir_text = cir_file.read().decode("latin1")
numeric_globals = {
name: value
for name, expression in GLOBAL_PARAMETERS.items()
if (value := resolve_numeric_expression(expression, {})) is not None
}
connections = {
str(connection["alias"]): connection
for connection in CONNECTION_SPECS
if connection["submodel"] == "PNL00R"
}
specs = []
for block in re.findall(r"<LINE>.*?</LINE>", cir_text, flags=re.DOTALL):
if _optional_text(block, "SUB_NAME") != "PNL00R":
continue
alias = _required_text(block, "ALIAS")
connection = connections.get(alias)
if connection is None:
raise ValueError(f"PNL00R line {alias!r} is absent from CONNECTION_SPECS")
real_parameters = _parameter_expressions(block, "RPARAM")
integer_parameters = _parameter_expressions(block, "IPARAM")
specs.append(
TestMqlPnl00rSpec(
alias=alias,
source_component=str(connection["source_component"]),
source_port=str(connection["source_port"]),
target_component=str(connection["target_component"]),
target_port=str(connection["target_port"]),
diameter_mm=_required_numeric(
alias, "diam", real_parameters, numeric_globals
),
length_m=_required_numeric(alias, "le", real_parameters, numeric_globals),
relative_roughness=_required_numeric(
alias, "rr", real_parameters, numeric_globals
),
gas_type_index=int(
_required_numeric(alias, "gi", integer_parameters, numeric_globals)
),
)
)
if set(connections) != {spec.alias for spec in specs}:
missing = sorted(set(connections) - {spec.alias for spec in specs})
raise ValueError(f"Missing PNL00R parameter blocks: {missing}")
return tuple(specs)
def _parameter_expressions(block: str, tag_name: str) -> dict[str, str]:
parameters = {}
for parameter_block in re.findall(
@@ -141,11 +322,11 @@ def _required_numeric(
variables: dict[str, float],
) -> float:
if name not in expressions:
raise ValueError(f"Missing {name!r} on PNL0001 line {alias!r}")
raise ValueError(f"Missing {name!r} on line {alias!r}")
value = resolve_numeric_expression(expressions[name], variables)
if value is None:
raise ValueError(
f"Cannot resolve {name!r}={expressions[name]!r} on PNL0001 line {alias!r}"
f"Cannot resolve {name!r}={expressions[name]!r} on line {alias!r}"
)
return value
@@ -7,10 +7,18 @@ from PythonModels.components.amesim_pneumatic import (
HELIUM_PNEUMATIC_GAS,
AmesimPneumaticGas,
)
from PythonModels.components.amesim_pneumatic_line import AmesimPnl0001Pipe
from PythonModels.components.amesim_pneumatic_line import (
AmesimPnl0001Pipe,
AmesimPnl0003Pipe,
AmesimPnl00rPipe,
)
from PythonModels.systems.test_mql_line_parameters import (
TestMqlPnl0001Spec,
TestMqlPnl0003Spec,
TestMqlPnl00rSpec,
load_test_mql_pnl0001_specs,
load_test_mql_pnl0003_specs,
load_test_mql_pnl00r_specs,
)
@@ -26,6 +34,30 @@ class TestMqlPnl0001Assembly:
raise KeyError(alias)
@dataclass(frozen=True)
class TestMqlPnl0003Assembly:
specs: tuple[TestMqlPnl0003Spec, ...]
lines: dict[str, AmesimPnl0003Pipe]
def spec(self, alias: str) -> TestMqlPnl0003Spec:
for spec in self.specs:
if spec.alias == alias:
return spec
raise KeyError(alias)
@dataclass(frozen=True)
class TestMqlPnl00rAssembly:
specs: tuple[TestMqlPnl00rSpec, ...]
lines: dict[str, AmesimPnl00rPipe]
def spec(self, alias: str) -> TestMqlPnl00rSpec:
for spec in self.specs:
if spec.alias == alias:
return spec
raise KeyError(alias)
def build_test_mql_pnl0001_assembly(
archive_path: str | Path,
*,
@@ -48,3 +80,48 @@ def build_test_mql_pnl0001_assembly(
for spec in specs
}
return TestMqlPnl0001Assembly(specs=specs, lines=lines)
def build_test_mql_pnl0003_assembly(
archive_path: str | Path,
*,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPnl0003Assembly:
specs = load_test_mql_pnl0003_specs(archive_path)
lines = {
spec.alias: AmesimPnl0003Pipe(
name=spec.alias,
diameter_mm=spec.diameter_mm,
length_m=spec.length_m,
relative_roughness=spec.relative_roughness,
polytropic_constant=spec.polytropic_constant,
heat_transfer_coefficient=spec.heat_transfer_coefficient,
external_temperature_k=spec.external_temperature_k,
gas=gas,
p1_0=spec.initial_absolute_pressure_1_pa,
T1_0=spec.initial_temperature_1_k,
p2_0=spec.initial_absolute_pressure_2_pa,
T2_0=spec.initial_temperature_2_k,
)
for spec in specs
}
return TestMqlPnl0003Assembly(specs=specs, lines=lines)
def build_test_mql_pnl00r_assembly(
archive_path: str | Path,
*,
gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
) -> TestMqlPnl00rAssembly:
specs = load_test_mql_pnl00r_specs(archive_path)
lines = {
spec.alias: AmesimPnl00rPipe(
name=spec.alias,
diameter_mm=spec.diameter_mm,
length_m=spec.length_m,
relative_roughness=spec.relative_roughness,
gas=gas,
)
for spec in specs
}
return TestMqlPnl00rAssembly(specs=specs, lines=lines)