实现test_mql PNL0003与PNL00R管路
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@@ -8,7 +8,7 @@ from PythonModels.components.amesim_pneumatic import (
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AmesimPneumaticGas,
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diameter_mm_to_area_m2,
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)
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from PythonModels.core.base import DynamicComponent
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from PythonModels.core.base import AlgebraicComponent, DynamicComponent
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from PythonModels.core.medium import ThermodynamicProperties
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from PythonModels.core.ports import PortState
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from PythonModels.core.state import VolumeState
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@@ -23,7 +23,89 @@ class AmesimPnl0001Diagnostics:
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pressure_drop_pa: float
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class AmesimPnl0001Pipe(DynamicComponent):
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class _DarcyPipeResistanceMixin:
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diameter: float
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length: float
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relative_roughness: float
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area: float
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def _mass_flow_for_pressure_drop(
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self,
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pressure_drop_pa: float,
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*,
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density: float,
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temperature: float,
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) -> float:
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if pressure_drop_pa <= 0.0:
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return 0.0
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upper = 1.0e-9
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while self._darcy_pressure_drop(
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upper,
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density=density,
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temperature=temperature,
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) < pressure_drop_pa:
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upper *= 10.0
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if upper > 1.0e3:
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raise ValueError("unable to bracket pneumatic pipe resistance flow")
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lower = 0.0
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for _ in range(80):
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middle = 0.5 * (lower + upper)
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if self._darcy_pressure_drop(
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middle,
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density=density,
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temperature=temperature,
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) < pressure_drop_pa:
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lower = middle
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else:
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upper = middle
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return 0.5 * (lower + upper)
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def _darcy_pressure_drop(
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self,
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mass_flow_kg_s: float,
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*,
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density: float,
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temperature: float,
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) -> float:
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if mass_flow_kg_s == 0.0:
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return 0.0
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reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
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friction_factor = self._friction_factor(reynolds)
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velocity = mass_flow_kg_s / (density * self.area)
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magnitude = (
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friction_factor
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* (self.length / self.diameter)
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* density
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* velocity
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* velocity
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/ 2.0
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)
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return magnitude if mass_flow_kg_s > 0.0 else -magnitude
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def _reynolds_number(self, mass_flow_kg_s: float, temperature: float) -> float:
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viscosity = helium_dynamic_viscosity(temperature)
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return 4.0 * abs(mass_flow_kg_s) / (pi * self.diameter * viscosity)
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def _friction_factor(self, reynolds_number: float) -> float:
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if reynolds_number <= 0.0:
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return 64_000_000.0
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laminar = 64.0 / reynolds_number
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if reynolds_number <= 2_300.0:
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return laminar
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turbulent = 1.0 / (
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-1.8
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* log10(
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(self.relative_roughness / 3.7) ** 1.11
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+ 6.9 / reynolds_number
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)
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) ** 2
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if reynolds_number >= 4_000.0:
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return turbulent
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fraction = (reynolds_number - 2_300.0) / 1_700.0
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return laminar + fraction * (turbulent - laminar)
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class AmesimPnl0001Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
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"""Physical first-pass implementation of AMESim ``PNL0001`` (C-R).
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Port 2 owns the lumped gas storage. Port 1 is connected through a Darcy
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@@ -193,80 +275,289 @@ class AmesimPnl0001Pipe(DynamicComponent):
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U=port_1_m_flow * inlet_h_1 + port_2_m_flow * inlet_h_2 + heat_flow,
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)
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def _mass_flow_for_pressure_drop(
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self,
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pressure_drop_pa: float,
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*,
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density: float,
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temperature: float,
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) -> float:
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if pressure_drop_pa <= 0.0:
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return 0.0
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upper = 1.0e-9
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while self._darcy_pressure_drop(
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upper,
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density=density,
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temperature=temperature,
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) < pressure_drop_pa:
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upper *= 10.0
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if upper > 1.0e3:
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raise ValueError("unable to bracket PNL0001 resistance flow")
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lower = 0.0
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for _ in range(80):
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middle = 0.5 * (lower + upper)
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if self._darcy_pressure_drop(
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middle,
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density=density,
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temperature=temperature,
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) < pressure_drop_pa:
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lower = middle
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else:
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upper = middle
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return 0.5 * (lower + upper)
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def _darcy_pressure_drop(
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class AmesimPnl0003Pipe(_DarcyPipeResistanceMixin, DynamicComponent):
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"""First-pass AMESim ``PNL0003`` (C-R-C) pipe.
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The two pipe-end compliances are represented as equal half-volume gas
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stores connected by the same auditable Darcy resistance used for PNL0001.
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Center flow is positive from port 1 storage to port 2 storage.
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"""
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state_size = 4
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def __init__(
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self,
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mass_flow_kg_s: float,
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name: str,
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*,
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density: float,
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temperature: float,
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) -> float:
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if mass_flow_kg_s == 0.0:
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diameter_mm: float,
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length_m: float,
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relative_roughness: float,
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polytropic_constant: float = 1.35,
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heat_transfer_coefficient: float = 0.0,
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external_temperature_k: float = 293.15,
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gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
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p1_0: float = 101_325.0,
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T1_0: float = 293.15,
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p2_0: float = 101_325.0,
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T2_0: float = 293.15,
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) -> None:
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if diameter_mm <= 0.0:
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raise ValueError("diameter_mm must be positive")
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if length_m <= 0.0:
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raise ValueError("length_m must be positive")
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if relative_roughness < 0.0:
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raise ValueError("relative_roughness must be non-negative")
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if polytropic_constant <= 0.0:
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raise ValueError("polytropic_constant must be positive")
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if heat_transfer_coefficient < 0.0:
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raise ValueError("heat_transfer_coefficient must be non-negative")
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if external_temperature_k <= 0.0:
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raise ValueError("external_temperature_k must be positive")
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super().__init__(name=name)
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self.diameter = diameter_mm * 1.0e-3
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self.length = length_m
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self.relative_roughness = relative_roughness
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self.polytropic_constant = polytropic_constant
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self.heat_transfer_coefficient = heat_transfer_coefficient
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self.external_temperature = external_temperature_k
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self.gas = gas
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self.area = diameter_mm_to_area_m2(diameter_mm)
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self.volume = self.area * self.length
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self.compliance_volume = self.volume / 2.0
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self.heat_transfer_area = pi * self.diameter * self.length
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self.state_1 = self._initial_state(p1_0, T1_0)
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self.state_2 = self._initial_state(p2_0, T2_0)
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self.port_1 = PortState()
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self.port_2 = PortState()
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def _initial_state(self, pressure: float, temperature: float) -> VolumeState:
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rho = self.gas.density(pressure, temperature)
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mass = rho * self.compliance_volume
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return VolumeState(
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m=mass,
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U=mass * self.gas.specific_internal_energy(temperature),
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)
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def get_state_vector(self) -> list[float]:
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return [*self.state_1.as_vector(), *self.state_2.as_vector()]
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def set_state_vector(self, values: list[float]) -> None:
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if len(values) != 4:
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raise ValueError("PNL0003 state vector requires four values")
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self.state_1 = VolumeState.from_vector(values[:2])
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self.state_2 = VolumeState.from_vector(values[2:])
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def properties_1(self) -> ThermodynamicProperties:
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properties = self._properties(self.state_1)
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self.port_1.p = properties.p
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self.port_1.h_outflow = properties.h
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return properties
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def properties_2(self) -> ThermodynamicProperties:
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properties = self._properties(self.state_2)
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self.port_2.p = properties.p
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self.port_2.h_outflow = properties.h
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return properties
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def _properties(self, state: VolumeState) -> ThermodynamicProperties:
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if state.m <= 0.0:
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raise ValueError("pipe mass must stay positive")
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temperature = self.gas.temperature_from_internal_energy(state.U / state.m)
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density = state.m / self.compliance_volume
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pressure = self.gas.pressure(density, temperature)
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return ThermodynamicProperties(
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p=pressure,
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T=temperature,
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rho=density,
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u=state.U / state.m,
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h=self.gas.specific_enthalpy(temperature),
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)
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def gas_mass_g(self) -> float:
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return (self.state_1.m + self.state_2.m) * 1.0e3
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def resistance_mass_flow(self) -> float:
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"""Return center mass flow from port 1 storage to port 2 storage."""
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port_1 = self.properties_1()
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port_2 = self.properties_2()
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pressure_difference = port_1.p - port_2.p
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if pressure_difference == 0.0:
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return 0.0
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upstream = port_1 if pressure_difference > 0.0 else port_2
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magnitude = self._mass_flow_for_pressure_drop(
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abs(pressure_difference),
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density=upstream.rho,
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temperature=upstream.T,
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)
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return magnitude if pressure_difference > 0.0 else -magnitude
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def diagnostics(
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self,
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*,
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mass_flow_kg_s: float,
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temperature_k: float | None = None,
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) -> AmesimPnl0001Diagnostics:
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port_1 = self.properties_1()
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port_2 = self.properties_2()
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temperature = temperature_k or (port_1.T if mass_flow_kg_s >= 0.0 else port_2.T)
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density = port_1.rho if mass_flow_kg_s >= 0.0 else port_2.rho
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reynolds = self._reynolds_number(mass_flow_kg_s, temperature)
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friction_factor = self._friction_factor(reynolds)
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velocity = mass_flow_kg_s / (density * self.area)
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magnitude = (
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friction_factor
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* (self.length / self.diameter)
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* density
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* velocity
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* velocity
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pressure_drop = self._darcy_pressure_drop(
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mass_flow_kg_s,
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density=density,
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temperature=temperature,
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)
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return AmesimPnl0001Diagnostics(
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mass_flow_kg_s=mass_flow_kg_s,
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reynolds_number=reynolds,
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gas_velocity_m_s=velocity,
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friction_factor=friction_factor,
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pressure_drop_pa=pressure_drop,
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)
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def derivatives_from_connections(
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self,
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*,
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port_1_m_flow: float,
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connected_h_1: float,
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port_2_m_flow: float,
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connected_h_2: float,
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) -> tuple[VolumeState, VolumeState]:
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port_1 = self.properties_1()
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port_2 = self.properties_2()
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center_flow = self.resistance_mass_flow()
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heat_flow_each = (
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self.heat_transfer_coefficient
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* self.heat_transfer_area
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* (self.external_temperature - 0.5 * (port_1.T + port_2.T))
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/ 2.0
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)
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return magnitude if mass_flow_kg_s > 0.0 else -magnitude
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port_1_external_h = self.connection_inlet_enthalpy(
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port_m_flow=port_1_m_flow,
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connected_h=connected_h_1,
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internal_h=port_1.h,
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)
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port_2_external_h = self.connection_inlet_enthalpy(
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port_m_flow=port_2_m_flow,
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connected_h=connected_h_2,
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internal_h=port_2.h,
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)
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port_1_center_h = self.connection_inlet_enthalpy(
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port_m_flow=-center_flow,
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connected_h=port_2.h,
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internal_h=port_1.h,
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)
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port_2_center_h = self.connection_inlet_enthalpy(
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port_m_flow=center_flow,
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connected_h=port_1.h,
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internal_h=port_2.h,
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)
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return (
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VolumeState(
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m=port_1_m_flow - center_flow,
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U=(
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port_1_m_flow * port_1_external_h
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- center_flow * port_1_center_h
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+ heat_flow_each
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),
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),
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VolumeState(
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m=port_2_m_flow + center_flow,
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U=(
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port_2_m_flow * port_2_external_h
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+ center_flow * port_2_center_h
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+ heat_flow_each
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),
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),
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)
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def _reynolds_number(self, mass_flow_kg_s: float, temperature: float) -> float:
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viscosity = helium_dynamic_viscosity(temperature)
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return 4.0 * abs(mass_flow_kg_s) / (pi * self.diameter * viscosity)
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def _friction_factor(self, reynolds_number: float) -> float:
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if reynolds_number <= 0.0:
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return 64_000_000.0
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laminar = 64.0 / reynolds_number
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if reynolds_number <= 2_300.0:
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return laminar
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turbulent = 1.0 / (
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-1.8
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* log10(
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(self.relative_roughness / 3.7) ** 1.11
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+ 6.9 / reynolds_number
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)
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) ** 2
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if reynolds_number >= 4_000.0:
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return turbulent
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fraction = (reynolds_number - 2_300.0) / 1_700.0
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return laminar + fraction * (turbulent - laminar)
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class AmesimPnl00rPipe(_DarcyPipeResistanceMixin, AlgebraicComponent):
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"""First-pass AMESim ``PNL00R`` (R) pipe resistance."""
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def __init__(
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self,
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name: str,
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*,
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diameter_mm: float,
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length_m: float,
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relative_roughness: float,
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gas: AmesimPneumaticGas = HELIUM_PNEUMATIC_GAS,
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) -> None:
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if diameter_mm <= 0.0:
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raise ValueError("diameter_mm must be positive")
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if length_m <= 0.0:
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raise ValueError("length_m must be positive")
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if relative_roughness < 0.0:
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raise ValueError("relative_roughness must be non-negative")
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super().__init__(name=name)
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self.diameter = diameter_mm * 1.0e-3
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self.length = length_m
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self.relative_roughness = relative_roughness
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self.gas = gas
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self.area = diameter_mm_to_area_m2(diameter_mm)
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self.port_1 = PortState()
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self.port_2 = PortState()
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def mass_flow(
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self,
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*,
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port_1_pressure_pa: float,
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port_1_temperature_k: float,
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port_2_pressure_pa: float,
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port_2_temperature_k: float,
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) -> float:
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"""Return mass flow from port 1 to port 2 in kg/s."""
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if port_1_pressure_pa <= 0.0 or port_2_pressure_pa <= 0.0:
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raise ValueError("port pressures must be positive")
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if port_1_temperature_k <= 0.0 or port_2_temperature_k <= 0.0:
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raise ValueError("port temperatures must be positive")
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pressure_difference = port_1_pressure_pa - port_2_pressure_pa
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if pressure_difference == 0.0:
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return 0.0
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upstream_pressure = max(port_1_pressure_pa, port_2_pressure_pa)
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upstream_temperature = (
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port_1_temperature_k
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if pressure_difference > 0.0
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else port_2_temperature_k
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)
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density = self.gas.density(upstream_pressure, upstream_temperature)
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magnitude = self._mass_flow_for_pressure_drop(
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abs(pressure_difference),
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density=density,
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temperature=upstream_temperature,
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)
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return magnitude if pressure_difference > 0.0 else -magnitude
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def diagnostics(
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self,
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*,
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mass_flow_kg_s: float,
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pressure_pa: float,
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temperature_k: float,
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) -> AmesimPnl0001Diagnostics:
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density = self.gas.density(pressure_pa, temperature_k)
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reynolds = self._reynolds_number(mass_flow_kg_s, temperature_k)
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friction_factor = self._friction_factor(reynolds)
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velocity = mass_flow_kg_s / (density * self.area)
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pressure_drop = self._darcy_pressure_drop(
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mass_flow_kg_s,
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density=density,
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temperature=temperature_k,
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)
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return AmesimPnl0001Diagnostics(
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mass_flow_kg_s=mass_flow_kg_s,
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reynolds_number=reynolds,
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gas_velocity_m_s=velocity,
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friction_factor=friction_factor,
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pressure_drop_pa=pressure_drop,
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)
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def helium_dynamic_viscosity(temperature_k: float) -> float:
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@@ -3860,6 +3860,8 @@ class TestMqlSystem:
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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)
|
||||
Reference in new issue
Block a user