接入test_mql双管路气室与PN3节点
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@@ -119,6 +119,29 @@ class TestMqlPnl0001ChamberSegmentSnapshot:
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outlet_flow: float
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@dataclass(frozen=True)
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class TestMqlPnl0001PairChamberSegmentComponents:
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inlet_line: AmesimPnl0001Pipe
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outlet_line: AmesimPnl0001Pipe
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volume: AmesimPneumaticVolume
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inlet_orifice: AmesimPneumaticOrifice
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outlet_orifice: AmesimPneumaticOrifice
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spec: TestMqlPneumaticChamberSegmentSpec
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@dataclass(frozen=True)
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class TestMqlPnl0001PairChamberSegmentSnapshot:
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inlet_line: ThermodynamicProperties
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chamber: ThermodynamicProperties
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outlet_line: ThermodynamicProperties
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inlet_node: ThermodynamicProperties
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outlet_node: ThermodynamicProperties
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inlet_node_to_line_flow: float
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inlet_line_to_chamber_flow: float
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outlet_node_to_line_flow: float
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outlet_line_to_chamber_flow: float
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@dataclass(frozen=True)
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class TestMqlPneumaticBranchComponents:
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name: str
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@@ -555,3 +578,199 @@ class TestMqlPnl0001ChamberSegmentClosure:
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internal_h=snapshot.chamber.h,
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)
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return [*line_derivative.as_vector(), *chamber_derivative.as_vector()]
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class TestMqlPnl0001PairChamberSegmentClosure:
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"""Six-state fixed chamber segment with both PNL0001 compliance states.
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Generated C shows that both line instances receive ``t1/p1`` from their
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PN3 nodes and send their explicit ``t2/p2`` states to the fixed orifices.
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The reduced closure therefore prescribes node pressure/temperature at both
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resistive port-1 boundaries while keeping both line storage states native.
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"""
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def __init__(
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self,
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*,
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components: TestMqlPnl0001PairChamberSegmentComponents,
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inlet_node: TestMqlPneumaticBoundaryCondition,
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outlet_node: TestMqlPneumaticBoundaryCondition,
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) -> None:
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self.components = components
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self.inlet_node = inlet_node
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self.outlet_node = outlet_node
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def initial_state_vector(self) -> list[float]:
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return [
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*self.components.inlet_line.get_state_vector(),
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*self.components.volume.get_state_vector(),
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*self.components.outlet_line.get_state_vector(),
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]
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def apply_state_vector(self, values: list[float]) -> None:
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if len(values) != 6:
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raise ValueError("PNL0001 pair/chamber state vector requires six values")
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self.components.inlet_line.set_state_vector(values[:2])
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self.components.volume.set_state_vector(values[2:4])
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self.components.outlet_line.set_state_vector(values[4:])
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def snapshot(
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self,
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state_vector: list[float] | None = None,
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) -> TestMqlPnl0001PairChamberSegmentSnapshot:
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if state_vector is not None:
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self.apply_state_vector(state_vector)
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inlet_line = self.components.inlet_line.properties()
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chamber = self.components.volume.properties()
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outlet_line = self.components.outlet_line.properties()
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inlet_node = self.inlet_node.properties(self.components.inlet_line.gas)
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outlet_node = self.outlet_node.properties(self.components.outlet_line.gas)
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inlet_node_to_line_flow = self.components.inlet_line.resistance_mass_flow(
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port_1_pressure_pa=inlet_node.p,
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port_1_temperature_k=inlet_node.T,
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)
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outlet_node_to_line_flow = self.components.outlet_line.resistance_mass_flow(
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port_1_pressure_pa=outlet_node.p,
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port_1_temperature_k=outlet_node.T,
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)
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inlet_line_to_chamber_flow = self._line_to_chamber_flow(
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line=inlet_line,
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chamber=chamber,
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orifice=self.components.inlet_orifice,
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)
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outlet_line_to_chamber_flow = self._line_to_chamber_flow(
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line=outlet_line,
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chamber=chamber,
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orifice=self.components.outlet_orifice,
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)
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snapshot = TestMqlPnl0001PairChamberSegmentSnapshot(
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inlet_line=inlet_line,
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chamber=chamber,
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outlet_line=outlet_line,
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inlet_node=inlet_node,
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outlet_node=outlet_node,
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inlet_node_to_line_flow=inlet_node_to_line_flow,
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inlet_line_to_chamber_flow=inlet_line_to_chamber_flow,
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outlet_node_to_line_flow=outlet_node_to_line_flow,
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outlet_line_to_chamber_flow=outlet_line_to_chamber_flow,
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)
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self._write_port_states(snapshot)
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return snapshot
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@staticmethod
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def _line_to_chamber_flow(
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*,
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line: ThermodynamicProperties,
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chamber: ThermodynamicProperties,
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orifice: AmesimPneumaticOrifice,
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) -> float:
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upstream_temperature = line.T if line.p >= chamber.p else chamber.T
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return orifice.mass_flow(line.p, chamber.p, upstream_temperature)
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@staticmethod
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def _port(
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component: AmesimPneumaticVolume | AmesimPneumaticOrifice,
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port_name: str,
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) -> PortState:
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return TestMqlPneumaticChamberSegmentClosure._port(component, port_name)
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def _write_port_states(
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self,
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snapshot: TestMqlPnl0001PairChamberSegmentSnapshot,
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) -> None:
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spec = self.components.spec
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chamber = self.components.volume
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chamber_inlet_port = self._port(chamber, spec.volume_inlet_port)
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chamber_outlet_port = self._port(chamber, spec.volume_outlet_port)
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self._write_line_side(
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line=self.components.inlet_line,
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line_properties=snapshot.inlet_line,
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node_properties=snapshot.inlet_node,
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node_to_line_flow=snapshot.inlet_node_to_line_flow,
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line_to_chamber_flow=snapshot.inlet_line_to_chamber_flow,
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orifice=self.components.inlet_orifice,
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orifice_boundary_port=spec.inlet_orifice_boundary_port,
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orifice_volume_port=spec.inlet_orifice_volume_port,
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chamber_port=chamber_inlet_port,
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chamber_properties=snapshot.chamber,
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)
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self._write_line_side(
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line=self.components.outlet_line,
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line_properties=snapshot.outlet_line,
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node_properties=snapshot.outlet_node,
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node_to_line_flow=snapshot.outlet_node_to_line_flow,
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line_to_chamber_flow=snapshot.outlet_line_to_chamber_flow,
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orifice=self.components.outlet_orifice,
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orifice_boundary_port=spec.outlet_orifice_boundary_port,
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orifice_volume_port=spec.outlet_orifice_volume_port,
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chamber_port=chamber_outlet_port,
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chamber_properties=snapshot.chamber,
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)
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def _write_line_side(
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self,
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*,
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line: AmesimPnl0001Pipe,
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line_properties: ThermodynamicProperties,
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node_properties: ThermodynamicProperties,
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node_to_line_flow: float,
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line_to_chamber_flow: float,
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orifice: AmesimPneumaticOrifice,
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orifice_boundary_port: str,
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orifice_volume_port: str,
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chamber_port: PortState,
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chamber_properties: ThermodynamicProperties,
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) -> None:
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line.port_1.p = node_properties.p
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line.port_1.m_flow = node_to_line_flow
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line.port_1.h_outflow = line_properties.h
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line.port_2.p = line_properties.p
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line.port_2.m_flow = -line_to_chamber_flow
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boundary_port = self._port(orifice, orifice_boundary_port)
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volume_port = self._port(orifice, orifice_volume_port)
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boundary_port.p = line_properties.p
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boundary_port.m_flow = line_to_chamber_flow
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boundary_port.h_outflow = line_properties.h
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volume_port.p = chamber_properties.p
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volume_port.m_flow = -line_to_chamber_flow
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volume_port.h_outflow = chamber_properties.h
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chamber_port.m_flow = line_to_chamber_flow
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def rhs(self, state_vector: list[float]) -> list[float]:
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snapshot = self.snapshot(state_vector)
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inlet_derivative = self.components.inlet_line.derivatives_from_connections(
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port_1_m_flow=snapshot.inlet_node_to_line_flow,
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connected_h_1=snapshot.inlet_node.h,
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port_2_m_flow=-snapshot.inlet_line_to_chamber_flow,
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connected_h_2=snapshot.chamber.h,
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)
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outlet_derivative = self.components.outlet_line.derivatives_from_connections(
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port_1_m_flow=snapshot.outlet_node_to_line_flow,
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connected_h_1=snapshot.outlet_node.h,
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port_2_m_flow=-snapshot.outlet_line_to_chamber_flow,
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connected_h_2=snapshot.chamber.h,
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)
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chamber = self.components.volume
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spec = self.components.spec
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chamber_derivative = chamber.derivatives_from_two_connections(
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port_a_m_flow=self._port(chamber, "port_1").m_flow,
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connected_h_a=(
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snapshot.inlet_line.h
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if spec.volume_inlet_port == "port_1"
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else snapshot.outlet_line.h
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),
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port_b_m_flow=self._port(chamber, "port_2").m_flow,
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connected_h_b=(
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snapshot.inlet_line.h
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if spec.volume_inlet_port == "port_2"
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else snapshot.outlet_line.h
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),
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internal_h=snapshot.chamber.h,
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)
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return [
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*inlet_derivative.as_vector(),
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*chamber_derivative.as_vector(),
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*outlet_derivative.as_vector(),
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]
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