添加test_mql pneumatic_96局部参考RHS候选

PythonModels/systems/test_mql_closure.py

@@ -490,10 +490,12 @@ class TestMqlPn3P4NodeChamberSegmentClosure:
         components: TestMqlPn3P4NodeChamberSegmentComponents,
         inlet_node: TestMqlPneumaticBoundaryCondition,
         resistance_boundary: TestMqlPneumaticBoundaryCondition,
+        use_inlet_line_reference_rhs: bool = False,
     ) -> None:
         self.components = components
         self.inlet_node = inlet_node
         self.resistance_boundary = resistance_boundary
+        self.use_inlet_line_reference_rhs = use_inlet_line_reference_rhs
 
     def initial_state_vector(self) -> list[float]:
         return [
@@ -2086,6 +2088,59 @@ class TestMqlPn3P4NodeChamberSegmentClosure:
         chamber.port_a.m_flow = -chamber_to_line_flow
         chamber.port_a.h_outflow = chamber_properties.h
 
+    @staticmethod
+    def _pnl0001_reference_enthalpy_derivative(
+        *,
+        line: AmesimPnl0001Pipe,
+        line_properties: ThermodynamicProperties,
+        port_1_properties: ThermodynamicProperties,
+        port_1_flow: float,
+        port_2_properties: ThermodynamicProperties,
+        port_2_flow: float,
+        reference_temperature_k: float = 298.15,
+    ) -> VolumeState:
+        def reference_enthalpy_flow(
+            *,
+            port_flow: float,
+            connected: ThermodynamicProperties,
+        ) -> float:
+            if port_flow > 0.0:
+                pressure = connected.p
+                temperature = connected.T
+            else:
+                pressure = line_properties.p
+                temperature = line_properties.T
+            return port_flow * line.gas.pressure_reference_enthalpy(
+                pressure,
+                temperature,
+                reference_temperature=reference_temperature_k,
+            )
+
+        mass_derivative = port_1_flow + port_2_flow
+        heat_flow = (
+            line.heat_transfer_coefficient
+            * line.heat_transfer_area
+            * (line.external_temperature - line_properties.T)
+        )
+        enthalpy_flow = reference_enthalpy_flow(
+            port_flow=port_1_flow,
+            connected=port_1_properties,
+        ) + reference_enthalpy_flow(
+            port_flow=port_2_flow,
+            connected=port_2_properties,
+        )
+        reference_offset_flow = (
+            line.gas.cp * reference_temperature_k - line.gas.cv * line_properties.T
+        ) * mass_derivative
+        temperature_derivative = (
+            enthalpy_flow + reference_offset_flow + heat_flow
+        ) / (line.state.m * line.gas.cv)
+        return VolumeState(
+            m=mass_derivative,
+            U=line.gas.cv
+            * (line.state.m * temperature_derivative + line_properties.T * mass_derivative),
+        )
+
     @staticmethod
     def _primary_chamber_line_derivatives(
         *,
@@ -2706,6 +2761,15 @@ class TestMqlPn3P4NodeChamberSegmentClosure:
             outlet_node_to_line_flow=snapshot.outlet_node_to_line_flow,
             outlet_line_to_chamber_flow=snapshot.outlet_line_to_chamber_flow,
         )
+        if self.use_inlet_line_reference_rhs:
+            inlet_derivative = self._pnl0001_reference_enthalpy_derivative(
+                line=self.components.inlet_line,
+                line_properties=snapshot.inlet_line,
+                port_1_properties=snapshot.p4_port3_remote_orifice_line_port_1,
+                port_1_flow=snapshot.inlet_node_to_line_flow,
+                port_2_properties=snapshot.chamber,
+                port_2_flow=-snapshot.inlet_line_to_chamber_flow,
+            )
         (
             node_line_derivative_1,
             node_line_derivative_2,