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纳管热路径优化、15 单元运行证据、浏览器与 API 报告，并补充北京时间更新日志和遗留问题。

.gitattributes

@@ -0,0 +1,3 @@
+*.bat text eol=crlf
+*.cmd text eol=crlf
+*.sh text eol=lf

.github/workflows/solver-regression.yml

@@ -0,0 +1,180 @@
+name: Solver regression
+
+on:
+  push:
+    paths:
+      - "app/simulation/**"
+      - "tests/**"
+      - "requirements.txt"
+      - "constraints/**"
+      - ".python-version"
+      - "README.md"
+      - ".github/workflows/solver-regression.yml"
+  pull_request:
+    paths:
+      - "app/simulation/**"
+      - "tests/**"
+      - "requirements.txt"
+      - "constraints/**"
+      - ".python-version"
+      - "README.md"
+      - ".github/workflows/solver-regression.yml"
+  schedule:
+    - cron: "17 3 * * 1-6"
+    - cron: "17 3 * * 0"
+  workflow_dispatch:
+    inputs:
+      suite:
+        description: Regression tier
+        required: true
+        default: quick
+        type: choice
+        options:
+          - quick
+          - historical
+          - main-long
+      case:
+        description: Longest main-model horizon (predecessors run first)
+        required: true
+        default: 0.2s
+        type: choice
+        options:
+          - 0.2s
+          - 1s
+          - 5s
+          - 10s
+      lane:
+        description: Output sampling lane
+        required: true
+        default: production
+        type: choice
+        options:
+          - solver-only
+          - production
+
+concurrency:
+  group: solver-regression-${{ github.ref }}-${{ github.event_name }}
+  cancel-in-progress: false
+
+permissions:
+  contents: read
+
+jobs:
+  quick:
+    if: >-
+      github.event_name == 'push' ||
+      github.event_name == 'pull_request' ||
+      (github.event_name == 'workflow_dispatch' && inputs.suite == 'quick')
+    runs-on: ubuntu-24.04
+    timeout-minutes: 15
+    steps:
+      - uses: actions/checkout@v4
+      - uses: actions/setup-python@v5
+        with:
+          python-version-file: .python-version
+          cache: pip
+          cache-dependency-path: |
+            requirements.txt
+            constraints/python312-direct.txt
+            constraints/python312-linux-x86_64.lock
+      - name: Install hashed Linux release lock
+        run: |
+          python -m pip install \
+            --force-reinstall \
+            -r constraints/python312-linux-x86_64.lock
+          python -m pip check
+      - name: Run solver foundation tests
+        env:
+          SYSTEM_SIMULATION_VERIFY_LOCKED_ENV: "1"
+        run: |
+          python -W error::ResourceWarning -m unittest \
+            tests.test_dependency_constraints \
+            tests.test_benchmark_regression \
+            tests.test_physical_state_v21 \
+            tests.test_test_mql_ame_contract \
+            tests.test_test_mql_8_regression \
+            tests.test_mql_full_branches_regression \
+            tests.test_pressure_flow_causal_execution \
+            tests.test_stream_pressure_block_solver \
+            tests.test_core_solver \
+            tests.test_supported_piston_tangent \
+            tests.test_three_piston_tangent \
+            tests.test_sparse_secant_jacobian \
+            tests.test_generic_jacobian_sparsity \
+            tests.test_generic_system_xml_simulation
+
+  historical-nightly:
+    if: >-
+      (github.event_name == 'schedule' && github.event.schedule == '17 3 * * 1-6') ||
+      (github.event_name == 'workflow_dispatch' && inputs.suite == 'historical')
+    runs-on: ubuntu-24.04
+    timeout-minutes: 15
+    steps:
+      - uses: actions/checkout@v4
+      - uses: actions/setup-python@v5
+        with:
+          python-version-file: .python-version
+          cache: pip
+          cache-dependency-path: |
+            requirements.txt
+            constraints/python312-direct.txt
+            constraints/python312-linux-x86_64.lock
+      - name: Install hashed Linux release lock
+        run: |
+          python -m pip install \
+            --force-reinstall \
+            -r constraints/python312-linux-x86_64.lock
+          python -m pip check
+      - name: Run 0.81 and 2.10 second historical regression
+        run: |
+          mkdir -p artifacts
+          python -m app.simulation.benchmark_regression \
+            --manifest tests/baselines/simulation/test_mql_full_branches/manifest.json \
+            --lane production \
+            --output artifacts/test-mql-full-branches.json
+      - if: always()
+        uses: actions/upload-artifact@v4
+        with:
+          name: historical-solver-regression
+          path: artifacts/*.json
+          if-no-files-found: warn
+
+  main-periodic:
+    if: >-
+      (github.event_name == 'schedule' && github.event.schedule == '17 3 * * 0') ||
+      (github.event_name == 'workflow_dispatch' && inputs.suite == 'main-long')
+    runs-on: ubuntu-24.04
+    timeout-minutes: 180
+    steps:
+      - uses: actions/checkout@v4
+      - uses: actions/setup-python@v5
+        with:
+          python-version-file: .python-version
+          cache: pip
+          cache-dependency-path: |
+            requirements.txt
+            constraints/python312-direct.txt
+            constraints/python312-linux-x86_64.lock
+      - name: Install hashed Linux release lock
+        run: |
+          python -m pip install \
+            --force-reinstall \
+            -r constraints/python312-linux-x86_64.lock
+          python -m pip check
+      - name: Run bounded progressive main-model regression
+        env:
+          REQUESTED_CASE: ${{ github.event_name == 'workflow_dispatch' && inputs.case || '10s' }}
+          REQUESTED_LANE: ${{ github.event_name == 'workflow_dispatch' && inputs.lane || 'production' }}
+        run: |
+          mkdir -p artifacts
+          python -m app.simulation.benchmark_regression \
+            --manifest tests/baselines/simulation/test_mql_8/manifest.json \
+            --lane "$REQUESTED_LANE" \
+            --case "$REQUESTED_CASE" \
+            --output artifacts/test-mql-8-progressive.json
+      - if: always()
+        uses: actions/upload-artifact@v4
+        with:
+          name: main-model-progressive-regression
+          path: artifacts/*.json
+          if-no-files-found: warn

.gitignore

@@ -12,11 +12,17 @@ htmlcov/
 # Local virtual environments
 .venv/
 .venv-win/
-PythonModels/runs/
+
+# Local Linux toolchain (downloaded for the startup scripts)
+.tools/node-*-linux-x64/
+
 app/data/
 frontend/node_modules/
 frontend/dist/
 frontend/.vite/
+frontend/test-results/
+frontend/playwright-report/
+frontend/blob-report/
 venv/
 env/
 

.python-version

@@ -0,0 +1 @@
+3.12.3

AmesimModels/help/source/PNCH012.c

@@ -0,0 +1,388 @@
+/* Submodel PNCH012 skeleton created by AME Submodel editing utility
+   mar. oct. 9 14:41:15 2018 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNCH012
+--------------------------------------------------------------------------------
+DESCRIPTION :
+   This submodel represents a pneumatic chamber with a variable volume
+   and pressure dynamics.
+
+   Each port receives a mass flow rate and an enthalpy flow rate as
+   input and gives the pressure and the temperature of the chamber as
+   output. Each port receives also the volume and volume variation as
+   input. The total volume is calculated by summing the four volume
+   inputs and a dead volume which is a parameter of PNCH012.
+
+   The model takes into account heat exchange. It express the variation
+   of internal energy U using the first law of thermodynamics applied to
+   an open system. Therefore, this model should be preferred to the simple
+   polytropic chamber PNCH011.
+
+   The total volume of the chamber is limited to a lower value equal to
+   the dead volume divided by 100.
+--------------------------------------------------------------------------------
+USAGE :
+   Use this submodel to simulate a pneumatic chamber in a jack, spool
+   valve or any pneumatic chamber in which the volume can vary.
+
+   This submodel can be directly connected to any pneumatic PCD
+   component or standard pneumatic component.
+
+   The submodels PNGD001, PNGD002, PNGD003, PNGD004 or PNRGD00 should be
+   included in your circuit to define the characteristics of the gas.
+--------------------------------------------------------------------------------
+PARAMETER SETTINGS:
+   The dead volume is the volume of the pneumatic fluid when all the input
+   volumes are zero. It is essential that this volume must be greater
+   than zero.
+--------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR :
+   2002 FS from PNCH12
+--------------------------------------------------------------------------------
+INDEX OF REVISIONS :
+   2008  OBA - Real gas improvements : the mass and volume were considered as
+         internal state variable, they are now coded as internal basic
+         variable. The mass initialisation was removed as it was linked
+         to the perfect gas formulation.
+--------------------------------------------------------------------------------
+LIST OF FUNCTIONS USED :
+   pn2getatp : get atmospheric pressure
+   firstc_   : checks if this is the first call to this submodel
+   pn2vol_   : pneumatic chamber with heat exchange
+   stepdn_   : reduce simulation step
+--------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNCH012"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 4 real parameters:
+
+   cvol0  dead volume                  [L -> m**3]
+   kth    thermal exchange coefficient [J/m**2/K/s -> W/m**2/K]
+   sth    thermal exchange area        [m**2]
+   extemp external temperature         [K]
+*/
+
+
+/* There is 1 integer parameter:
+
+   gi gas type index
+*/
+
+void pnch012in_(int *n, double rp[4], int ip[1], double c[2]
+      , int ic[2], double *temp, double *press, double *dvol1
+      , double *vol1, double *dvol2, double *vol2, double *dvol3
+      , double *vol3, double *dvol4, double *vol4)
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi;
+   double cvol0, kth, sth, extemp;
+
+   gi         = ip[0];
+
+   cvol0      = rp[0];
+   kth        = rp[1];
+   sth        = rp[2];
+   extemp     = rp[3];
+   loop = 0;
+   error = 0;
+
+/* Assign default values to input(s) with default.  */
+
+   *dvol1     =     0.00000000000000e+000;
+   *vol1      =     0.00000000000000e+000;
+   *dvol2     =     0.00000000000000e+000;
+   *vol2      =     0.00000000000000e+000;
+   *dvol3     =     0.00000000000000e+000;
+   *vol3      =     0.00000000000000e+000;
+   *dvol4     =     0.00000000000000e+000;
+   *vol4      =     0.00000000000000e+000;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..3]
+   *temp
+   *press
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (cvol0 <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nVolume chamber must be strictly positive.\n");
+   }
+
+   if (kth < 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nthermal exchange coefficient must be positive.\n");
+   }
+
+   if (sth < 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nthermal exchange area must be positive.\n");
+   }
+
+   if (extemp <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nExternal temperature must be strictly positive.\n");
+   }
+
+   if (*temp <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial temperature must be strictly positive.\n");
+   }
+
+
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+
+   if(error == 1)
+   {
+      amefprintf(stderr, "\nWarning in %s instance %d.\n", _SUBMODELNAME_, *n);
+   }
+   else if(error == 2)
+   {
+      amefprintf(stderr, "\nFatal error in %s instance %d.\n", _SUBMODELNAME_, *n);
+      amefprintf(stderr, "Terminating the program.\n");
+      AmeExit(1);
+   }
+
+/* Common -> SI units conversions. */
+
+   rp[0]    *= 1.00000000000000e-003;
+   cvol0      = rp[0];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+
+   c[0] = cvol0 / 100;
+
+   /* Set initial value for the test of limited volume :
+      ic[1] = 1 when the chamber volume is limited to cvol0 / 100 else ic[1] = 0*/
+   ic[1] = 0;
+
+   /* set atmospheric pressure */
+   c[1] = pn2getatp_();
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 4 ports.
+
+   Port 1 has 6 variables:
+
+      1 temp      temperature                    [K]               explicit state (derivative `dtemp')
+      2 press     pressure                       [Pa]              explicit state (derivative `dpress')
+      3 dh1       enthalpy flow rate at port 1   [J/s -> W]        basic variable input
+      4 dm1       mass flow rate at port 1       [g/s -> kg/s]     basic variable input
+      5 dvol1     derivative of volume at port 1 [L/min -> m**3/s] basic variable input with default 0.000000e+000
+      6 vol1      volume at port 1               [cm**3 -> m**3]   basic variable input with default 0.000000e+000
+
+   Port 2 has 6 variables:
+
+      1 temp2      duplicate of temp             
+      2 press2     duplicate of press            
+      3 dh2        enthalpy flow rate at port 2   [J/s -> W]        basic variable input
+      4 dm2        mass flow rate at port 2       [g/s -> kg/s]     basic variable input
+      5 dvol2      derivative of volume at port 2 [L/min -> m**3/s] basic variable input with default 0.000000e+000
+      6 vol2       volume at port 2               [cm**3 -> m**3]   basic variable input with default 0.000000e+000
+
+   Port 3 has 6 variables:
+
+      1 temp3      duplicate of temp             
+      2 press3     duplicate of press            
+      3 dh3        enthalpy flow rate at port 3   [J/s -> W]        basic variable input
+      4 dm3        mass flow rate at port 3       [g/s -> kg/s]     basic variable input
+      5 dvol3      derivative of volume at port 3 [L/min -> m**3/s] basic variable input with default 0.000000e+000
+      6 vol3       volume at port 3               [cm**3 -> m**3]   basic variable input with default 0.000000e+000
+
+   Port 4 has 6 variables:
+
+      1 temp4      duplicate of temp             
+      2 press4     duplicate of press            
+      3 dh4        enthalpy flow rate at port 4   [J/s -> W]        basic variable input
+      4 dm4        mass flow rate at port 4       [g/s -> kg/s]     basic variable input
+      5 dvol4      derivative of volume at port 4 [L/min -> m**3/s] basic variable input with default 0.000000e+000
+      6 vol4       volume at port 4               [cm**3 -> m**3]   basic variable input with default 0.000000e+000
+*/
+
+/*  There are 2 internal variables.
+
+      1 vol       volume of pneumatic chamber [cm**3 -> m**3] basic variable
+      2 mgas1     mass of gas in chamber      [g -> kg]       basic variable
+*/
+
+void pnch012_(int *n, double *temp, double *dtemp, double *press
+      , double *dpress, double *dh1, double *dm1, double *dvol1
+      , double *vol1, double *dh2, double *dm2, double *dvol2
+      , double *vol2, double *dh3, double *dm3, double *dvol3
+      , double *vol3, double *dh4, double *dm4, double *dvol4
+      , double *vol4, double *vol, double *mgas1, double rp[4]
+      , int ip[1], double c[2], int ic[2])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   double dvol;
+   double sdm, sdh;
+   double dq;
+   double pressa;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi;
+   double cvol0, kth, sth, extemp;
+
+   gi         = ip[0];
+
+   cvol0      = rp[0];
+   kth        = rp[1];
+   sth        = rp[2];
+   extemp     = rp[3];
+   loop = 0;
+
+/* Common -> SI units conversions. */
+
+   *dm1      *= 1.00000000000000e-003;
+   *dvol1    *= 1.66666666666667e-005;
+   *vol1     *= 1.00000000000000e-006;
+   *dm2      *= 1.00000000000000e-003;
+   *dvol2    *= 1.66666666666667e-005;
+   *vol2     *= 1.00000000000000e-006;
+   *dm3      *= 1.00000000000000e-003;
+   *dvol3    *= 1.66666666666667e-005;
+   *vol3     *= 1.00000000000000e-006;
+   *dm4      *= 1.00000000000000e-003;
+   *dvol4    *= 1.66666666666667e-005;
+   *vol4     *= 1.00000000000000e-006;
+
+/*
+   Set all submodel outputs below:
+
+   *dtemp      = ??;
+   *dpress     = ??;
+   *vol        = ??;
+   *mgas1      = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressure */
+   pressa = *press + c[1];
+
+   /*** sum of the volume variation and volume ***/
+   dvol = *dvol1 + *dvol2 + *dvol3 + *dvol4;
+
+   /*** setup the initial mass of the gaz inside of the chamber ***/
+   *vol = *vol1 + *vol2 + *vol3 + *vol4 + cvol0;
+
+   /*** sum of the flows ***/
+   sdm = *dm1 + *dm2 + *dm3 + *dm4;   /* mass flow */
+   sdh = *dh1 + *dh2 + *dh3 + *dh4;   /* heat flow */
+
+   /*** V, M, T and P can not be lower than zero ***/
+   *vol = llimit_(vol, &c[0], &ic[0]);
+
+   if (ic[0] == -1)
+   {
+      dvol = 0.;
+      if (ic[1] == 0)
+      {
+         amefprintf(stderr, "\nWarning in %s instance %d chamber volume is limited by cvol0 / 100 = %g cm**3.\n", _SUBMODELNAME_, *n, c[0]*1E+6);
+         ic[1] = 1;
+      }
+   }
+
+   if (*vol < c[0]/10)
+   {
+      *vol = c[0]/10;
+   }
+
+   if ( (*mgas1 <= 1.0e-10) && (!firstc_()) )
+   {
+      /* panic step reduction */
+      stepdn_();
+      *mgas1 = 1.0e-10;
+   }
+
+   if (pressa <= 1.0e-10)
+   {
+      /* panic step reduction */
+      stepdn_();
+      *press = 1.0e-10 - c[1];
+   }
+
+   if (*temp <= 1.0e-10)
+   {
+      /* panic step reduction */
+      stepdn_();
+      *temp = 1.0e-10;
+   }
+
+   /*** temperature & pressure variation ***/
+   dq = kth*sth*(extemp-*temp);
+
+   pn2vol_(dtemp, dpress, mgas1, temp, &pressa,
+           &sdm, &sdh, vol, &dvol, &dq, &gi);
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm1      /= 1.00000000000000e-003;
+   *dvol1    /= 1.66666666666667e-005;
+   *vol1     /= 1.00000000000000e-006;
+   *dm2      /= 1.00000000000000e-003;
+   *dvol2    /= 1.66666666666667e-005;
+   *vol2     /= 1.00000000000000e-006;
+   *dm3      /= 1.00000000000000e-003;
+   *dvol3    /= 1.66666666666667e-005;
+   *vol3     /= 1.00000000000000e-006;
+   *dm4      /= 1.00000000000000e-003;
+   *dvol4    /= 1.66666666666667e-005;
+   *vol4     /= 1.00000000000000e-006;
+   *vol      /= 1.00000000000000e-006;
+   *mgas1    /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNCH012.spe

@@ -0,0 +1,356 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="16.0.0 - 68387-65635 2017">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>33</SUB_ID_MAX>
+  <DEFAULT_ICON>pn_c1</DEFAULT_ICON>
+  <SUB_LABEL>variable volume pneumatic chamber with heat exchange (preferred)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>2</R_STORES_NUMBER>
+  <I_STORES_NUMBER>2</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>27</SUB_ID>
+    <TITLE>dead volume</TITLE>
+    <VARNAME>cvol0</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+00</DEF_VALUE>
+    <VALUE>1.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+005</MAX_VALUE>
+    <UNITS>L</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>28</SUB_ID>
+    <TITLE>thermal exchange coefficient</TITLE>
+    <VARNAME>kth</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>0.00000000000000e+00</DEF_VALUE>
+    <VALUE>0.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <UNITS>J/m**2/K/s</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>29</SUB_ID>
+    <TITLE>thermal exchange area</TITLE>
+    <VARNAME>sth</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e-01</DEF_VALUE>
+    <VALUE>1.00000000000000e-01</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+002</MAX_VALUE>
+    <UNITS>m**2</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>30</SUB_ID>
+    <TITLE>external temperature</TITLE>
+    <VARNAME>extemp</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>2.93150000000000e+02</DEF_VALUE>
+    <VALUE>2.93150000000000e+02</VALUE>
+    <MIN_VALUE>1.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+003</MAX_VALUE>
+    <UNITS>K</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>31</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>32</SUB_ID>
+    <TITLE>volume of pneumatic chamber</TITLE>
+    <VARNAME>vol</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>cm**3</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>33</SUB_ID>
+    <TITLE>mass of gas in chamber</TITLE>
+    <VARNAME>mgas1</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>g</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>1</SUB_ID>
+     <TITLE>temperature</TITLE>
+     <VARNAME>temp</VARNAME>
+     <VARNAME2>dtemp</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>K</UNITS>
+     <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+003</MAX_VALUE>
+     <DEF_VALUE>2.93150000000000e+002</DEF_VALUE>
+     <VALUE>2.93150000000000e+002</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>2</SUB_ID>
+     <TITLE>pressure</TITLE>
+     <VARNAME>press</VARNAME>
+     <VARNAME2>dpress</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>Pa</UNITS>
+     <MIN_VALUE>-1.01300000000000e+005</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+012</MAX_VALUE>
+     <DEF_VALUE>0.00000000000000e+000</DEF_VALUE>
+     <VALUE>0.00000000000000e+000</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>enthalpy flow rate at port 1</TITLE>
+     <VARNAME>dh1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>mass flow rate at port 1</TITLE>
+     <VARNAME>dm1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <TITLE>derivative of volume at port 1</TITLE>
+     <VARNAME>dvol1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>L/min</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <TITLE>volume at port 1</TITLE>
+     <VARNAME>vol1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>cm**3</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <VARNAME>temp2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>0</PRIMARY_VAR>
+     <DUP_TYPE>0</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <VARNAME>press2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>1</PRIMARY_VAR>
+     <DUP_TYPE>0</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>9</SUB_ID>
+     <TITLE>enthalpy flow rate at port 2</TITLE>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>10</SUB_ID>
+     <TITLE>mass flow rate at port 2</TITLE>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>11</SUB_ID>
+     <TITLE>derivative of volume at port 2</TITLE>
+     <VARNAME>dvol2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>L/min</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>12</SUB_ID>
+     <TITLE>volume at port 2</TITLE>
+     <VARNAME>vol2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>cm**3</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>13</SUB_ID>
+     <VARNAME>temp3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>0</PRIMARY_VAR>
+     <DUP_TYPE>0</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>14</SUB_ID>
+     <VARNAME>press3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>1</PRIMARY_VAR>
+     <DUP_TYPE>0</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>15</SUB_ID>
+     <TITLE>enthalpy flow rate at port 3</TITLE>
+     <VARNAME>dh3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>16</SUB_ID>
+     <TITLE>mass flow rate at port 3</TITLE>
+     <VARNAME>dm3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>17</SUB_ID>
+     <TITLE>derivative of volume at port 3</TITLE>
+     <VARNAME>dvol3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>L/min</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>18</SUB_ID>
+     <TITLE>volume at port 3</TITLE>
+     <VARNAME>vol3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>cm**3</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>19</SUB_ID>
+     <VARNAME>temp4</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>0</PRIMARY_VAR>
+     <DUP_TYPE>0</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>20</SUB_ID>
+     <VARNAME>press4</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>1</PRIMARY_VAR>
+     <DUP_TYPE>0</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>21</SUB_ID>
+     <TITLE>enthalpy flow rate at port 4</TITLE>
+     <VARNAME>dh4</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>22</SUB_ID>
+     <TITLE>mass flow rate at port 4</TITLE>
+     <VARNAME>dm4</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>23</SUB_ID>
+     <TITLE>derivative of volume at port 4</TITLE>
+     <VARNAME>dvol4</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>L/min</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>24</SUB_ID>
+     <TITLE>volume at port 4</TITLE>
+     <VARNAME>vol4</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>3</IO>
+     <UNITS>cm**3</UNITS>
+     <DEF_VALUE>0</DEF_VALUE>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/help/source/PNL0001.c

@@ -0,0 +1,348 @@
+/* Submodel PNL0001 skeleton created by AME Submodel editing utility
+   mer. juin 20 14:20:39 2018 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNL0001 (C-R)
+------------------------------------------------------------------------------
+DESCRIPTION :
+   PNL0001 is a submodel of a pneumatic pipe with only compressibility
+   and friction effects taking into account heat exchange. 
+              
+   The compressibility of the gas is taken into account by using a
+   simple polytropic model or a more complex one taking into account
+   heat exchange. 
+ 
+   The polytropic model is a simplified form of the general internal
+   energy model based on the first law of thermodynamics. The polytropic
+   approach is obtained by representing the thermal exchange phenomena
+   by a polytropic constant k. In that case, the temperature and
+   pressure are no more independent variables.
+ 
+   The reduction of the complexity of the model implies a lack of
+   accuracy. For general studies, you'd better use the heat exchange
+   approach.
+ 
+   Pipe friction is taken into account using a friction factor based on
+   the Reynolds number and the relative roughness.
+  
+   The temperature and pressure in the volume are state variables. 
+------------------------------------------------------------------------------
+USAGE :
+   Use this submodel to simulate a pneumatic pipe with compressibility
+   and friction effects, when the Mach number is low, ie gas velocity
+   < 0.3 * speed of sound .
+ 
+   The submodels PNGD001 or PNGD002 should be included in your circuit to
+   define the characteristics of the gas.
+------------------------------------------------------------------------------
+PARAMETER SETTINGS : 
+------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR : 
+   2002 FS from PNL01 SN.
+------------------------------------------------------------------------------
+REVISIONS :
+------------------------------------------------------------------------------
+LIST OF FUNCTIONS USED :
+   pn2getatp_()   : get atmospheric pressure
+   pn2ri_()       : get perfect gas constant
+   pn2vol1_()     : polytropic model for chambers
+   pn2vol_()      : heat exchange model for chambers
+   pn2pipefr_()   : frictional coeffitient in pneumatic pipes
+------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNL0001"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+#define TABFR      0 /* real store 0, 1 & 2 are used by pn2pipefr */
+#define PATM       3
+#define AREA       4
+#define VOL        5
+#define AREAEX     6
+
+#define SPL_FR   0
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 6 real parameters:
+
+   diam   diameter of pipe             [mm -> m]
+   le     pipe length                  [m]
+   rr     relative roughness           [null]
+   k      polytropic constant          [null]
+   kth    thermal exchange coefficient [J/m**2/K/s -> W/m**2/K]
+   extemp external temperature         [K]
+*/
+
+
+/* There are 2 integer parameters:
+
+   gi   gas type index
+   mode model         
+*/
+
+void pnl0001in_(int *n, double rp[6], int ip[2], double c[7]
+      , int ic[1], double *t2, double *p2)
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi, mode;
+   double diam, le, rr, k, kth, extemp;
+
+   gi         = ip[0];
+   mode       = ip[1];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   k          = rp[3];
+   kth        = rp[4];
+   extemp     = rp[5];
+   loop = 0;
+   error = 0;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..5]
+   *t2
+   *p2
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (*p2 < -GPATMOS)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial pressure at port 2 should be > 0 [barA].\n");
+   }
+
+   if (*t2 <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial temperature at port 2 should be > 0 [K].\n");
+   }
+
+   if (diam <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nDiameter of pipe should be > 0 [mm].\n");
+   }
+
+   if (le <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nPipe length should be > 0 [m].\n");
+   }
+
+   if (rr < 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nRelative roughness should be >= 0.\n");
+   }
+
+   if (mode == 1)
+   {
+      if (k <= 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nPolytropic constant should be > 0.\n");
+      }
+   }
+   else
+   {
+      if (kth < 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nThermal exchange coefficient should be >= 0 [J/m**2/K/s].\n");
+      }
+
+      if (extemp <= 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nExternal temperature should be > 0 [K].\n");
+      }
+   }
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+   if (mode < 1 || mode > 2)
+   {
+      amefprintf(stderr, "\nmodel must be in range [1..2].\n");
+      error = 2;
+   }
+
+   SUBMODEL_HANDLE_AND_RESET_ERROR(_SUBMODELNAME_, n, error)
+
+/* Common -> SI units conversions. */
+
+   rp[0]    *= 1.00000000000000e-003;
+   diam       = rp[0];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+
+   /* get atmospheric pressure */
+   c[PATM] = pn2getatp_();
+
+   /* Compute the cross-sectional area of pipe. */
+   c[AREA] =  M_PI * (diam) * (diam) / 4.0;
+
+   /* Compute volume of pipe. */
+   c[VOL] = c[AREA] * le;
+
+   /* Compute exchange area of pipe. */
+   c[AREAEX] = M_PI * diam * le;
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 2 ports.
+
+   Port 1 has 4 variables:
+
+      1 dh1     enthalpy flow rate at port 1 [J/s -> W]    basic variable output
+      2 dm1     mass flow rate at port 1     [g/s -> kg/s] basic variable output
+      3 t1      temperature at port 1        [K]           basic variable input
+      4 p1      pressure at port 1           [Pa]          basic variable input
+
+   Port 2 has 4 variables:
+
+      1 t2      temperature at port 2        [K]           explicit state (derivative `dt2')
+      2 p2      pressure at port 2           [Pa]          explicit state (derivative `dp2')
+      3 dh2     enthalpy flow rate at port 2 [J/s -> W]    basic variable input
+      4 dm2     mass flow rate at port 2     [g/s -> kg/s] basic variable input
+*/
+
+/*  There are 5 internal variables.
+
+      1 mgas     mass of gas in pipe      [g -> kg]         basic variable
+      2 re       Reynolds number          [null]            basic variable
+      3 cm       mass flow parameter (cm) [(kg*K/J)**(1/2)] basic variable
+      4 v        mean gas velocity        [m/s]             basic variable
+      5 ff       friction factor          [null]            basic variable
+*/
+
+void pnl0001_(int *n, double *dh1, double *dm1, double *t1, double *p1
+      , double *t2, double *dt2, double *p2, double *dp2, double *dh2
+      , double *dm2, double *mgas, double *re, double *cm, double *v
+      , double *ff, double rp[6], int ip[2], double c[7], int ic[1])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   static double zero = 0.0;
+   double sdh;
+   double dh2i, dm2i;
+   double dq;
+   double pa1, pa2, dmgas;
+   double r;
+   int dummyreg;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi, mode;
+   double diam, le, rr, k, kth, extemp;
+
+   gi         = ip[0];
+   mode       = ip[1];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   k          = rp[3];
+   kth        = rp[4];
+   extemp     = rp[5];
+   loop = 0;
+
+/* Common -> SI units conversions. */
+
+   *dm2      *= 1.00000000000000e-003;
+
+/*
+   Set all submodel outputs below:
+
+   *dh1        = ??;
+   *dm1        = ??;
+   *dt2        = ??;
+   *dp2        = ??;
+   *mgas       = ??;
+   *re         = ??;
+   *cm         = ??;
+   *v          = ??;
+   *ff         = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressures */
+   pa1 = *p1 + c[PATM];
+   pa2 = *p2 + c[PATM];
+
+   /* Compute flows through the pipe */
+   pn2pipefr_(&pa1, t1, &pa2, t2, &diam, &rr, &le, &c[AREA], re, v,ff,
+              dh1, dm1, &dh2i, &dm2i, cm, &c[TABFR], &gi, &ic[SPL_FR], &dummyreg);
+
+   /* Compute mass variation */
+   dmgas = (*dm2) + dm2i;
+
+   /* sum of enthalpy flows */
+   sdh = (*dh2) + dh2i;
+
+   /*** temperature & pressure variation ***/
+
+   if (mode == 1) /* Polytropic model. */
+   {
+      r = pn2ri_(&gi);
+      /* Compute initial mass of gas inside the pipe */
+      *mgas = (pa2) * c[VOL] / ((*t2) * r);
+
+      pn2vol1_(dt2, dp2, t2, &pa2,
+              &dmgas, mgas, &zero, &c[VOL], &k, &gi);
+   }
+   else  /* Heat exchange. */
+   {
+      dq = kth * c[AREAEX] * (extemp - *t2);
+
+      pn2vol_(dt2, dp2, mgas, t2, &pa2,
+              &dmgas, &sdh, &c[VOL], &zero, &dq, &gi);
+   }
+
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm1      /= 1.00000000000000e-003;
+   *dm2      /= 1.00000000000000e-003;
+   *mgas     /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNL0001.spe

@@ -0,0 +1,257 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="16.0.0 - 68387-65635 2017">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>22</SUB_ID_MAX>
+  <DEFAULT_ICON>p2port</DEFAULT_ICON>
+  <SUB_LABEL>Compressibility + friction submodel of pneumatic pipe (C-R)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>7</R_STORES_NUMBER>
+  <I_STORES_NUMBER>1</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>14</SUB_ID>
+    <TITLE>diameter of pipe</TITLE>
+    <VARNAME>diam</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+01</DEF_VALUE>
+    <VALUE>1.00000000000000e+01</VALUE>
+    <MIN_VALUE>1.00000000000000e-003</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+007</MAX_VALUE>
+    <UNITS>mm</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>15</SUB_ID>
+    <TITLE>pipe length</TITLE>
+    <VARNAME>le</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+00</DEF_VALUE>
+    <VALUE>1.00000000000000e+00</VALUE>
+    <MIN_VALUE>1.00000000000000e-006</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+004</MAX_VALUE>
+    <UNITS>m</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>16</SUB_ID>
+    <TITLE>relative roughness</TITLE>
+    <VARNAME>rr</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e-05</DEF_VALUE>
+    <VALUE>1.00000000000000e-05</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e-001</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>17</SUB_ID>
+    <TITLE>polytropic constant</TITLE>
+    <VARNAME>k</VARNAME>
+    <VISIBILITY>(mode == 1)</VISIBILITY>
+    <DEF_VALUE>1.35000000000000e+00</DEF_VALUE>
+    <VALUE>1.35000000000000e+00</VALUE>
+    <MIN_VALUE>5.00000000000000e-001</MIN_VALUE>
+    <MAX_VALUE>2.00000000000000e+000</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>18</SUB_ID>
+    <TITLE>thermal exchange coefficient</TITLE>
+    <VARNAME>kth</VARNAME>
+    <VISIBILITY>(mode == 2)</VISIBILITY>
+    <DEF_VALUE>0.00000000000000e+00</DEF_VALUE>
+    <VALUE>0.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <UNITS>J/m**2/K/s</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>19</SUB_ID>
+    <TITLE>external temperature</TITLE>
+    <VARNAME>extemp</VARNAME>
+    <VISIBILITY>(mode == 2)</VISIBILITY>
+    <DEF_VALUE>2.93150000000000e+02</DEF_VALUE>
+    <VALUE>2.93150000000000e+02</VALUE>
+    <MIN_VALUE>1.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+003</MAX_VALUE>
+    <UNITS>K</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>20</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+   <IPARAM>
+    <SUB_ID>21</SUB_ID>
+    <TITLE>model</TITLE>
+    <VARNAME>mode</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>2</DEF_VALUE>
+    <VALUE>2</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>2</MAX_VALUE>
+    <ENUM_LIST>
+     <ENUM>
+      <ENUM_STRING>polytropic</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>with thermal exchange</ENUM_STRING>
+     </ENUM>
+    </ENUM_LIST>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>22</SUB_ID>
+    <TITLE>mass of gas in pipe</TITLE>
+    <VARNAME>mgas</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>g</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>10</SUB_ID>
+    <TITLE>Reynolds number</TITLE>
+    <VARNAME>re</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>11</SUB_ID>
+    <TITLE>mass flow parameter (cm)</TITLE>
+    <VARNAME>cm</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>(kg*K/J)**(1/2)</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>12</SUB_ID>
+    <TITLE>mean gas velocity</TITLE>
+    <VARNAME>v</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>m/s</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>13</SUB_ID>
+    <TITLE>friction factor</TITLE>
+    <VARNAME>ff</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>1</SUB_ID>
+     <TITLE>enthalpy flow rate at port 1</TITLE>
+     <VARNAME>dh1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>2</SUB_ID>
+     <TITLE>mass flow rate at port 1</TITLE>
+     <VARNAME>dm1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>temperature at port 1</TITLE>
+     <VARNAME>t1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>pressure at port 1</TITLE>
+     <VARNAME>p1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <TITLE>temperature at port 2</TITLE>
+     <VARNAME>t2</VARNAME>
+     <VARNAME2>dt2</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>K</UNITS>
+     <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+004</MAX_VALUE>
+     <DEF_VALUE>2.93150000000000e+002</DEF_VALUE>
+     <VALUE>2.93150000000000e+002</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <TITLE>pressure at port 2</TITLE>
+     <VARNAME>p2</VARNAME>
+     <VARNAME2>dp2</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>Pa</UNITS>
+     <MIN_VALUE>-1.01300000000000e+005</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+012</MAX_VALUE>
+     <DEF_VALUE>0.00000000000000e+000</DEF_VALUE>
+     <VALUE>0.00000000000000e+000</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <TITLE>enthalpy flow rate at port 2</TITLE>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <TITLE>mass flow rate at port 2</TITLE>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/help/source/PNL0002.c

@@ -0,0 +1,368 @@
+/* Submodel PNL0002 skeleton created by AME Submodel editing utility
+   mer. juin 20 14:35:13 2018 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNL0002 (R-C-R)
+------------------------------------------------------------------------------
+DESCRIPTION :
+   PNL0002 is a submodel of a pneumatic pipe with only compressibility
+   and friction effects taking into account heat exchange. 
+ 
+   The compressibility of the gas is taken into account by using a
+   simple polytropic model or a more complex one taking into account
+   heat exchange. 
+ 
+   The polytropic model is a simplified form of the general internal
+   energy model based on the first law of thermodynamics. The polytropic
+   approach is obtained by representing the thermal exchange phenomena
+   by a polytropic constant k. In that case, the temperature and
+   pressure are no more independent variables.
+ 
+   The reduction of the complexity of the model implies a lack of
+   accuracy. For general studies, you'd better use the heat exchange
+   approach.
+ 
+   Pipe friction is taken into account using a friction factor based on
+   the Reynolds number and the relative roughness.
+ 
+   The temperature and pressure in the middle volume are state variables. 
+------------------------------------------------------------------------------
+USAGE :
+   Use this submodel to simulate a pneumatic pipe with compressibility
+   and friction effects, when the Mach number is low, ie gas velocity
+   < 0.3 * speed of sound .
+  
+   PNL0002 is basically similar to PNL0001 and PNL0003 differing only in the
+   input and output requirements.
+ 
+   The submodels PNGD01 or PNGD02 should be included in your circuit to
+   define the characteristics of the gas.
+------------------------------------------------------------------------------
+PARAMETER SETTINGS : 
+------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR : 
+  2002 FS from PNL02 SN.
+------------------------------------------------------------------------------
+REVISIONS :
+------------------------------------------------------------------------------
+LIST OF FUNCTIONS USED :
+   pn2getatp_()   : get atmospheric pressure
+   pn2ri_()       : get perfect gas constant
+   pn2vol1_()     : polytropic model for chambers  
+   pn2vol_()      : heat exchange model for chambers
+   pn2pipefr_()   : frictional coeffitient in pneumatic pipes
+------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNL0002"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+#define TABFR      0 /* real store 0, 1 & 2 are used by pn2pipefr */
+#define PATM       3
+#define AREA       4
+#define VOL        5
+#define HALFLE     6
+#define AREAEX     7
+
+
+#define SPL_FR   0
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 6 real parameters:
+
+   diam   diameter of pipe             [mm -> m]
+   le     pipe length                  [m]
+   rr     relative roughness           [null]
+   k      polytropic constant          [null]
+   kth    thermal exchange coefficient [J/m**2/K/s -> W/m**2/K]
+   extemp external temperature         [K]
+*/
+
+
+/* There are 2 integer parameters:
+
+   gi   gas type index
+   mode model         
+*/
+
+void pnl0002in_(int *n, double rp[6], int ip[2], double c[8]
+      , int ic[1], double *tctr, double *pctr)
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi, mode;
+   double diam, le, rr, k, kth, extemp;
+
+   gi         = ip[0];
+   mode       = ip[1];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   k          = rp[3];
+   kth        = rp[4];
+   extemp     = rp[5];
+   loop = 0;
+   error = 0;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..5]
+   *tctr
+   *pctr
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (*pctr < -GPATMOS)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial pressure at center of pipe should be > 0 [barA].\n");
+   }
+
+   if (*tctr <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial temperature at center of pipe should be > 0 [K].\n");
+   }
+
+   if (diam <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nDiameter of pipe should be > 0 [mm].\n");
+   }
+
+   if (le <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nPipe length should be > 0 [m].\n");
+   }
+
+   if (rr < 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nRelative roughness should be >= 0.\n");
+   }
+
+   if (mode == 1)
+   {
+      if (k <= 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nPolytropic constant should be > 0.\n");
+      }
+   }
+   else
+   {
+      if (kth < 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nThermal exchange coefficient should be >= 0 [J/m**2/K/s].\n");
+      }
+
+      if (extemp <= 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nExternal temperature should be > 0 [K].\n");
+      }
+   }
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+   if (mode < 1 || mode > 2)
+   {
+      amefprintf(stderr, "\nmodel must be in range [1..2].\n");
+      error = 2;
+   }
+
+   SUBMODEL_HANDLE_AND_RESET_ERROR(_SUBMODELNAME_, n, error)
+
+/* Common -> SI units conversions. */
+
+   rp[0]    *= 1.00000000000000e-003;
+   diam       = rp[0];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+
+   /* get atmospheric pressure */
+   c[PATM] = pn2getatp_();
+
+   /* Compute the cross-sectional area of pipe. */
+   c[AREA] = M_PI * (diam) * (diam) / 4.0;
+
+   /* Compute volume of pipe. */
+   c[VOL] = c[AREA] * le;
+
+   /* Divide the restriction in 2 identical restrictions */
+   c[HALFLE] = 0.5 * le;
+
+   /* Compute exchange area of pipe. */
+   c[AREAEX] = M_PI * diam * le;
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 2 ports.
+
+   Port 1 has 4 variables:
+
+      1 dh1     enthalpy flow rate at port 1 [J/s -> W]    basic variable output
+      2 dm1     mass flow rate at port 1     [g/s -> kg/s] basic variable output
+      3 t1      temperature at port 1        [K]           basic variable input
+      4 p1      pressure at port 1           [Pa]          basic variable input
+
+   Port 2 has 4 variables:
+
+      1 dh2     enthalpy flow rate at port 2 [J/s -> W]    basic variable output
+      2 dm2     mass flow rate at port 2     [g/s -> kg/s] basic variable output
+      3 t2      temperature at port 2        [K]           basic variable input
+      4 p2      pressure at port 2           [Pa]          basic variable input
+*/
+
+/*  There are 7 internal variables.
+
+      1 tctr     temperature at center of pipe [K]               explicit state (derivative `dtctr')
+      2 pctr     pressure at center of pipe    [Pa]              explicit state (derivative `dpctr')
+      3 mgas     mass of gas in pipe           [g -> kg]         basic variable
+      4 re       mean Reynolds number          [null]            basic variable
+      5 cm       mean mass flow parameter      [(kg*K/J)**(1/2)] basic variable
+      6 v        mean gas velocity             [m/s]             basic variable
+      7 ff       mean friction factor          [null]            basic variable
+*/
+
+void pnl0002_(int *n, double *dh1, double *dm1, double *t1, double *p1
+      , double *dh2, double *dm2, double *t2, double *p2, double *tctr
+      , double *dtctr, double *pctr, double *dpctr, double *mgas
+      , double *re, double *cm, double *v, double *ff, double rp[6]
+      , int ip[2], double c[8], int ic[1])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   static double zero = 0.0;
+   double sdh;
+   double dh1i, dm1i;
+   double dh2i, dm2i;
+   double ff1, ff2, re1, re2, cm1, cm2;
+   double dq;
+   double pa1, pa2, pactr;
+   double v1, v2;
+   double dmgas;
+   double r;
+   int dummyreg;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi, mode;
+   double diam, le, rr, k, kth, extemp;
+
+   gi         = ip[0];
+   mode       = ip[1];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   k          = rp[3];
+   kth        = rp[4];
+   extemp     = rp[5];
+   loop = 0;
+
+/*
+   Set all submodel outputs below:
+
+   *dh1        = ??;
+   *dm1        = ??;
+   *dh2        = ??;
+   *dm2        = ??;
+   *dtctr      = ??;
+   *dpctr      = ??;
+   *mgas       = ??;
+   *re         = ??;
+   *cm         = ??;
+   *v          = ??;
+   *ff         = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressure */
+   pa1   =   *p1 + c[PATM];
+   pa2   =   *p2 + c[PATM];
+   pactr = *pctr + c[PATM];
+
+   /* Compute flows through the pipe */
+   pn2pipefr_(&pa1, t1, &pactr, tctr, &diam, &rr, &c[HALFLE], &c[AREA], &re1, &v1, &ff1,
+              dh1, dm1, &dh1i, &dm1i, &cm1, &c[TABFR], &gi, &ic[SPL_FR], &dummyreg);
+
+   pn2pipefr_(&pactr, tctr, &pa2, t2, &diam, &rr, &c[HALFLE], &c[AREA], &re2, &v2, &ff2,
+              &dh2i, &dm2i, dh2, dm2, &cm2, &c[TABFR], &gi, &ic[SPL_FR], &dummyreg);
+
+   /* Mean variables */
+   *ff = 0.5 * (ff1 + ff2);
+   *re = 0.5 * (re1 + re2);
+   *cm = 0.5 * (cm1 + cm2);
+   *v  = 0.5 * (fabs(v1) + fabs(v2));
+
+   /* Compute mass variation */
+   dmgas = dm1i + dm2i;
+
+   /* sum of enthalpy flows */
+   sdh = dh1i + dh2i;
+
+   /*** temperature & pressure variation ***/
+   if (mode == 1) /* Polytropic model. */
+   {
+      r = pn2ri_(&gi);
+      *mgas = (pactr) * c[VOL] / ((*tctr) * r);
+
+      pn2vol1_(dtctr, dpctr, tctr, &pactr,
+               &dmgas, mgas, &zero, &c[VOL], &k, &gi);
+   }
+   else /* Heat exchange. */
+   {
+      dq = kth * c[AREAEX] * (extemp-*tctr);
+
+      pn2vol_(dtctr, dpctr, mgas, tctr, &pactr,
+              &dmgas, &sdh, &c[VOL], &zero, &dq, &gi);
+   }
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm1      /= 1.00000000000000e-003;
+   *dm2      /= 1.00000000000000e-003;
+   *mgas     /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNL0002.spe

@@ -0,0 +1,275 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="16.0.0 - 68387-65635 2017">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>24</SUB_ID_MAX>
+  <DEFAULT_ICON>p2port</DEFAULT_ICON>
+  <SUB_LABEL>Compressibility + friction submodel of pneumatic pipe (R-C-R)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>8</R_STORES_NUMBER>
+  <I_STORES_NUMBER>1</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>16</SUB_ID>
+    <TITLE>diameter of pipe</TITLE>
+    <VARNAME>diam</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+01</DEF_VALUE>
+    <VALUE>1.00000000000000e+01</VALUE>
+    <MIN_VALUE>1.00000000000000e-003</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+007</MAX_VALUE>
+    <UNITS>mm</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>17</SUB_ID>
+    <TITLE>pipe length</TITLE>
+    <VARNAME>le</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+00</DEF_VALUE>
+    <VALUE>1.00000000000000e+00</VALUE>
+    <MIN_VALUE>1.00000000000000e-006</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+004</MAX_VALUE>
+    <UNITS>m</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>18</SUB_ID>
+    <TITLE>relative roughness</TITLE>
+    <VARNAME>rr</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e-05</DEF_VALUE>
+    <VALUE>1.00000000000000e-05</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e-001</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>19</SUB_ID>
+    <TITLE>polytropic constant</TITLE>
+    <VARNAME>k</VARNAME>
+    <VISIBILITY>(mode == 1)</VISIBILITY>
+    <DEF_VALUE>1.35000000000000e+00</DEF_VALUE>
+    <VALUE>1.35000000000000e+00</VALUE>
+    <MIN_VALUE>5.00000000000000e-001</MIN_VALUE>
+    <MAX_VALUE>2.00000000000000e+000</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>20</SUB_ID>
+    <TITLE>thermal exchange coefficient</TITLE>
+    <VARNAME>kth</VARNAME>
+    <VISIBILITY>(mode == 2)</VISIBILITY>
+    <DEF_VALUE>0.00000000000000e+00</DEF_VALUE>
+    <VALUE>0.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <UNITS>J/m**2/K/s</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>21</SUB_ID>
+    <TITLE>external temperature</TITLE>
+    <VARNAME>extemp</VARNAME>
+    <VISIBILITY>(mode == 2)</VISIBILITY>
+    <DEF_VALUE>2.93150000000000e+02</DEF_VALUE>
+    <VALUE>2.93150000000000e+02</VALUE>
+    <MIN_VALUE>1.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+003</MAX_VALUE>
+    <UNITS>K</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>22</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+   <IPARAM>
+    <SUB_ID>23</SUB_ID>
+    <TITLE>model</TITLE>
+    <VARNAME>mode</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>2</DEF_VALUE>
+    <VALUE>2</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>2</MAX_VALUE>
+    <ENUM_LIST>
+     <ENUM>
+      <ENUM_STRING>polytropic</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>with thermal exchange</ENUM_STRING>
+     </ENUM>
+    </ENUM_LIST>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>9</SUB_ID>
+    <TITLE>temperature at center of pipe</TITLE>
+    <VARNAME>tctr</VARNAME>
+    <VARNAME2>dtctr</VARNAME2>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>1</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>K</UNITS>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <DEF_VALUE>2.931500e+02</DEF_VALUE>
+    <VALUE>2.931500e+02</VALUE>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>10</SUB_ID>
+    <TITLE>pressure at center of pipe</TITLE>
+    <VARNAME>pctr</VARNAME>
+    <VARNAME2>dpctr</VARNAME2>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>1</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>Pa</UNITS>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <DEF_VALUE>1.013000e+00</DEF_VALUE>
+    <VALUE>1.013000e+00</VALUE>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>24</SUB_ID>
+    <TITLE>mass of gas in pipe</TITLE>
+    <VARNAME>mgas</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>g</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>12</SUB_ID>
+    <TITLE>mean Reynolds number</TITLE>
+    <VARNAME>re</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>13</SUB_ID>
+    <TITLE>mean mass flow parameter</TITLE>
+    <VARNAME>cm</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>(kg*K/J)**(1/2)</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>14</SUB_ID>
+    <TITLE>mean gas velocity</TITLE>
+    <VARNAME>v</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>m/s</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>15</SUB_ID>
+    <TITLE>mean friction factor</TITLE>
+    <VARNAME>ff</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>1</SUB_ID>
+     <TITLE>enthalpy flow rate at port 1</TITLE>
+     <VARNAME>dh1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>2</SUB_ID>
+     <TITLE>mass flow rate at port 1</TITLE>
+     <VARNAME>dm1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>temperature at port 1</TITLE>
+     <VARNAME>t1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>pressure at port 1</TITLE>
+     <VARNAME>p1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <TITLE>enthalpy flow rate at port 2</TITLE>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <TITLE>mass flow rate at port 2</TITLE>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <TITLE>temperature at port 2</TITLE>
+     <VARNAME>t2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <TITLE>pressure at port 2</TITLE>
+     <VARNAME>p2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/help/source/PNL0003.c

@@ -0,0 +1,399 @@
+/* Submodel PNL0003 skeleton created by AME Submodel editing utility
+   mer. juin 20 14:17:28 2018 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNL0003 (C-R-C)
+------------------------------------------------------------------------------
+DESCRIPTION :
+   PNL0003 is a submodel of a pneumatic pipe with only compressibility
+   and friction effects taking into account heat exchange. 
+ 
+   The compressibility of the gas is taken into account by using a
+   simple polytropic model or a more complex one taking into account
+   heat exchange. 
+ 
+   The polytropic model is a simplified form of the general internal
+   energy model based on the first law of thermodynamics. The polytropic
+   approach is obtained by representing the thermal exchange phenomena
+   by a polytropic constant k. In that case, the temperature and
+   pressure are no more independent variables.
+ 
+   The reduction of the complexity of the model implies a lack of
+   accuracy. For general studies, you'd better use the heat exchange
+   approach.
+ 
+   Pipe friction is taken into account using a friction factor based on
+   the Reynolds number and the relative roughness.
+ 
+   The temperature and pressure in each two volumes are state variables. 
+------------------------------------------------------------------------------
+USAGE :
+   Use this submodel to simulate a pneumatic pipe with compressibility
+   and friction effects, when the Mach number is low, ie gas velocity
+   < 0.3 * speed of sound .
+  
+   PNL0003 is basically similar to PNL0001 and PNL0002 differing only in the
+   input and output requirements.
+ 
+   The submodels PNGD01 or PNGD02 should be included in your circuit to
+   define the characteristics of the gas.
+------------------------------------------------------------------------------
+PARAMETER SETTINGS : 
+------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR : 
+   2002 FS from PNL03 SN.
+------------------------------------------------------------------------------
+REVISIONS :
+------------------------------------------------------------------------------
+LIST OF FUNCTIONS USED :
+   pn2getatp_() :  get atmospheric pressure
+   pn2ri_()     :  get perfect gas constant
+   pn2vol1_()   :  polytropic model for chambers
+   pn2vol_()    :  heat exchange model for chambers
+   pn2pipefr_() :  frictional coefficient in pneumatic pipes
+------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNL0003"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+#define TABFR        0 /* real store 0, 1 & 2 are used by pn2pipefr */
+#define PATM         3
+#define AREA         4
+#define HALFVOL      5
+#define HALFAREAEX   6
+
+
+#define SPL_FR   0
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 6 real parameters:
+
+   diam   diameter of pipe             [mm -> m]
+   le     pipe length                  [m]
+   rr     relative roughness           [null]
+   k      polytropic constant          [null]
+   kth    thermal exchange coefficient [J/m**2/K/s -> W/m**2/K]
+   extemp external temperature         [K]
+*/
+
+
+/* There are 2 integer parameters:
+
+   gi   gas type index
+   mode model         
+*/
+
+void pnl0003in_(int *n, double rp[6], int ip[2], double c[7]
+      , int ic[1], double *t1, double *p1, double *t2, double *p2)
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+   double vol, areaex;
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi, mode;
+   double diam, le, rr, k, kth, extemp;
+
+   gi         = ip[0];
+   mode       = ip[1];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   k          = rp[3];
+   kth        = rp[4];
+   extemp     = rp[5];
+   loop = 0;
+   error = 0;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..5]
+   *t1
+   *p1
+   *t2
+   *p2
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (*p1 < -GPATMOS)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial pressure at port 1 should be > 0 [barA].\n");
+   }
+
+   if (*t1 <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial temperature at port 1 should be > 0 [K].\n");
+   }
+
+   if (*p2 < -GPATMOS)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial pressure at port 2 should be > 0 [barA].\n");
+   }
+
+   if (*t2 <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nInitial temperature at port 2 should be > 0 [K].\n");
+   }
+
+   if (diam <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nDiameter of pipe should be > 0 [mm].\n");
+   }
+
+   if (le <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nPipe length should be > 0 [m].\n");
+   }
+
+   if (rr < 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nRelative roughness should be >= 0.\n");
+   }
+
+   if (mode == 1)
+   {
+      if (k <= 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nPolytropic constant should be > 0.\n");
+      }
+   }
+   else
+   {
+      if (kth < 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nThermal exchange coefficient should be >= 0 [J/m**2/K/s].\n");
+      }
+
+      if (extemp <= 0.)
+      {
+         error = 2;
+         amefprintf(stderr, "\nExternal temperature should be > 0 [K].\n");
+      }
+   }
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+   if (mode < 1 || mode > 2)
+   {
+      amefprintf(stderr, "\nmodel must be in range [1..2].\n");
+      error = 2;
+   }
+
+   SUBMODEL_HANDLE_AND_RESET_ERROR(_SUBMODELNAME_, n, error)
+
+/* Common -> SI units conversions. */
+
+   rp[0]    *= 1.00000000000000e-003;
+   diam       = rp[0];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+   /* set atmospheric pressure */
+   c[PATM] = pn2getatp_();
+
+   /* Compute the cross-sectional area of pipe. */
+   c[AREA] = M_PI * (diam) * (diam) / 4.0;
+
+   /* Compute volume of pipe. */
+   vol = c[AREA] * le;
+
+   /* Divide the volume in 2 identical volumes */
+   c[HALFVOL] = 0.5 * vol;
+
+   /* Compute exchange area of pipe. */
+   areaex = M_PI * diam * le;
+
+   /* Divide the exchange area of pipe in 2 identical areas */
+   c[HALFAREAEX] = 0.5 * areaex;
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 2 ports.
+
+   Port 1 has 4 variables:
+
+      1 t1      temperature at port 1        [K]           explicit state (derivative `dt1')
+      2 p1      pressure at port 1           [Pa]          explicit state (derivative `dp1')
+      3 dh1     enthalpy flow rate at port 1 [J/s -> W]    basic variable input
+      4 dm1     mass flow rate at port 1     [g/s -> kg/s] basic variable input
+
+   Port 2 has 4 variables:
+
+      1 t2      temperature at port 2        [K]           explicit state (derivative `dt2')
+      2 p2      pressure at port 2           [Pa]          explicit state (derivative `dp2')
+      3 dh2     enthalpy flow rate at port 2 [J/s -> W]    basic variable input
+      4 dm2     mass flow rate at port 2     [g/s -> kg/s] basic variable input
+*/
+
+/*  There are 7 internal variables.
+
+      1 dhctr     enthalpy flow at center of pipe [J/s -> W]        basic variable
+      2 dmctr     mass flow at center of pipe     [g/s -> kg/s]     basic variable
+      3 mgas      mass of gas in pipe             [g -> kg]         basic variable
+      4 re        Reynolds number                 [null]            basic variable
+      5 cm        mass flow parameter (cm)        [(kg*K/J)**(1/2)] basic variable
+      6 v         mean gas velocity               [m/s]             basic variable
+      7 ff        friction factor                 [null]            basic variable
+*/
+
+void pnl0003_(int *n, double *t1, double *dt1, double *p1, double *dp1
+      , double *dh1, double *dm1, double *t2, double *dt2, double *p2
+      , double *dp2, double *dh2, double *dm2, double *dhctr
+      , double *dmctr, double *mgas, double *re, double *cm, double *v
+      , double *ff, double rp[6], int ip[2], double c[7], int ic[1])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   static double zero = 0.0;
+   double dh1i, dm1i;
+   double dh2i, dm2i;
+   double sdh1, sdm1;
+   double sdh2, sdm2;
+   double m1, m2;
+   double dq1, dq2;
+   double pa1, pa2;
+   double dmgas;
+   double r;
+   int dummyreg;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi, mode;
+   double diam, le, rr, k, kth, extemp;
+
+   gi         = ip[0];
+   mode       = ip[1];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   k          = rp[3];
+   kth        = rp[4];
+   extemp     = rp[5];
+   loop = 0;
+
+/* Common -> SI units conversions. */
+
+   *dm1      *= 1.00000000000000e-003;
+   *dm2      *= 1.00000000000000e-003;
+
+/*
+   Set all submodel outputs below:
+
+   *dt1        = ??;
+   *dp1        = ??;
+   *dt2        = ??;
+   *dp2        = ??;
+   *dhctr      = ??;
+   *dmctr      = ??;
+   *mgas       = ??;
+   *re         = ??;
+   *cm         = ??;
+   *v          = ??;
+   *ff         = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressures */
+   pa1 = *p1 + c[PATM];
+   pa2 = *p2 + c[PATM];
+
+   /* Compute flow through the pipe */
+   pn2pipefr_(&pa1, t1, &pa2, t2, &diam, &rr, &le, &c[AREA], re, v, ff,
+              &dh1i, &dm1i, &dh2i, &dm2i, cm, &c[TABFR], &gi, &ic[SPL_FR], &dummyreg);
+
+   /* Enthalpy flow and mass flow at center of pipe */
+   *dhctr = dh1i;     /* = -dh2i */
+   *dmctr = dm1i;     /* = -dm2i */
+
+   /* Compute the sum of the flows inside each volume */
+   sdm1 = *dm1 + dm1i;
+   sdh1 = *dh1 + dh1i;
+   sdm2 = *dm2 + dm2i;
+   sdh2 = *dh2 + dh2i;
+
+   dmgas = sdm1 + sdm2;
+
+   /*** temperature & pressure variation ***/
+   if (mode == 1) /* Polytropic model. */
+   {
+      r = pn2ri_(&gi);
+
+      /* Current mass in each volume */
+      m1 = pa1 * c[HALFVOL] / (*t1 * r);
+      m2 = pa2 * c[HALFVOL] / (*t2 * r);
+
+      pn2vol1_(dt1, dp1, t1, &pa1,
+               &sdm1, &m1, &zero, &c[HALFVOL], &k,&gi);
+
+      pn2vol1_(dt2, dp2, t2, &pa2,
+               &sdm2, &m2, &zero, &c[HALFVOL], &k,&gi);
+   }
+   else /* Heat exchange. */
+   {
+      dq1 = kth * c[HALFAREAEX] * (extemp - *t1);
+
+      pn2vol_(dt1, dp1, &m1, t1, &pa1,
+              &sdm1, &sdh1, &c[HALFVOL], &zero, &dq1, &gi);
+
+      dq2 = kth * c[HALFAREAEX] * (extemp - *t2);
+
+      pn2vol_(dt2, dp2, &m2, t2, &pa2,
+              &sdm2, &sdh2, &c[HALFVOL], &zero, &dq2, &gi);
+   }
+
+   *mgas = m1 + m2;
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm1      /= 1.00000000000000e-003;
+   *dm2      /= 1.00000000000000e-003;
+   *dmctr    /= 1.00000000000000e-003;
+   *mgas     /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNL0003.spe

@@ -0,0 +1,285 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="16.0.0 - 68387-65635 2017">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>24</SUB_ID_MAX>
+  <DEFAULT_ICON>p2port</DEFAULT_ICON>
+  <SUB_LABEL>Compressibility + friction submodel of pneumatic pipe (C-R-C)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>7</R_STORES_NUMBER>
+  <I_STORES_NUMBER>1</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>16</SUB_ID>
+    <TITLE>diameter of pipe</TITLE>
+    <VARNAME>diam</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+01</DEF_VALUE>
+    <VALUE>1.00000000000000e+01</VALUE>
+    <MIN_VALUE>1.00000000000000e-003</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+007</MAX_VALUE>
+    <UNITS>mm</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>17</SUB_ID>
+    <TITLE>pipe length</TITLE>
+    <VARNAME>le</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+00</DEF_VALUE>
+    <VALUE>1.00000000000000e+00</VALUE>
+    <MIN_VALUE>1.00000000000000e-006</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+004</MAX_VALUE>
+    <UNITS>m</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>18</SUB_ID>
+    <TITLE>relative roughness</TITLE>
+    <VARNAME>rr</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e-05</DEF_VALUE>
+    <VALUE>1.00000000000000e-05</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e-001</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>19</SUB_ID>
+    <TITLE>polytropic constant</TITLE>
+    <VARNAME>k</VARNAME>
+    <VISIBILITY>(mode == 1)</VISIBILITY>
+    <DEF_VALUE>1.35000000000000e+00</DEF_VALUE>
+    <VALUE>1.35000000000000e+00</VALUE>
+    <MIN_VALUE>5.00000000000000e-001</MIN_VALUE>
+    <MAX_VALUE>2.00000000000000e+000</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>20</SUB_ID>
+    <TITLE>thermal exchange coefficient</TITLE>
+    <VARNAME>kth</VARNAME>
+    <VISIBILITY>(mode == 2)</VISIBILITY>
+    <DEF_VALUE>0.00000000000000e+00</DEF_VALUE>
+    <VALUE>0.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <UNITS>J/m**2/K/s</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>21</SUB_ID>
+    <TITLE>external temperature</TITLE>
+    <VARNAME>extemp</VARNAME>
+    <VISIBILITY>(mode == 2)</VISIBILITY>
+    <DEF_VALUE>2.93150000000000e+02</DEF_VALUE>
+    <VALUE>2.93150000000000e+02</VALUE>
+    <MIN_VALUE>1.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+003</MAX_VALUE>
+    <UNITS>K</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>22</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+   <IPARAM>
+    <SUB_ID>23</SUB_ID>
+    <TITLE>model</TITLE>
+    <VARNAME>mode</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>2</DEF_VALUE>
+    <VALUE>2</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>2</MAX_VALUE>
+    <ENUM_LIST>
+     <ENUM>
+      <ENUM_STRING>polytropic</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>with thermal exchange</ENUM_STRING>
+     </ENUM>
+    </ENUM_LIST>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>9</SUB_ID>
+    <TITLE>enthalpy flow at center of pipe</TITLE>
+    <VARNAME>dhctr</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>J/s</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>10</SUB_ID>
+    <TITLE>mass flow at center of pipe</TITLE>
+    <VARNAME>dmctr</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>g/s</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>24</SUB_ID>
+    <TITLE>mass of gas in pipe</TITLE>
+    <VARNAME>mgas</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>g</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>12</SUB_ID>
+    <TITLE>Reynolds number</TITLE>
+    <VARNAME>re</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>13</SUB_ID>
+    <TITLE>mass flow parameter (cm)</TITLE>
+    <VARNAME>cm</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>(kg*K/J)**(1/2)</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>14</SUB_ID>
+    <TITLE>mean gas velocity</TITLE>
+    <VARNAME>v</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>m/s</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>15</SUB_ID>
+    <TITLE>friction factor</TITLE>
+    <VARNAME>ff</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>1</SUB_ID>
+     <TITLE>temperature at port 1</TITLE>
+     <VARNAME>t1</VARNAME>
+     <VARNAME2>dt1</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>K</UNITS>
+     <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+     <DEF_VALUE>2.93150000000000e+002</DEF_VALUE>
+     <VALUE>2.93150000000000e+002</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>2</SUB_ID>
+     <TITLE>pressure at port 1</TITLE>
+     <VARNAME>p1</VARNAME>
+     <VARNAME2>dp1</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>Pa</UNITS>
+     <MIN_VALUE>-1.01300000000000e+005</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+012</MAX_VALUE>
+     <DEF_VALUE>0.00000000000000e+000</DEF_VALUE>
+     <VALUE>0.00000000000000e+000</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>enthalpy flow rate at port 1</TITLE>
+     <VARNAME>dh1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>mass flow rate at port 1</TITLE>
+     <VARNAME>dm1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <TITLE>temperature at port 2</TITLE>
+     <VARNAME>t2</VARNAME>
+     <VARNAME2>dt2</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>K</UNITS>
+     <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+004</MAX_VALUE>
+     <DEF_VALUE>2.93150000000000e+002</DEF_VALUE>
+     <VALUE>2.93150000000000e+002</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <TITLE>pressure at port 2</TITLE>
+     <VARNAME>p2</VARNAME>
+     <VARNAME2>dp2</VARNAME2>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>1</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>Pa</UNITS>
+     <MIN_VALUE>-1.01300000000000e+005</MIN_VALUE>
+     <MAX_VALUE>1.00000000000000e+012</MAX_VALUE>
+     <DEF_VALUE>0.00000000000000e+000</DEF_VALUE>
+     <VALUE>0.00000000000000e+000</VALUE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <TITLE>enthalpy flow rate at port 2</TITLE>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <TITLE>mass flow rate at port 2</TITLE>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/help/source/PNL00R.c

@@ -0,0 +1,224 @@
+/* Submodel PNL00R skeleton created by AME Submodel editing utility
+   ven. 5. août 14:34:41 2016 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNL00R
+------------------------------------------------------------------------------
+DESCRIPTION :
+   PNL00R is a submodel of a pneumatic pipe with only friction effects.
+  
+   Pipe friction is taken into account using a friction factor based on
+   the Reynolds number and the relative roughness.
+------------------------------------------------------------------------------
+USAGE :
+   Use this submodel to simulate a pneumatic pipe with friction effects,
+   when the Mach number is low, ie gas velocity < 0.3 * speed of sound .
+   
+   The submodels PNGD001 or PNGD002 should be included in your circuit to
+   define the characteristics of the gas.
+------------------------------------------------------------------------------
+PARAMETER SETTINGS : 
+------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR : 
+  2002 FS from PNL0R SN
+------------------------------------------------------------------------------
+REVISIONS :
+------------------------------------------------------------------------------
+LIST OF FUNCTIONS USED :
+   pn2pipefr_()   : frictional coefficient in pneumatic pipes
+   pn2getatp_()   : get atmospheric pressure
+------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNL00R"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+#define TABFR      0 /* real store 0, 1 & 2 are used by pn2pipefr */
+#define PATM       3
+#define AREA       4
+
+
+#define SPL_FR  0
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 3 real parameters:
+
+   diam diameter of pipe   [mm -> m]
+   le   pipe length        [m]
+   rr   relative roughness [null]
+*/
+
+
+/* There is 1 integer parameter:
+
+   gi gas type index
+*/
+
+void pnl00rin_(int *n, double rp[3], int ip[1], double c[5], int ic[1])
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi;
+   double diam, le, rr;
+
+   gi         = ip[0];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   loop = 0;
+   error = 0;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..2]
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (diam <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nDiameter of pipe should be > 0 [mm].\n");
+   }
+
+   if (le <= 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nPipe length should be > 0 [m].\n");
+   }
+
+   if (rr < 0.0)
+   {
+      error = 2;
+      amefprintf(stderr, "\nRelative roughness should be >= 0.\n");
+   }
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+
+   SUBMODEL_HANDLE_AND_RESET_ERROR(_SUBMODELNAME_, n, error)
+
+/* Common -> SI units conversions. */
+
+   rp[0]    *= 1.00000000000000e-003;
+   diam       = rp[0];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+
+   c[PATM] = pn2getatp_();
+
+   /* Compute the cross-sectional area of pipe. */
+   c[AREA] =  M_PI * (diam) * (diam) / 4.0;
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 2 ports.
+
+   Port 1 has 4 variables:
+
+      1 dh1     duplicate of dh2             (sign reversed)
+      2 dm1     duplicate of dm2             (sign reversed)
+      3 t1      temperature at port 1        [K]  basic variable input
+      4 p1      pressure at port 1           [Pa] basic variable input
+
+   Port 2 has 4 variables:
+
+      1 dh2     enthalpy flow rate at port 2 [J/s -> W]    basic variable output
+      2 dm2     mass flow rate at port 2     [g/s -> kg/s] basic variable output
+      3 t2      temperature at port 2        [K]           basic variable input
+      4 p2      pressure at port 2           [Pa]          basic variable input
+*/
+
+/*  There are 4 internal variables.
+
+      1 re     Reynolds number          [null]            basic variable
+      2 cm     mass flow parameter (cm) [(kg*K/J)**(1/2)] basic variable
+      3 v      mean gas velocity        [m/s]             basic variable
+      4 ff     friction factor          [null]            basic variable
+*/
+
+void pnl00r_(int *n, double *t1, double *p1, double *dh2, double *dm2
+      , double *t2, double *p2, double *re, double *cm, double *v
+      , double *ff, double rp[3], int ip[1], double c[5], int ic[1])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   double pa1, pa2;
+   double dh1loc, dm1loc;
+   int dummyreg;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi;
+   double diam, le, rr;
+
+   gi         = ip[0];
+
+   diam       = rp[0];
+   le         = rp[1];
+   rr         = rp[2];
+   loop = 0;
+
+/*
+   Set all submodel outputs below:
+
+   *dh2        = ??;
+   *dm2        = ??;
+   *re         = ??;
+   *cm         = ??;
+   *v          = ??;
+   *ff         = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressure */
+   pa1 = *p1 + c[PATM];
+   pa2 = *p2 + c[PATM];
+
+   /* Compute flow through the pipe */
+
+   pn2pipefr_(&pa2, t2, &pa1, t1, &diam, &rr, &le, &c[AREA], re, v, ff,
+              dh2, dm2, &dh1loc, &dm1loc, cm, &c[TABFR], &gi, &ic[SPL_FR], &dummyreg);
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm2      /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNL00R.spe

@@ -0,0 +1,185 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="14.0.0 -  42489-40361 2015">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>18</SUB_ID_MAX>
+  <DEFAULT_ICON>p2port</DEFAULT_ICON>
+  <SUB_LABEL>Friction submodel of pneumatic pipe (R)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>5</R_STORES_NUMBER>
+  <I_STORES_NUMBER>1</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>13</SUB_ID>
+    <TITLE>diameter of pipe</TITLE>
+    <VARNAME>diam</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+01</DEF_VALUE>
+    <VALUE>1.00000000000000e+01</VALUE>
+    <MIN_VALUE>1.00000000000000e-003</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+007</MAX_VALUE>
+    <UNITS>mm</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>14</SUB_ID>
+    <TITLE>pipe length</TITLE>
+    <VARNAME>le</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e+00</DEF_VALUE>
+    <VALUE>1.00000000000000e+00</VALUE>
+    <MIN_VALUE>1.00000000000000e-006</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+004</MAX_VALUE>
+    <UNITS>m</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>15</SUB_ID>
+    <TITLE>relative roughness</TITLE>
+    <VARNAME>rr</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1.00000000000000e-05</DEF_VALUE>
+    <VALUE>1.00000000000000e-05</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e-001</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>16</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>9</SUB_ID>
+    <TITLE>Reynolds number</TITLE>
+    <VARNAME>re</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>10</SUB_ID>
+    <TITLE>mass flow parameter (cm)</TITLE>
+    <VARNAME>cm</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>(kg*K/J)**(1/2)</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>11</SUB_ID>
+    <TITLE>mean gas velocity</TITLE>
+    <VARNAME>v</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>m/s</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>12</SUB_ID>
+    <TITLE>friction factor</TITLE>
+    <VARNAME>ff</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>17</SUB_ID>
+     <VARNAME>dh1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>1</PRIMARY_PORT>
+     <PRIMARY_VAR>0</PRIMARY_VAR>
+     <DUP_TYPE>1</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>18</SUB_ID>
+     <VARNAME>dm1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>1</PRIMARY_PORT>
+     <PRIMARY_VAR>1</PRIMARY_VAR>
+     <DUP_TYPE>1</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>temperature at port 1</TITLE>
+     <VARNAME>t1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>pressure at port 1</TITLE>
+     <VARNAME>p1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <TITLE>enthalpy flow rate at port 2</TITLE>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <TITLE>mass flow rate at port 2</TITLE>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <TITLE>temperature at port 2</TITLE>
+     <VARNAME>t2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <TITLE>pressure at port 2</TITLE>
+     <VARNAME>p2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/help/source/PNOR001.c

@@ -0,0 +1,240 @@
+/* Submodel PNOR001 skeleton created by AME Submodel editing utility
+   lun. 10. juil. 17:22:57 2017 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNOR001
+------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR : 
+  2002 : Created by FS from PNOR01
+------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNOR001"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+
+/* real stores */
+#define PATM      0
+#define AREA      1
+#define CQ        2
+
+/* integer stores */
+#define DISC_ORIF    0
+
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 4 real parameters:
+
+   cq   flow coefficient (Cq) [null]
+   area orifice area          [mm**2 -> m**2]
+   Cv   flow coefficient (Cv) [null]
+   Kv   flow coefficient (Kv) [null]
+*/
+
+
+/* There are 2 integer parameters:
+
+   gi      gas type index          
+   flowset flow coefficient setting
+*/
+
+void pnor001in_(int *n, double rp[4], int ip[2], double c[3]
+      , int ic[1])
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi, flowset;
+   double cq, area, Cv, Kv;
+
+   gi         = ip[0];
+   flowset    = ip[1];
+
+   cq         = rp[0];
+   area       = rp[1];
+   Cv         = rp[2];
+   Kv         = rp[3];
+   loop = 0;
+   error = 0;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..3]
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (flowset == 1)
+   {
+      if (area < 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nOrifice area should be positive.\n");
+      }
+
+      if (cq <= 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nFlow coefficient should be strictly positive.\n");
+      }
+   }
+   else if (flowset == 2)
+   {
+      if (Cv < 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nFlow coefficient (Cv) should be positive (value is %g).\n", Cv);
+      }
+   }
+   else
+   {
+      if (Kv < 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nFlow coefficient (Kv) should be positive (value is %g).\n", Kv);
+      }
+   }
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+   if (flowset < 1 || flowset > 3)
+   {
+      amefprintf(stderr, "\nflow coefficient setting must be in range [1..3].\n");
+      error = 2;
+   }
+
+   SUBMODEL_HANDLE_AND_RESET_ERROR(_SUBMODELNAME_, n, error)
+
+/* Common -> SI units conversions. */
+
+   rp[1]    *= 1.00000000000000e-006;
+   area       = rp[1];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+
+   /* get atmospheric pressure */
+   c[PATM] = pn2getatp_();
+
+   if (flowset == 1)
+   {
+      c[CQ] = cq;
+      c[AREA] = area;
+   }
+   else
+   {
+      /* calculation of equivalent area with Cv or Kv.
+         Default value of cq; the same value will be used in pn2rcqfix. */
+      c[CQ] = 0.72;
+
+      if (flowset == 2)   /* Cv */
+         orif_areafromcv_(&Cv, &c[CQ], &c[AREA]);
+      else
+         orif_areafromkv_(&Kv, &c[CQ], &c[AREA]);
+   }
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 2 ports.
+
+   Port 1 has 4 variables:
+
+      1 dh1        enthalpy flow rate at port 1 [J/s -> W]    basic variable output
+      2 dm1        mass flow rate at port 1     [g/s -> kg/s] basic variable output
+      3 temp1      temperature at port 1        [K]           basic variable input
+      4 press1     pressure at port 1           [Pa]          basic variable input
+
+   Port 2 has 4 variables:
+
+      1 dh2        duplicate of dh1             (sign reversed)
+      2 dm2        duplicate of dm1             (sign reversed)
+      3 temp2      temperature at port 2        [K]  basic variable input
+      4 press2     pressure at port 2           [Pa] basic variable input
+*/
+
+/*  There are 2 internal variables.
+
+      1 cm         mass flow parameter (cm)    [(kg*K/J)**(1/2)] basic variable
+      2 gasvel     vena contracta gas velocity [m/s]             basic variable
+*/
+
+void pnor001_(int *n, double *dh1, double *dm1, double *temp1
+      , double *press1, double *temp2, double *press2, double *cm
+      , double *gasvel, double rp[4], int ip[2], double c[3]
+      , int ic[1])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   double pressa1, pressa2;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi, flowset;
+   double cq, area, Cv, Kv;
+
+   gi         = ip[0];
+   flowset    = ip[1];
+
+   cq         = rp[0];
+   area       = rp[1];
+   Cv         = rp[2];
+   Kv         = rp[3];
+   loop = 0;
+
+/*
+   Set all submodel outputs below:
+
+   *dh1        = ??;
+   *dm1        = ??;
+   *cm         = ??;
+   *gasvel     = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressures */
+   pressa1 = *press1 + c[PATM];
+   pressa2 = *press2 + c[PATM];
+
+   /* calculation of the flows */
+   pn2rcqfix_( dh1, dm1, temp1, &pressa1, temp2, &pressa2, &c[AREA], &c[CQ], &gi,
+               cm, gasvel, &ic[DISC_ORIF]);
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm1      /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNOR001.spe

@@ -0,0 +1,199 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="14.0.0 -  42489-40361 2015">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>18</SUB_ID_MAX>
+  <DEFAULT_ICON>pn_orifice</DEFAULT_ICON>
+  <SUB_LABEL>pneumatic orifice (constant flow coefficient)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>3</R_STORES_NUMBER>
+  <I_STORES_NUMBER>1</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>12</SUB_ID>
+    <TITLE>flow coefficient (Cq)</TITLE>
+    <VARNAME>cq</VARNAME>
+    <VISIBILITY>flowset==1</VISIBILITY>
+    <DEF_VALUE>7.20000000000000e-01</DEF_VALUE>
+    <VALUE>7.20000000000000e-01</VALUE>
+    <MIN_VALUE>1.00000000000000e-010</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+000</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>11</SUB_ID>
+    <TITLE>orifice area</TITLE>
+    <VARNAME>area</VARNAME>
+    <VISIBILITY>flowset==1</VISIBILITY>
+    <DEF_VALUE>5.00000000000000e+00</DEF_VALUE>
+    <VALUE>5.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <UNITS>mm**2</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>17</SUB_ID>
+    <TITLE>flow coefficient (Cv)</TITLE>
+    <VARNAME>Cv</VARNAME>
+    <VISIBILITY>flowset==2</VISIBILITY>
+    <DEF_VALUE>5.00000000000000e-01</DEF_VALUE>
+    <VALUE>5.00000000000000e-01</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+030</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>18</SUB_ID>
+    <TITLE>flow coefficient (Kv)</TITLE>
+    <VARNAME>Kv</VARNAME>
+    <VISIBILITY>flowset==3</VISIBILITY>
+    <DEF_VALUE>4.00000000000000e-01</DEF_VALUE>
+    <VALUE>4.00000000000000e-01</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+030</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>13</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+   <IPARAM>
+    <SUB_ID>14</SUB_ID>
+    <TITLE>flow coefficient setting</TITLE>
+    <VARNAME>flowset</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>3</MAX_VALUE>
+    <ENUM_LIST>
+     <ENUM>
+      <ENUM_STRING>Cq</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>Cv</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>Kv</ENUM_STRING>
+     </ENUM>
+    </ENUM_LIST>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>9</SUB_ID>
+    <TITLE>mass flow parameter (cm)</TITLE>
+    <VARNAME>cm</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>(kg*K/J)**(1/2)</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>10</SUB_ID>
+    <TITLE>vena contracta gas velocity</TITLE>
+    <VARNAME>gasvel</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>m/s</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>1</SUB_ID>
+     <TITLE>enthalpy flow rate at port 1</TITLE>
+     <VARNAME>dh1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>2</SUB_ID>
+     <TITLE>mass flow rate at port 1</TITLE>
+     <VARNAME>dm1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>temperature at port 1</TITLE>
+     <VARNAME>temp1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>pressure at port 1</TITLE>
+     <VARNAME>press1</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>0</PRIMARY_VAR>
+     <DUP_TYPE>1</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>0</PRIMARY_PORT>
+     <PRIMARY_VAR>1</PRIMARY_VAR>
+     <DUP_TYPE>1</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <TITLE>temperature at port 2</TITLE>
+     <VARNAME>temp2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <TITLE>pressure at port 2</TITLE>
+     <VARNAME>press2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/help/source/PNVO001.c

@@ -0,0 +1,254 @@
+/* Submodel PNVO001 skeleton created by AME Submodel editing utility
+   ven. 6. oct. 11:10:58 2017 */
+
+
+
+#include <math.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include "ameutils.h"
+/* *******************************************************************************
+TITLE : PNVO001
+------------------------------------------------------------------------------
+DATE OF CREATION / AUTHOR : 
+   2002 : Created by FS from PNVO01
+------------------------------------------------------------------------------
+SOURCE :
+
+   This material contains trade secrets or otherwise confidential
+   information owned by Siemens Industry Software Inc. or its
+   affiliates (collectively, "Siemens"), or its licensors. Access to
+   and use of this information is strictly limited as set forth in the
+   Customer's applicable agreements with Siemens.
+   
+   Unpublished work. Copyright 2023 Siemens
+
+******************************************************************************* */
+
+#define _SUBMODELNAME_ "PNVO001"
+
+/* >>>>>>>>>>>>Insert Private Code Here. */
+
+/* real stores */
+#define PATM      0
+#define AREAMAX   1
+#define CQ        2
+
+/* integer stores */
+#define DISC_LIMIT   0
+#define DISC_ORIF    1
+
+/* <<<<<<<<<<<<End of Private Code. */
+
+
+/* There are 4 real parameters:
+
+   cq    flow coefficient (Cq)           [null]
+   area0 orifice area at maximum opening [mm**2 -> m**2]
+   Cv    maximum flow coefficient (Cv)   [null]
+   Kv    maximum flow coefficient (Kv)   [null]
+*/
+
+
+/* There are 2 integer parameters:
+
+   gi      gas type index          
+   flowset flow coefficient setting
+*/
+
+void pnvo001in_(int *n, double rp[4], int ip[2], double c[3]
+      , int ic[2])
+
+{
+   int loop, error;
+/* >>>>>>>>>>>>Extra Initialization Function Declarations Here. */
+/* <<<<<<<<<<<<End of Extra Initialization declarations. */
+   int gi, flowset;
+   double cq, area0, Cv, Kv;
+
+   gi         = ip[0];
+   flowset    = ip[1];
+
+   cq         = rp[0];
+   area0      = rp[1];
+   Cv         = rp[2];
+   Kv         = rp[3];
+   loop = 0;
+   error = 0;
+
+/*
+   If necessary, check values of the following:
+
+   rp[0..3]
+*/
+
+
+/* >>>>>>>>>>>>Initialization Function Check Statements. */
+
+   pn2_valid_gas_(&gi, &error);
+
+   if (flowset == 1)
+   {
+      if (area0 < 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nOrifice area at maximum opening should be positive.\n");
+      }
+
+      if (cq <= 0.0 )
+      {
+         error = 2;
+         amefprintf(stderr, "\nFlow coefficient should be strictly positive.\n");
+      }
+   }
+   else if (flowset == 2)
+   {
+      if (Cv < 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nMaximum flow coefficient (Cv) should be positive (value is %g).\n", Cv);
+      }
+   }
+   else
+   {
+      if (Kv < 0.0)
+      {
+         error = 2;
+         amefprintf(stderr, "\nMaximum flow coefficient (Kv) should be positive (value is %g).\n", Kv);
+      }
+   }
+
+/* <<<<<<<<<<<<End of Initialization Check Statements. */
+
+/*   Integer parameter checking:   */
+
+   if (gi < 1 || gi > 99)
+   {
+      amefprintf(stderr, "\ngas type index must be in range [1..99].\n");
+      error = 2;
+   }
+   if (flowset < 1 || flowset > 3)
+   {
+      amefprintf(stderr, "\nflow coefficient setting must be in range [1..3].\n");
+      error = 2;
+   }
+
+   SUBMODEL_HANDLE_AND_RESET_ERROR(_SUBMODELNAME_, n, error)
+
+/* Common -> SI units conversions. */
+
+   rp[1]    *= 1.00000000000000e-006;
+   area0      = rp[1];
+
+
+/* >>>>>>>>>>>>Initialization Function Executable Statements. */
+
+   /* get atmospheric pressure */
+   c[PATM] = pn2getatp_();
+
+   if (flowset == 1)
+   {
+      c[CQ] = cq;
+      c[AREAMAX] = area0;
+   }
+   else
+   {
+      /* calculation of equivalent maximal area with Cv or Kv.
+         Default value of cq; the same value will be used in pn2rcqfix. */
+      c[CQ] = 0.72;
+
+      if (flowset == 2)   /* Cv */
+         orif_areafromcv_(&Cv, &c[CQ], &c[AREAMAX]);
+      else
+         orif_areafromkv_(&Kv, &c[CQ], &c[AREAMAX]);
+   }
+
+/* <<<<<<<<<<<<End of Initialization Executable Statements. */
+}
+
+/*  There are 3 ports.
+
+   Port 1 has 1 variable:
+
+      1 res     input signal [null] basic variable input
+
+   Port 2 has 4 variables:
+
+      1 dh2        enthalpy flow rate at port 2 [J/s -> W]    basic variable output
+      2 dm2        mass flow rate at port 2     [g/s -> kg/s] basic variable output
+      3 temp2      temperature at port 2        [K]           basic variable input
+      4 press2     pressure at port 2           [Pa]          basic variable input
+
+   Port 3 has 4 variables:
+
+      1 dh3        duplicate of dh2             (sign reversed)
+      2 dm3        duplicate of dm2             (sign reversed)
+      3 temp3      temperature at port 3        [K]  basic variable input
+      4 press3     pressure at port 3           [Pa] basic variable input
+*/
+
+/*  There are 3 internal variables.
+
+      1 xv         fractional opening          [null]            basic variable
+      2 cm         mass flow parameter (cm)    [(kg*K/J)**(1/2)] basic variable
+      3 gasvel     vena contracta gas velocity [m/s]             basic variable
+*/
+
+void pnvo001_(int *n, double *res, double *dh2, double *dm2
+      , double *temp2, double *press2, double *temp3, double *press3
+      , double *xv, double *cm, double *gasvel, double rp[4]
+      , int ip[2], double c[3], int ic[2])
+
+{
+   int loop;
+/* >>>>>>>>>>>>Extra Calculation Function Declarations Here. */
+   double marea;   /* modulated area */
+   double pressa2, pressa3;
+   static double zero = 0.0, one = 1.0;
+/* <<<<<<<<<<<<End of Extra Calculation declarations. */
+   int gi, flowset;
+   double cq, area0, Cv, Kv;
+
+   gi         = ip[0];
+   flowset    = ip[1];
+
+   cq         = rp[0];
+   area0      = rp[1];
+   Cv         = rp[2];
+   Kv         = rp[3];
+   loop = 0;
+
+/*
+   Set all submodel outputs below:
+
+   *dh2        = ??;
+   *dm2        = ??;
+   *xv         = ??;
+   *cm         = ??;
+   *gasvel     = ??;
+*/
+
+
+
+/* >>>>>>>>>>>>Calculation Function Executable Statements. */
+
+   /* set absolute pressure */
+   pressa2 = *press2 + c[PATM];
+   pressa3 = *press3 + c[PATM];
+
+   *xv = dlimit_(res, &zero, &one, &ic[DISC_LIMIT]);
+
+   /* limitation of the modulated area */
+   marea = *xv * c[AREAMAX];
+
+   /*** calculation of the flows ***/
+   pn2rcqfix_( dh2, dm2, temp2, &pressa2, temp3, &pressa3, &marea, &c[CQ], &gi,
+               cm, gasvel, &ic[DISC_ORIF] );
+
+/* <<<<<<<<<<<<End of Calculation Executable Statements. */
+
+/* SI -> Common units conversions. */
+
+   *dm2      /= 1.00000000000000e-003;
+}
+

AmesimModels/help/source/PNVO001.spe

@@ -0,0 +1,220 @@
+<?xml version="1.0" encoding="ISO-8859-1"?>
+<!DOCTYPE SPE>
+<SPE DOC_VERSION="2" AME_VERSION="14.0.0 -  42489-40361 2015">
+
+ <SUBMODEL>
+  <SUB_TYPE>0</SUB_TYPE>
+  <SUB_ID_MAX>20</SUB_ID_MAX>
+  <DEFAULT_ICON>pn_morifice</DEFAULT_ICON>
+  <SUB_LABEL>modulated pneumatic orifice (constant flow coefficient)</SUB_LABEL>
+  <SUB_UNIT>0</SUB_UNIT>
+  <R_STORES_NUMBER>3</R_STORES_NUMBER>
+  <I_STORES_NUMBER>2</I_STORES_NUMBER>
+  <OUTPUT_TYPE>1</OUTPUT_TYPE>
+  <RPARAMS_LIST>
+   <RPARAM>
+    <SUB_ID>12</SUB_ID>
+    <TITLE>flow coefficient (Cq)</TITLE>
+    <VARNAME>cq</VARNAME>
+    <VISIBILITY>flowset==1</VISIBILITY>
+    <DEF_VALUE>7.20000000000000e-01</DEF_VALUE>
+    <VALUE>7.20000000000000e-01</VALUE>
+    <MIN_VALUE>1.00000000000000e-010</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+000</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>13</SUB_ID>
+    <TITLE>orifice area at maximum opening</TITLE>
+    <VARNAME>area0</VARNAME>
+    <VISIBILITY>flowset==1</VISIBILITY>
+    <DEF_VALUE>5.00000000000000e+00</DEF_VALUE>
+    <VALUE>5.00000000000000e+00</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+006</MAX_VALUE>
+    <UNITS>mm**2</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>18</SUB_ID>
+    <TITLE>maximum flow coefficient (Cv)</TITLE>
+    <VARNAME>Cv</VARNAME>
+    <VISIBILITY>flowset==2</VISIBILITY>
+    <DEF_VALUE>5.00000000000000e-01</DEF_VALUE>
+    <VALUE>5.00000000000000e-01</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+030</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+   <RPARAM>
+    <SUB_ID>19</SUB_ID>
+    <TITLE>maximum flow coefficient (Kv)</TITLE>
+    <VARNAME>Kv</VARNAME>
+    <VISIBILITY>flowset==3</VISIBILITY>
+    <DEF_VALUE>4.00000000000000e-01</DEF_VALUE>
+    <VALUE>4.00000000000000e-01</VALUE>
+    <MIN_VALUE>0.00000000000000e+000</MIN_VALUE>
+    <MAX_VALUE>1.00000000000000e+030</MAX_VALUE>
+    <UNITS>null</UNITS>
+   </RPARAM>
+  </RPARAMS_LIST>
+  <IPARAMS_LIST>
+   <IPARAM>
+    <SUB_ID>14</SUB_ID>
+    <TITLE>gas type index</TITLE>
+    <VARNAME>gi</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>99</MAX_VALUE>
+   </IPARAM>
+   <IPARAM>
+    <SUB_ID>15</SUB_ID>
+    <TITLE>flow coefficient setting</TITLE>
+    <VARNAME>flowset</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <DEF_VALUE>1</DEF_VALUE>
+    <VALUE>1</VALUE>
+    <MIN_VALUE>1</MIN_VALUE>
+    <MAX_VALUE>3</MAX_VALUE>
+    <ENUM_LIST>
+     <ENUM>
+      <ENUM_STRING>Cq</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>Cv</ENUM_STRING>
+     </ENUM>
+     <ENUM>
+      <ENUM_STRING>Kv</ENUM_STRING>
+     </ENUM>
+    </ENUM_LIST>
+   </IPARAM>
+  </IPARAMS_LIST>
+  <IVARS_LIST>
+   <IVAR>
+    <SUB_ID>20</SUB_ID>
+    <TITLE>fractional opening</TITLE>
+    <VARNAME>xv</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>null</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>10</SUB_ID>
+    <TITLE>mass flow parameter (cm)</TITLE>
+    <VARNAME>cm</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>(kg*K/J)**(1/2)</UNITS>
+   </IVAR>
+   <IVAR>
+    <SUB_ID>11</SUB_ID>
+    <TITLE>vena contracta gas velocity</TITLE>
+    <VARNAME>gasvel</VARNAME>
+    <VISIBILITY>True</VISIBILITY>
+    <TYPE>0</TYPE>
+    <DIMENSION>1</DIMENSION>
+    <UNITS>m/s</UNITS>
+   </IVAR>
+  </IVARS_LIST>
+  <EVARS_LIST>
+   <PORT>
+    <EVAR>
+     <SUB_ID>1</SUB_ID>
+     <TITLE>input signal</TITLE>
+     <VARNAME>res</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>null</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>2</SUB_ID>
+     <TITLE>enthalpy flow rate at port 2</TITLE>
+     <VARNAME>dh2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>J/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>3</SUB_ID>
+     <TITLE>mass flow rate at port 2</TITLE>
+     <VARNAME>dm2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>2</IO>
+     <UNITS>g/s</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>4</SUB_ID>
+     <TITLE>temperature at port 2</TITLE>
+     <VARNAME>temp2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>5</SUB_ID>
+     <TITLE>pressure at port 2</TITLE>
+     <VARNAME>press2</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+   <PORT>
+    <EVAR>
+     <SUB_ID>6</SUB_ID>
+     <VARNAME>dh3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>1</PRIMARY_PORT>
+     <PRIMARY_VAR>0</PRIMARY_VAR>
+     <DUP_TYPE>1</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>7</SUB_ID>
+     <VARNAME>dm3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>4</TYPE>
+     <PRIMARY_PORT>1</PRIMARY_PORT>
+     <PRIMARY_VAR>1</PRIMARY_VAR>
+     <DUP_TYPE>1</DUP_TYPE>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>8</SUB_ID>
+     <TITLE>temperature at port 3</TITLE>
+     <VARNAME>temp3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>K</UNITS>
+    </EVAR>
+    <EVAR>
+     <SUB_ID>9</SUB_ID>
+     <TITLE>pressure at port 3</TITLE>
+     <VARNAME>press3</VARNAME>
+     <VISIBILITY>True</VISIBILITY>
+     <TYPE>0</TYPE>
+     <DIMENSION>1</DIMENSION>
+     <IO>1</IO>
+     <UNITS>Pa</UNITS>
+    </EVAR>
+   </PORT>
+  </EVARS_LIST>
+  <SUBIDS_RESET>0</SUBIDS_RESET>
+ </SUBMODEL>
+</SPE>

AmesimModels/test_mql/README.md

@@ -0,0 +1,140 @@
+# test_mql
+
+本目录记录 AMESim 模型 `test_mql.ame` 向 `app.simulation` 迁移时使用的源模型信息、结果对齐约定和当前进度。
+
+## 目标
+
+迁移目标不是复制 AMESim `.results` 中的观测值，而是建立真实的 Python 仿真链路：
+
+`组件方程 -> SimulationNetwork/系统装配 -> closure -> snapshot/端口写回 -> RHS -> solver -> reporting/comparison`
+
+Python 输出只有通过 AMESim baseline 对比后才能作为数值一致性依据。duplicate、反号或派生观测可以用于验证端口方向，但不能替代组件方程和网络闭合。
+
+## 模型与源数据
+
+- AMESim 源模型：`AmesimModels/test_mql.ame`
+- Python 系统类：`app.simulation.examples.test_mql.system.TestMqlSystem`
+- 结构运行入口：`app.simulation.examples.test_mql.run`
+- 132 状态比较入口：`app.simulation.examples.test_mql.run_full_state_comparison`
+- AMESim 组件数：117
+- LINE 连接数：84
+- 连续状态数：132
+- 离散状态数：24
+- 全局参数：`D1=20`、`D2=20`、`D3=14`、`P0=153`、`Pdq=1`、`V=15`、`cf=0.45`
+
+`.ame` 文件是 tar 包，迁移和校验主要使用其中的：
+
+- `test_mql_.cir`：组件、连接、参数表达式和生成代码线索。
+- `test_mql_.param` / `test_mql_.data`：参数和结果配套数据。
+- `test_mql_.modelinfo` / `test_mql_.sim`：状态数和仿真设置。
+- `test_mql_.var` / `test_mql_.results`：AMESim `Data_Path` 目录和 baseline 时序。
+
+当前结果解析器可读取 1002 个时间点和 1116 个保存变量，无需先转换成 CSV。
+
+## 当前实现
+
+当前已经完成：
+
+- AMESim 组件、LINE 连接、直接组件接触、全局参数和变量目录解析。
+- 氦气 Peng-Robinson 物性；内部使用绝对压力，AMESim `press` 按相对 `101300 Pa` 的表压输出。
+- `PNCH023 / PNCH012 / PNOR001 / PNVO001` 气动组件。
+- `PNL0001 / PNL0002 / PNL0003 / PNL00R` 管路动态或阻性关系。
+- `PN3NODE2 / P4NODE2` 代数节点、真实邻接拓扑、canonical flow 和端口写回。
+- `PNRP17 / MECMAS21 / LSTP00A / LMECHN1 / UD00 / FORC` 当前工况可确认的机械行为。
+- 112 个气动状态和 20 个机械状态组成的 132 状态总闭包。
+- 活塞运动学、变容气室机械反馈、气动力、外力、端止动和质量约束耦合。
+- 关键 `Data_Path` 序列导出、schema validation、AMESim 插值 comparison、误差排序、端点诊断和变容气室 RHS 拆解。
+
+主要实现位置：
+
+- `app/simulation/examples/test_mql/system.py`
+- `app/simulation/examples/test_mql/closure.py`
+- `app/simulation/examples/test_mql/pneumatic.py`
+- `app/simulation/examples/test_mql/mechanical.py`
+- `app/simulation/examples/test_mql/lines.py`
+- `app/simulation/examples/test_mql/primitives/`
+- `app/simulation/examples/test_mql/structural_network.py`
+- `app/simulation/reporting/amesim_results.py`
+- `app/simulation/reporting/test_mql_comparison.py`
+- `app/simulation/examples/test_mql/run_full_state_comparison.py`
+
+## 当前对比结果
+
+默认 comparison 已从区间内插值的 `t=1e-5 s` 改为与 AMESim
+首个保存时刻精确对齐的 `t=0.01 s`，当前比较 13 个关键信号，并
+新增 `xv@pn_morifice_1`、`dm2@pn_morifice_1` 的结构化 PNVO 诊断。
+
+事件前 `t=0.01 s` 对比：
+
+- `press@pn_c1_8`：Python `-1286.601221 Pa`，AMESim
+  `-1288.253185 Pa`，绝对误差约 `1.651964 Pa`。
+- `dm1@pneumatic_69`：Python `-0.002485112 g/s`，AMESim
+  `-0.002054255 g/s`；换算后的 canonical 流量绝对误差约
+  `4.30857e-7 kg/s`。
+- `xv@pn_morifice_1` 和 `dm2@pn_morifice_1` 在两侧均为 0，确认
+  STEP0 事件前 PNVO 保持关闭。
+- `vol1@pn_brp2_8` 绝对误差约 `8.76e-5`，机械位移、速度和加速度
+  仍保持较小误差；当前较明显的累计差异集中在 PNL0001 流量和
+  PNCH012 压力/能量链路。
+
+新增 `--pnvo-event-boundary` 诊断：先积分到 `0.04 s` 的左极限，
+再按 STEP0 的右连续语义在事件时刻读取开度和流量。结果为：
+
+- `xv@pn_morifice_1`：Python/AMESim 均为 `1`。
+- `dm2@pn_morifice_1`：Python `502.945005 g/s`，AMESim
+  `497.823823 g/s`，绝对误差约 `5.121182 g/s`，相对约 `1.03%`。
+- `press@pn_c1_8` 绝对误差约 `55.4815 Pa`；
+  `dm1@pneumatic_69` 绝对误差约 `0.00281880 g/s`。
+
+这说明 PNVO 开启瞬间的开度语义和主流量量级已经对齐，但事件前
+累积压力/支路流量仍有偏差。常规积分直接跨越事件到 `0.05 s` 时，
+当前进程会被系统终止，尚未形成可信的事件后结果；不能据此声明
+完整 `0.04 -> 0.05 s` 窗口已经可运行。
+
+## 下一步
+
+1. 优先定位 `0 -> 0.04 s` 累积的 `pneumatic_69` 流量与
+   `pn_c1_8` 压力偏差，区分 PNL0001 阻力和 PNCH012 能量方程。
+2. 采用显式事件分段或针对事件后的局部数值策略，解决跨越
+   `t=0.04 s` 后积分进程被终止的问题，再验证 `t=0.05 s` 保存点。
+3. 保留 `press@pn_c1_8`、`dm1@pneumatic_69`、PNVO `xv/dm2`
+   和 chamber RHS breakdown 作为同一条诊断链。
+4. 在完整开启窗口稳定后，再判断是否需要校准 PNVO 流量系数。
+
+`pn_c1_8` 的直接主线是 `pneumatic_69`；`pneumatic_96`
+属于另一条固定气室支路，不是该诊断对象。
+
+## 运行与验证
+
+运行默认短时域 comparison：
+
+```bash
+python3 -m app.simulation.examples.test_mql.run_full_state_comparison
+```
+
+运行 PNVO 事件边界诊断：
+
+```bash
+python3 -m app.simulation.examples.test_mql.run_full_state_comparison --pnvo-event-boundary
+```
+
+运行相关测试：
+
+```bash
+python3 -m unittest tests.test_run_test_mql_full_state_comparison tests.test_test_mql_pnl0001_segment
+```
+
+运行全量测试：
+
+```bash
+python3 -m unittest discover -s tests -t .
+```
+
+## 对齐约定
+
+- 组件 alias 和输出名优先保持 AMESim 原名及 `Data_Path`。
+- `PortState.m_flow > 0` 表示流入当前组件。
+- closure 先定义 canonical flow，再按各组件端口方向写回 `m_flow`。
+- AMESim 管路质量流量通常以 `g/s` 保存，Python 内部统一使用 `kg/s`。
+- CSV 是人工检查和交换格式，不是读取 AMESim baseline 的前置条件。
+- 未完成真实 Python 输出对比前，不使用“与 AMESim 完全一致”之类结论。

PythonModels/.gitignore

@@ -1,2 +0,0 @@
-__pycache__/
-*.pyc

PythonModels/__init__.py

@@ -1,2 +0,0 @@
-"""Python port scaffold for the Modelica-based pressurization system."""
-

PythonModels/components/cylinder.py

@@ -1,55 +0,0 @@
-from __future__ import annotations
-
-from PythonModels.core.base import DynamicComponent
-from PythonModels.core.medium import IdealGasMedium, ThermodynamicProperties
-from PythonModels.core.ports import PortState
-from PythonModels.core.state import VolumeState
-
-
-class Cylinder(DynamicComponent):
-    """Python port of ModelicaModels.Mycylinder."""
-
-    def __init__(
-        self,
-        name: str,
-        medium: IdealGasMedium,
-        V: float = 0.01,
-        p0: float = 35e6,
-        T0: float = 300.0,
-    ) -> None:
-        super().__init__(name=name)
-        self.medium = medium
-        self.V = V
-        m0 = p0 * V / (medium.R_gas * T0)
-        U0 = m0 * medium.specific_internal_energy(T0)
-        self.state = VolumeState(m=m0, U=U0)
-        self.port_b = PortState()
-
-    def get_state_vector(self) -> list[float]:
-        return self.state.as_vector()
-
-    def set_state_vector(self, values: list[float]) -> None:
-        self.state = VolumeState.from_vector(values)
-
-    def properties(self) -> ThermodynamicProperties:
-        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
-        self.port_b.p = props.p
-        self.port_b.h_outflow = props.h
-        return props
-
-    def derivatives_from_connection(
-        self,
-        *,
-        connected_h: float,
-        port_m_flow: float,
-        internal_h: float,
-    ) -> VolumeState:
-        inlet_h = self.connection_inlet_enthalpy(
-            port_m_flow=port_m_flow,
-            connected_h=connected_h,
-            internal_h=internal_h,
-        )
-        return self.derivatives(inlet_h, port_m_flow)
-
-    def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
-        return VolumeState(m=m_flow, U=m_flow * inlet_h)

PythonModels/components/orifice.py

@@ -1,28 +0,0 @@
-from __future__ import annotations
-
-from math import sqrt
-
-from PythonModels.core.base import AlgebraicComponent
-from PythonModels.core.ports import PortState
-
-
-class Orifice(AlgebraicComponent):
-    """Python port of ModelicaModels.Myorifice."""
-
-    def __init__(self, name: str, opening: float = 1.0, K: float = 1e-7) -> None:
-        super().__init__(name=name)
-        self.opening = opening
-        self.K = K
-        self.port_a = PortState()
-        self.port_b = PortState()
-
-    @property
-    def K_eff(self) -> float:
-        return self.K * max(self.opening, 0.001)
-
-    def mass_flow(self, p_a: float, p_b: float) -> float:
-        dp = p_a - p_b
-        if dp == 0.0:
-            return 0.0
-        return self.K_eff * sqrt(abs(dp)) * (1.0 if dp > 0.0 else -1.0)
-

PythonModels/components/pipe.py

@@ -1,133 +0,0 @@
-from __future__ import annotations
-
-from PythonModels.core.base import DynamicComponent
-from PythonModels.core.medium import IdealGasMedium, ThermodynamicProperties
-from PythonModels.core.ports import PortState
-from PythonModels.core.state import VolumeState
-
-
-class Pipe(DynamicComponent):
-    """Python port of ModelicaModels.Mypipe."""
-
-    def __init__(
-        self,
-        name: str,
-        medium: IdealGasMedium,
-        L: float = 5.0,
-        D: float = 0.02,
-        lambda_darcy: float = 0.02,
-        p0: float = 1e5,
-        T0: float = 300.0,
-    ) -> None:
-        super().__init__(name=name)
-        self.medium = medium
-        self.L = L
-        self.D = D
-        self.lambda_darcy = lambda_darcy
-        self.area = 3.141592653589793 * D * D / 4.0
-        self.V = self.area * L
-        m0 = p0 * self.V / (medium.R_gas * T0)
-        U0 = m0 * medium.specific_internal_energy(T0)
-        self.state = VolumeState(m=m0, U=U0)
-        self.port_a = PortState()
-        self.port_b = PortState()
-
-    def get_state_vector(self) -> list[float]:
-        return self.state.as_vector()
-
-    def set_state_vector(self, values: list[float]) -> None:
-        self.state = VolumeState.from_vector(values)
-
-    def properties(self) -> ThermodynamicProperties:
-        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
-        self.port_b.p = props.p
-        self.port_a.h_outflow = props.h
-        self.port_b.h_outflow = props.h
-        return props
-
-    def inlet_pressure(self, m_flow_a: float, rho: float, core_pressure: float) -> float:
-        resistance = self.lambda_darcy * (self.L / self.D)
-        dynamic_term = m_flow_a * abs(m_flow_a) / (2.0 * rho * self.area * self.area)
-        return core_pressure + resistance * dynamic_term
-
-    def port_a_inlet_enthalpy(
-        self,
-        *,
-        port_a_m_flow: float,
-        connected_h: float,
-        internal_h: float,
-    ) -> float:
-        return self.connection_inlet_enthalpy(
-            port_m_flow=port_a_m_flow,
-            connected_h=connected_h,
-            internal_h=internal_h,
-        )
-
-    def port_b_inlet_enthalpy(
-        self,
-        *,
-        port_b_m_flow: float,
-        connected_h: float,
-        internal_h: float,
-    ) -> float:
-        return self.connection_inlet_enthalpy(
-            port_m_flow=port_b_m_flow,
-            connected_h=connected_h,
-            internal_h=internal_h,
-        )
-
-    def connection_inlet_enthalpies(
-        self,
-        *,
-        port_a_m_flow: float,
-        connected_h_a: float,
-        port_b_m_flow: float,
-        connected_h_b: float,
-        internal_h: float,
-    ) -> tuple[float, float]:
-        return (
-            self.port_a_inlet_enthalpy(
-                port_a_m_flow=port_a_m_flow,
-                connected_h=connected_h_a,
-                internal_h=internal_h,
-            ),
-            self.port_b_inlet_enthalpy(
-                port_b_m_flow=port_b_m_flow,
-                connected_h=connected_h_b,
-                internal_h=internal_h,
-            ),
-        )
-
-    def derivatives_from_connections(
-        self,
-        *,
-        port_a_m_flow: float,
-        connected_h_a: float,
-        port_b_m_flow: float,
-        connected_h_b: float,
-        internal_h: float,
-    ) -> VolumeState:
-        inlet_h_a, inlet_h_b = self.connection_inlet_enthalpies(
-            port_a_m_flow=port_a_m_flow,
-            connected_h_a=connected_h_a,
-            port_b_m_flow=port_b_m_flow,
-            connected_h_b=connected_h_b,
-            internal_h=internal_h,
-        )
-        return self.derivatives(
-            inlet_h_a=inlet_h_a,
-            inlet_h_b=inlet_h_b,
-            m_flow_a=port_a_m_flow,
-            m_flow_b=port_b_m_flow,
-        )
-
-    def derivatives(
-        self,
-        inlet_h_a: float,
-        inlet_h_b: float,
-        m_flow_a: float,
-        m_flow_b: float,
-    ) -> VolumeState:
-        dm_dt = m_flow_a + m_flow_b
-        dU_dt = m_flow_a * inlet_h_a + m_flow_b * inlet_h_b
-        return VolumeState(m=dm_dt, U=dU_dt)

PythonModels/components/tank.py

@@ -1,55 +0,0 @@
-from __future__ import annotations
-
-from PythonModels.core.base import DynamicComponent
-from PythonModels.core.medium import IdealGasMedium, ThermodynamicProperties
-from PythonModels.core.ports import PortState
-from PythonModels.core.state import VolumeState
-
-
-class Tank(DynamicComponent):
-    """Python port of ModelicaModels.Mytank."""
-
-    def __init__(
-        self,
-        name: str,
-        medium: IdealGasMedium,
-        V: float = 0.1,
-        p0: float = 1e5,
-        T0: float = 300.0,
-    ) -> None:
-        super().__init__(name=name)
-        self.medium = medium
-        self.V = V
-        m0 = p0 * V / (medium.R_gas * T0)
-        U0 = m0 * medium.specific_internal_energy(T0)
-        self.state = VolumeState(m=m0, U=U0)
-        self.port_a = PortState()
-
-    def get_state_vector(self) -> list[float]:
-        return self.state.as_vector()
-
-    def set_state_vector(self, values: list[float]) -> None:
-        self.state = VolumeState.from_vector(values)
-
-    def properties(self) -> ThermodynamicProperties:
-        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
-        self.port_a.p = props.p
-        self.port_a.h_outflow = props.h
-        return props
-
-    def derivatives_from_connection(
-        self,
-        *,
-        connected_h: float,
-        port_m_flow: float,
-        internal_h: float,
-    ) -> VolumeState:
-        inlet_h = self.connection_inlet_enthalpy(
-            port_m_flow=port_m_flow,
-            connected_h=connected_h,
-            internal_h=internal_h,
-        )
-        return self.derivatives(inlet_h, port_m_flow)
-
-    def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
-        return VolumeState(m=m_flow, U=m_flow * inlet_h)

PythonModels/core/base.py

@@ -1,48 +0,0 @@
-from __future__ import annotations
-
-from abc import ABC, abstractmethod
-
-
-class Component(ABC):
-    def __init__(self, name: str) -> None:
-        self.name = name
-
-
-class DynamicComponent(Component):
-    state_size = 2
-
-    @staticmethod
-    def actual_stream_enthalpy(
-        port_m_flow: float,
-        connected_h: float,
-        internal_h: float,
-    ) -> float:
-        """Approximate `actualStream(port.h_outflow)` for a mixed control volume port."""
-
-        return connected_h if port_m_flow > 0.0 else internal_h
-
-    def connection_inlet_enthalpy(
-        self,
-        port_m_flow: float,
-        connected_h: float,
-        internal_h: float,
-    ) -> float:
-        """Resolve the enthalpy convected into this control volume through one port."""
-
-        return self.actual_stream_enthalpy(
-            port_m_flow=port_m_flow,
-            connected_h=connected_h,
-            internal_h=internal_h,
-        )
-
-    @abstractmethod
-    def get_state_vector(self) -> list[float]:
-        raise NotImplementedError
-
-    @abstractmethod
-    def set_state_vector(self, values: list[float]) -> None:
-        raise NotImplementedError
-
-
-class AlgebraicComponent(Component):
-    """Stateless element described by algebraic constraints only."""

PythonModels/core/medium.py

@@ -1,96 +0,0 @@
-from __future__ import annotations
-
-from dataclasses import dataclass
-
-
-@dataclass(frozen=True)
-class ThermodynamicProperties:
-    p: float
-    T: float
-    rho: float
-    u: float
-    h: float
-
-
-@dataclass(frozen=True)
-class IdealGasMedium:
-    """Temperature-dependent ideal-gas air approximation.
-
-    This is still not a strict clone of `Modelica.Media.Air.SimpleAir`.
-    The small linear `cp(T)` term is kept configurable for calibration, but the
-    current default is calibrated against the committed Testmodel baseline and
-    therefore falls back to the constant-heat-capacity limit.
-    """
-
-    name: str = "SimpleAirApprox"
-    R_gas: float = 287.0
-    cp_ref: float = 1005.0
-    T_ref: float = 300.0
-    cp_slope: float = 0.0
-
-    @property
-    def cv(self) -> float:
-        return self.cv_at_temperature(self.T_ref)
-
-    @property
-    def gamma(self) -> float:
-        return self.cp_at_temperature(self.T_ref) / self.cv
-
-    def cp_at_temperature(self, T: float) -> float:
-        return self.cp_ref + self.cp_slope * (T - self.T_ref)
-
-    def cv_at_temperature(self, T: float) -> float:
-        return self.cp_at_temperature(T) - self.R_gas
-
-    def density(self, p: float, T: float) -> float:
-        return p / (self.R_gas * T)
-
-    def specific_internal_energy(self, T: float) -> float:
-        delta_T = T - self.T_ref
-        return (
-            self.cv * self.T_ref
-            + self.cv * delta_T
-            + 0.5 * self.cp_slope * delta_T * delta_T
-        )
-
-    def specific_enthalpy(self, T: float) -> float:
-        delta_T = T - self.T_ref
-        return (
-            self.cp_ref * self.T_ref
-            + self.cp_ref * delta_T
-            + 0.5 * self.cp_slope * delta_T * delta_T
-        )
-
-    def temperature_from_internal_energy(self, u: float) -> float:
-        reference_internal_energy = self.cv * self.T_ref
-        delta_u = u - reference_internal_energy
-
-        if abs(self.cp_slope) <= 1e-15:
-            return self.T_ref + delta_u / self.cv
-
-        a = 0.5 * self.cp_slope
-        b = self.cv
-        c = -delta_u
-        discriminant = max(b * b - 4.0 * a * c, 0.0)
-        positive_root = (-b + discriminant**0.5) / (2.0 * a)
-        negative_root = (-b - discriminant**0.5) / (2.0 * a)
-        delta_T = positive_root if abs(positive_root) <= abs(negative_root) else negative_root
-        return self.T_ref + delta_T
-
-    def temperature_from_mass_internal_energy(self, m: float, U: float) -> float:
-        if m <= 0.0:
-            raise ValueError("Mass must stay positive when recovering temperature.")
-        return self.temperature_from_internal_energy(U / m)
-
-    def pressure(self, m: float, T: float, V: float) -> float:
-        if V <= 0.0:
-            raise ValueError("Volume must stay positive.")
-        return m * self.R_gas * T / V
-
-    def properties_from_mU(self, m: float, U: float, V: float) -> ThermodynamicProperties:
-        T = self.temperature_from_mass_internal_energy(m, U)
-        p = self.pressure(m, T, V)
-        rho = m / V
-        u = U / m
-        h = self.specific_enthalpy(T)
-        return ThermodynamicProperties(p=p, T=T, rho=rho, u=u, h=h)

PythonModels/core/ports.py

@@ -1,13 +0,0 @@
-from __future__ import annotations
-
-from dataclasses import dataclass
-
-
-@dataclass
-class PortState:
-    """Python-side analogue of a Modelica fluid port."""
-
-    p: float = 0.0
-    m_flow: float = 0.0
-    h_outflow: float = 0.0
-

PythonModels/core/solver.py

@@ -1,102 +0,0 @@
-from __future__ import annotations
-
-from dataclasses import dataclass
-from typing import Callable
-
-
-@dataclass(frozen=True)
-class SolveIVPConfig:
-    t_start: float = 0.0
-    t_stop: float = 20.0
-    method: str = "BDF"
-    rtol: float = 1e-6
-    atol: float = 1e-8
-    max_step: float = 1e-3
-
-
-@dataclass(frozen=True)
-class ODESolution:
-    t: list[float]
-    y: list[list[float]]
-    success: bool
-    message: str
-
-
-def _vector_add(a: list[float], b: list[float], scale: float = 1.0) -> list[float]:
-    return [x + scale * y for x, y in zip(a, b)]
-
-
-def _runge_kutta_4(
-    rhs: Callable[[float, list[float]], list[float]],
-    initial_state: list[float],
-    config: SolveIVPConfig,
-    t_eval: list[float] | None,
-) -> ODESolution:
-    if t_eval is None:
-        point_count = max(
-            2,
-            int((config.t_stop - config.t_start) / max(config.max_step, 1e-6)) + 1,
-        )
-        step = (config.t_stop - config.t_start) / (point_count - 1)
-        t_eval = [config.t_start + index * step for index in range(point_count)]
-
-    state = list(initial_state)
-    states = [[value] for value in state]
-    times = [float(t_eval[0])]
-    current_time = float(t_eval[0])
-
-    for target_time in t_eval[1:]:
-        while current_time < target_time - 1e-15:
-            dt = min(config.max_step, target_time - current_time)
-            k1 = rhs(current_time, state)
-            k2 = rhs(current_time + 0.5 * dt, _vector_add(state, k1, 0.5 * dt))
-            k3 = rhs(current_time + 0.5 * dt, _vector_add(state, k2, 0.5 * dt))
-            k4 = rhs(current_time + dt, _vector_add(state, k3, dt))
-            state = [
-                value + (dt / 6.0) * (a + 2.0 * b + 2.0 * c + d)
-                for value, a, b, c, d in zip(state, k1, k2, k3, k4)
-            ]
-            current_time += dt
-
-        times.append(float(target_time))
-        for index, value in enumerate(state):
-            states[index].append(value)
-
-    return ODESolution(
-        t=times,
-        y=states,
-        success=True,
-        message="Integrated with built-in RK4 fallback because SciPy is unavailable.",
-    )
-
-
-def integrate_ode(
-    rhs: Callable[[float, list[float]], list[float]],
-    initial_state: list[float],
-    config: SolveIVPConfig,
-    t_eval: list[float] | None = None,
-):
-    """Thin wrapper around scipy.integrate.solve_ivp with a pure-Python fallback."""
-
-    if abs(config.t_stop - config.t_start) <= 1e-15:
-        return ODESolution(
-            t=[float(config.t_start)],
-            y=[[value] for value in initial_state],
-            success=True,
-            message="Skipped integration because t_start equals t_stop.",
-        )
-
-    try:
-        from scipy.integrate import solve_ivp
-    except ImportError:
-        return _runge_kutta_4(rhs, initial_state, config, t_eval)
-
-    return solve_ivp(
-        fun=rhs,
-        t_span=(config.t_start, config.t_stop),
-        y0=initial_state,
-        method=config.method,
-        rtol=config.rtol,
-        atol=config.atol,
-        t_eval=t_eval,
-    )

README.md

@@ -1,2 +1,114 @@
 # SystemSimulationApp
 
+ReactFlow 系统建模与 `app.simulation` 仿真后端。
+
+## 开发环境准备
+
+后端统一使用 Python 3.12；仓库根目录的 `.python-version` 记录本轮参考补丁版本
+`3.12.3`。`requirements.txt` 保留支持范围，
+`constraints/python312-direct.txt` 固定跨平台开发环境的直接依赖参考版本；
+`constraints/python312-linux-x86_64.lock` 则完整固定发布与 CI 所用的 Linux x86_64
+wheel、全部传递依赖及其 SHA-256。
+
+Windows：
+
+```powershell
+py -3.12 -m venv .venv-win
+.\.venv-win\Scripts\python.exe -m pip install `
+  -r requirements.txt `
+  -c constraints/python312-direct.txt
+.\.venv-win\Scripts\python.exe -m pip check
+```
+
+Linux：
+
+```bash
+python3.12 -m venv .venv
+./.venv/bin/python -m pip install \
+  -r constraints/python312-linux-x86_64.lock
+./.venv/bin/python -m pip check
+```
+
+Linux 发布锁仅适用于兼容 manylinux_2_28 的 Linux x86_64 和 CPython 3.12。它启用
+`--only-binary=:all:` 与 `--require-hashes`，因此不会静默改用源码包或未审计 wheel；
+CI 和正式性能复测必须直接以 `-r` 安装该文件。Windows 或其他平台的开发环境继续
+使用 `requirements.txt` 加 `constraints/python312-direct.txt`。若要测试
+`requirements.txt` 声明的兼容范围，可显式省略约束，但这类结果不应与锁定环境的
+性能数据直接比较。
+
+升级参考版本时，应在干净的 Python 3.12 Linux x86_64 虚拟环境中解析范围文件，
+仅下载兼容 wheel，逐个记录 wheel 的 SHA-256，再从空环境安装发布锁并运行
+`pip check`、依赖契约测试与后端测试。不能只复制 `pip freeze`，因为它既不证明
+依赖来源，也不校验安装产物。
+
+前端使用 Vite 8，需要 Node.js `20.19+` 或 `22.12+`。首次启动前安装前端依赖。
+
+Windows（PowerShell，使用仓库内的便携 Node.js）：
+
+```powershell
+$nodeDir = Get-ChildItem .tools -Directory -Filter "node-*-win-x64" |
+  Where-Object { (Test-Path "$($_.FullName)\node.exe") -and (Test-Path "$($_.FullName)\npm.cmd") } |
+  Select-Object -First 1
+& "$($nodeDir.FullName)\npm.cmd" --prefix frontend ci
+```
+
+Linux：
+
+```bash
+cd frontend
+npm ci
+cd ..
+```
+
+Windows 启动脚本会自动使用 `.tools/node-*-win-x64` 下兼容的便携 Node.js；Linux 启动脚本优先使用 `.tools/node-*-linux-x64` 下兼容的运行时（如果存在），否则使用 `PATH` 中的 `node` 和 `npm`。`start-all.sh` 需要 Bash 4.3 或更高版本。
+
+## 启动项目
+
+脚本统一存放在 `bat/` 目录。三个入口分别用于同时启动、只启动后端、只启动前端。
+
+Windows：
+
+```bat
+bat\start-all.bat
+bat\start-backend.bat
+bat\start-reactflow.bat
+```
+
+Linux：
+
+```bash
+./bat/start-all.sh
+./bat/start-backend.sh
+./bat/start-reactflow.sh
+```
+
+后端地址为 `http://127.0.0.1:8000`，前端地址为 `http://127.0.0.1:5173`。Windows 的 `start-all.bat` 会分别打开两个命令行窗口；Linux 的 `start-all.sh` 会在同一终端管理两个进程，按 `Ctrl+C` 会同时停止它们。
+
+## 后端接口
+
+- `GET /api/components/catalog`：返回组件库与模型版本、分类、图标键、端口布局和参数契约，供 ReactFlow 启动时自动加载。
+- `POST /api/reactflow/system-xml`：导出精简的 System XML v3。
+- `POST /api/reactflow/compile-model`：将 ReactFlow 节点、参数和连线编译为仿真网络，并返回组件端口、无方向物理连接、压力-流量方程结构及未连接端口。
+- `POST /api/reactflow/simulate-testmodel`：运行现有固定拓扑 TestModel；该接口暂时不是任意拓扑求解器。
+- `POST /api/reactflow/simulate-test-mql`：返回固定拓扑 AMESim `test_mql` 的结构与采样摘要；132 状态数值对比使用独立 comparison 入口。AMESim 子模型已有 19 个第一版公开模型，但该接口本身不是任意拖拽拓扑求解器。
+- `POST /api/system-xml/validate`：接收原始 System XML v3，返回 XML、XSD 和模型语义三层诊断。
+- `POST /api/system-xml/parse`：校验 XML，并返回可直接编译、求解的规范化模型数据；它不还原 ReactFlow 画布布局。
+- `POST /api/system-xml/compile-model`：校验并解析 XML，然后创建 `app.simulation` 组件网络。
+- `POST /api/system-xml/simulate`：按 XML 中的组件、连接、参数和仿真设置运行当前支持的气动、标量信号及一维机械网络 MVP，并返回组件及端口时间序列。
+- `POST /api/simulation-results/csv`：校验结构化结果快照并导出 UTF-8 CSV 文件。
+
+气动端口的后端契约采用 `p` 势变量相等、`m_flow` 流变量代数和为零、`h_outflow` 按 stream 规则混合。所有组件统一规定 `m_flow > 0` 表示流入组件，物理连接的端点顺序不表示流向。
+
+当前网络层可按端口域处理气动压力-流量残差与 stream 焓、标量信号传播，以及一维机械 `x/v` 等值和 `f` 平衡，并使用 SciPy 完成非线性代数闭合和时间积分。XML 通用仿真当前采用半显式 ODE/代数 MVP：气瓶和贮箱作为储能元件，孔板及 XML 管段作为阻性元件，三通作为等压零结点，同时支持已登记的信号和机械基础件。它不是完整 DAE 或事件求解器，也不等价于严格 Modelica.Fluid 实现。
+
+XML 解析依赖 `lxml` 执行本地 XSD 校验，该依赖已包含在 `requirements.txt` 中。
+
+## 文档
+
+- [开发文档索引](docs/README.md)
+- [后端接口版本与定义规范 v1](docs/standard/backend-interface-version-spec-v1.md)
+- [组件模型建模规范 v1](docs/standard/component-model-authoring-spec-v1.md)
+- [组件库分类、发现与读取规范 v1](docs/standard/component-library-spec-v1.md)
+- [组件目录 JSON Schema v1](schemas/component-catalog-v1.schema.json)
+- [System XML v3 协议（当前规范）](docs/standard/system-xml-v3.md)
+- [System XML v3 XSD（当前 Schema）](schemas/system-simulation-v3.xsd)

app/simulation/README.md

@@ -1,41 +1,94 @@
-# PythonModels
+# 仿真后端
 
-`PythonModels` 用于承接 `ModelicaModels` 的 Python 平台移植。
+`app.simulation` 是 SystemSimulationApp 的仿真子包，用于承接模型定义、系统装配、数值求解和结果导出。
 
-目标不是把 `.mo` 文件逐行翻译成 Python，而是建立一个可运行、可对比、可逐步逼近 `OpenModelica` 行为的 Python 仿真框架。
+目标不是逐行翻译源模型，而是建立可运行、可测试、可导出，并能与 OpenModelica 或 AMESim baseline 对比的 Python 仿真框架。
 
-当前状态不是“只有骨架”，而是“`Testmodel` 已有一版可运行的 ODE 近似实现，并具备基础结果导出与对比能力”。
+当前包含两条模型线：`Testmodel` 已有可运行的 ODE 近似和 OpenModelica 对比能力；`test_mql` 已形成 132 状态气动机械总闭包，正在按 AMESim baseline 做数值校准。
 
 ## 当前目录
 
-- `core/`: 通用基础设施
+- `core/`: 元件基类、端口、状态、介质、方程和元数据协议。
-  包含组件基类、状态与端口数据结构、介质模型、网络装配、积分入口。
+- `solvers/`: ODE、压力流量代数方程和 stream 求解。
-- `components/`: 元件级 Python 实现
+- `components/experimental/`: 用于验证元件开发规范的临时组件库。
-  目前有 `Cylinder`、`Tank`、`Pipe`、`Orifice`、`Tee` 五类元件。
+- `components/experimental/storage/`: 气瓶和贮箱等储能元件。
-- `systems/`: 系统级装配与闭合
+- `components/experimental/flow/`: 对外注册的阻性管道和孔板等流动元件。
-  当前只有 `TestModelSystem`，对应 `ModelicaModels/Testmodel.mo`。
+- `components/experimental/junctions/`: 三通等连接节点。
-- `reporting/`: 结果导出与对比
+- `components/amesim/`: AMESim 气动、信号和机械组件原语。
-  当前承接主变量 CSV、温度 CSV/SVG、Python 对 OpenModelica 的对比表与误差摘要导出。
+- `systems/`: 通用仿真网络与 XML 驱动系统装配。
-- `scripts/`: 运行脚本
+- `examples/testmodel/`: 固定 TestModel、专用闭合逻辑和基线运行入口。
-  当前入口是 `run_testmodel.py`。
+- `examples/test_mql/`: AMESim `test_mql` 的系统装配、校准原语、诊断和运行入口。
-- `baselines/`: 提交进仓库的稳定基线
+- `reporting/`: CSV、SVG、运行报告、Modelica 对比结果、AMESim 结果读取和诊断报告导出。
-  当前承接 Python 主变量基线和 Python 对 Modelica 的误差摘要基线。
+- `registry.py`: 从已启用库清单受控发现、校验和实例化组件。
-- `runs/`: 每次实际运行的默认输出目录
+- `paths.py`: 项目、运行产物、基准和 Modelica 参考结果路径。
-  当前脚本默认会在这里创建带时间戳的子目录，用来放这次运行生成的产物。
+
+稳定基准存放在 `tests/baselines/simulation/`，实际运行产物默认写入被 Git 忽略的
+`app/data/simulation-runs/`。新增或修改元件时，先阅读 `components/example.md`。
+需要把运行产物写到仓库外时，可以设置 `SIMULATIONAPP_DATA_DIR` 环境变量。
+
+FastAPI 的 `GET /api/components/catalog` 会把注册表转换成前端组件目录。ReactFlow
+启动时自动读取该接口；接口暂时不可用时使用内置的同结构兜底定义。
+
+临时组件库的声明入口是 `components/experimental/library.py`，AMESim 第一版
+公开临时库入口是 `components/amesim/library.py`。公开模型必须在
+模型类中声明 `MODEL_TYPE / MODEL_VERSION / PORTS / PARAMETERS /
+RESULT_VARIABLES / DISPLAY / create()`，再把类路径加入库清单。完整规范参见
+[`组件模型建模规范 v1`](../../docs/standard/component-model-authoring-spec-v1.md)和
+[`组件库分类、发现与读取规范 v1`](../../docs/standard/component-library-spec-v1.md)。
 
 当前关键文件：
 
-- `core/medium.py`: 理想气体近似介质 `IdealGasMedium`
+- `core/medium.py`: 气体介质协议 `GasMedium` 与通用理想气体实现 `IdealGasMedium`
-- `core/medium.py`: 温度相关的空气近似介质 `IdealGasMedium`
+- `components/amesim/media/`: AMESim 零端口介质物性定义元件；具体类型确定介质，`property_model` 下拉参数选择计算方法，当前提供空气理想气体和氦气 Peng-Robinson
-- `core/network.py`: `SimulationNetwork`，负责组件注册、连接拓扑和状态向量拼装
+- `components/amesim/gases.py`: AMESim `gi` 介质物性实例注册表；`gi=0` 固定为空气（理想气体，内置默认），`gi=1..99` 引用画布中的显式介质定义
-- `core/solver.py`: `integrate_ode()`，优先走 `SciPy solve_ivp`，缺依赖时回退到内置 RK4，并支持 `t_start == t_stop` 的零时长返回
+- `core/peng_robinson.py`: `test_mql` 与公开氦气介质共用的 Peng-Robinson 状态方程
-- `components/pipe.py`: 单阻容管道近似，入口压降 + 出口直连内容腔
+- `performance.py`: 默认关闭、按单次仿真隔离的阶段与物性性能埋点
-- `components/tee.py`: 三通的最小 stream 混合 helper
+- `benchmark_performance.py`: System XML 主求解路径的可重复命令行基准工具
-- `systems/testmodel.py`: `Testmodel` 的系统装配壳与外部运行入口
+- `systems/network.py`: `SimulationNetwork`，负责组件注册、连接拓扑和状态向量拼装
-- `systems/testmodel_closure.py`: `Testmodel` 当前专用的闭合、初始化投影、分支求解与端口回写
+- `solvers/solver.py`: `integrate_ode()`，优先走 `SciPy solve_ivp`，缺依赖时回退到内置 RK4，并支持 `t_start == t_stop` 的零时长返回
+- `examples/testmodel/dynamic_pipe.py`: TestModel 专用单阻容管道近似，入口压降 + 出口直连内容腔
+- `components/experimental/junctions/tee.py`: 三通的最小 stream 混合 helper
+- `examples/testmodel/system.py`: `Testmodel` 的系统装配壳与外部运行入口
+- `examples/testmodel/closure.py`: `Testmodel` 当前专用的闭合、初始化投影、分支求解与端口回写
+- `examples/test_mql/system.py`: `test_mql` 系统装配、132 状态总闭包和关键输出映射
+- `examples/test_mql/closure.py`: `test_mql` 气动网络 closure、snapshot、流量计算和端口写回
+- `examples/test_mql/primitives/`: 固定算例专用的 Peng-Robinson 氦气、管路和机械校准原语
+- `examples/test_mql/structural_network.py`: 固定算例专用的结构网络；不替代带端口契约校验的通用网络
 - `reporting/testmodel_outputs.py`: `Testmodel` 的 CSV/SVG/对比摘要导出
-- `scripts/run_testmodel.py`: 基线运行与程序化执行入口
+- `reporting/amesim_results.py`: AMESim 结果读取入口
-- `tests/test_pythonmodels_regression.py`: 当前 Python 基线回归测试
+- `examples/test_mql/run_full_state_comparison.py`: `test_mql` 短时域 AMESim comparison 和诊断入口
+- `examples/test_mql/run.py`: `test_mql` 结构运行与程序化执行入口
+- `tests/`: 当前组件契约、XML、通用系统、AMESim 迁移和结果导出测试
+
+## 可选性能诊断
+
+`SIMULATIONAPP_PROFILE` 支持 `off`（默认）、`standard` 和 `audit`。`standard`
+只统计低频的大阶段；`audit` 才展开 RHS、代数闭合、stream 和物性调用，开销也
+明显更高。最终优化收益必须在 `off` 下复测。
+
+Peng–Robinson 氦气的高开销物性默认使用一次仿真内独立的精确 LRU 缓存；不同
+仿真任务不会共享条目，仿真结束后自动释放。可在启动进程前设置
+`SIMULATIONAPP_PROPERTY_CACHE=off` 做数值和性能 A/B，正常运行保持默认 `on`。
+缓存只复用完全相同的输入，不做四舍五入或容差匹配。
+
+FastAPI worker 默认在 lifespan 启动阶段预热 SciPy 积分、非线性求解、稀疏
+Jacobian 和 System XML XSD，完成后才开始接收请求。它不会运行业务模型，也不
+写入文件；如需诊断冷启动，可设置 `SIMULATIONAPP_WARMUP=off`。每个 worker 都会
+独立暖机一次。
+
+```powershell
+.venv-win\Scripts\python.exe -m app.simulation.benchmark_performance `
+  --mode audit --warmups 1 --runs 3 `
+  --factory "helium_step=tests.test_amesim_pnvo001_signal_xml:high_pressure_helium_step_project" `
+  --output app/data/performance-evaluations/helium-step.json
+```
+
+缓存关闭对照可在同一命令中增加 `--disable-property-cache`。缓存容量、命中、
+未命中和驱逐数会在 audit 响应的
+`diagnostics.performance.propertyCache` 中返回。
+
+基准原始 JSON 默认放到已忽略的 `app/data/` 下。指标字段、实测结果和使用边界见
+[`仿真性能评估 2026-08-15`](../../docs/other/仿真性能评估-2026-08-15.md)。
 
 ## 当前阶段进度
 
@@ -73,7 +126,7 @@
 本次推送已经把上一轮建议里的 `M2-M5` 推进到下面这个状态：
 
 1. `M2`：已完成当前阶段首版
-   - 已把 `Testmodel` 的专用闭合、初始化投影、分支入口流量求解、下游支路出口流量闭合、端口状态回写，从 `systems/testmodel.py` 拆到新的 `systems/testmodel_closure.py`
+   - 已把 `Testmodel` 的专用闭合、初始化投影、分支入口流量求解、下游支路出口流量闭合、端口状态回写，从 `examples/testmodel/system.py` 拆到 `examples/testmodel/closure.py`
    - `TestModelSystem` 现在主要承担组件装配、网络注册和对闭合器的委托，不再继续堆积系统级手写细节
 
 2. `M3`：已完成当前阶段首版
@@ -165,31 +218,31 @@
    `testmodel_tank_temperature.svg`
 11. 基于 `ModelicaModels/Simulation/Testmodel_res.csv` 的逐时刻对比与误差摘要导出。
 12. 基于 `unittest` 的自动回归测试，当前已覆盖初始化守恒、主变量基线、运行接口、内部闭合诊断、通用分支兼容层、通用结果键与旧键别名一致性，以及部分中间闭合过程行为。
+13. 面向 System XML v3 的拓扑驱动仿真 MVP：压力-流量非线性闭合、stream 焓传播、动态状态自动拼装和端口结果序列。
 
 当前没有实现：
 
 - 通用 DAE 初始化器
 - `Modelica.Media.Air.SimpleAir` 的严格复刻
-- 面向任意拓扑的通用 connector/stream 求解器
+- 一般高指数 DAE、事件和严格 Modelica `inStream/actualStream` 求解器
 
 ## 当前怎么运行
 
 最小运行方式：
 
 ```bash
-python3 -m PythonModels.scripts.run_testmodel
+python -m app.simulation.examples.testmodel.run
 ```
 
 如果要改模型参数或运行参数，建议直接改配置对象，而不是改源码里的默认值。例如：
 
 ```python
-from PythonModels.core.solver import SolveIVPConfig
+from app.simulation.examples.testmodel.run import (
-from PythonModels.scripts.run_testmodel import (
     TestModelRunConfig,
     TestModelSamplingConfig,
     run_testmodel,
 )
-from PythonModels.systems.testmodel import (
+from app.simulation.examples.testmodel.system import (
     BranchConfig,
     CylinderConfig,
     OrificeConfig,
@@ -197,6 +250,7 @@ from PythonModels.systems.testmodel import (
     TankConfig,
     TestModelConfig,
 )
+from app.simulation.solvers.solver import SolveIVPConfig
 
 run_config = TestModelRunConfig(
     model=TestModelConfig(
@@ -217,7 +271,7 @@ result = run_testmodel(run_config=run_config)
 如果调用方想先确认“这次运行最后到底会用哪些路径、哪些采样点”，可以先准备请求，再执行：
 
 ```python
-from PythonModels.scripts.run_testmodel import (
+from app.simulation.examples.testmodel.run import (
     prepare_testmodel_run,
     run_prepared_testmodel,
     TestModelRunConfig,
@@ -237,12 +291,13 @@ print(result.used_modelica_reference)
 1. 构建 `TestModelSystem`
 2. 打印原始初值向量与约束一致后的初值向量
 3. 运行 `0 s -> 20 s` 的仿真，默认采样间隔 `0.1 s`
-4. 将结果写入 `PythonModels/runs/` 下本次运行专属的时间戳目录
+4. 将结果写入 `app/data/simulation-runs/` 下本次运行专属的时间戳目录
 5. 若存在 `ModelicaModels/Simulation/Testmodel_res.csv`，自动生成 Python 与 OpenModelica 对比结果
 
-当前脚本默认不会再把运行结果直接写到提交基线目录，而是会在 `PythonModels/runs/` 下创建一个带时间戳的子目录，例如：
+当前脚本默认不会把运行结果直接写到提交基线目录，而是会在
+`app/data/simulation-runs/` 下创建一个带时间戳的子目录，例如：
 
-- `PythonModels/runs/testmodel_20260512_103000_123456/`
+- `app/data/simulation-runs/testmodel_20260512_103000_123456/`
 
 该目录里通常会包含：
 
@@ -256,18 +311,30 @@ print(result.used_modelica_reference)
 ## 基线结果
 
 当前基线对比摘要来自：
-[testmodel_modelica_comparison_summary.txt](/home/lujz/projects/pressurization-transfer-system/PythonModels/baselines/testmodel/testmodel_modelica_comparison_summary.txt)
+[`testmodel_modelica_comparison_summary.txt`](../../tests/data/testmodel/testmodel_modelica_comparison_summary.txt)
 
 当前四个主变量的最大误差为：
 
-- `mytank.p`: `max_abs_error = 134.960857 Pa`, `max_rel_error = 0.006798%`
+- `mytank.p`: `max_abs_error = 134.960858 Pa`, `max_rel_error = 0.006798%`
 - `mytank.T`: `max_abs_error = 0.035507 K`, `max_rel_error = 0.009016%`
 - `mycylinder.p`: `max_abs_error = 1391.986349 Pa`, `max_rel_error = 0.009447%`
 - `mycylinder.T`: `max_abs_error = 0.009069 K`, `max_rel_error = 0.003870%`
 
 这说明在当前基线工况下，Python 版主变量已经能较好贴近 OpenModelica 结果。
 
-## 当前架构判断
+## AMESim test_mql 当前进度
+
+`test_mql` 从 `AmesimModels/test_mql.ame` 迁移，并与旧 `testmodel` 保持独立。
+固定算例实现统一位于 `examples/test_mql/`，结果读取和比较能力位于
+`reporting/`；公开拖拽组件由 `components/amesim/library.py` 单独登记。
+
+当前已形成 112 个气动状态和 20 个机械状态的总闭包、AMESim 原生结果读取、
+`Data_Path` 输出校验及短时域 comparison。这里不再复制易过期的数值进度；
+最新对比结果、运行命令、限制和下一步校准路径以
+[`AmesimModels/test_mql/README.md`](../../AmesimModels/test_mql/README.md)
+为唯一说明。当前仍不能宣称 Python 时域仿真与 AMESim 全局一致。
+
+## Testmodel 当前架构判断
 
 如果按“组件正确 -> 网络闭合 -> 积分可跑 -> 结果对齐 -> 去近似”来看，当前大致处于：
 
@@ -281,14 +348,14 @@ print(result.used_modelica_reference)
 
 `Testmodel` 已有一版可运行、可导出、可对比的 Python 近似实现。
 
-## 已知限制
+## Testmodel 已知限制
 
 当前最主要的限制可以直接理解成下面几条：
 
 - 介质模型已从常 `cp/cv` 推进到温度相关空气近似，但仍不是 `Modelica.Media.Air.SimpleAir` 的严格复刻。
 - 系统整体仍是 ODE 化近似，不是原始 Modelica DAE 的直接复现。
 - `mytee1 -> mytank` 这一段虽然已经去掉早期的“虚拟出口导通系数”，改成了基于压力一致性的下游能量闭合，但本质上仍是工程近似。
-- 当前 `Tee` 的 stream 语义只覆盖了当前 `Testmodel` 需要的最小集合，还不是通用的 `inStream/actualStream` 框架。
+- 通用 XML 求解链路已经支持按实际流向传播和三通混合 stream 焓，但仍是正则化 MVP，不是严格的 Modelica `inStream/actualStream` 框架。
 - 当前一致初值仍是 ODE 入口处的约束投影，不等同于真正的 DAE 初始化求解。
 - 当前自动校验主要锁的是 Python 提交基线，还不是稳定的 Modelica 阈值回归。
 - 当前闭合器、系统层和 reporting 层虽然已经开始做“双支路结构化”，但对外结果序列、报告字段和部分导出命名仍然保留 `Testmodel` 专名兼容层，还没有完全转成通用表达。
@@ -307,7 +374,7 @@ print(result.used_modelica_reference)
 - 作为最终工程结论的唯一依据
 - 直接扩展到更复杂拓扑而不补通用连接器语义
 
-## 文件级现状
+## Testmodel 文件级现状
 
 按代码现状逐项看：
 
@@ -317,24 +384,24 @@ print(result.used_modelica_reference)
   `PortState` 目前只保留 `p`、`m_flow`、`h_outflow` 三个必要字段。
 - `core/state.py`: 正常
   `VolumeState` 只负责 `[m, U]` 状态打包。
-- `core/network.py`: 正常
+- `systems/network.py`: 正常
   负责状态向量拼装和连接摘要，不参与物理求解。
-- `core/solver.py`: 正常
+- `solvers/solver.py`: 正常
   已支持 SciPy、RK4 回退和零时长仿真。
-- `components/*.py`: 正常
+- `components/experimental/**/*.py`: 正常
   都是当前一版近似模型，没有发现与 README 明显冲突的“未记录能力”。
-- `systems/testmodel.py`: 是当前最重要的技术债集中区
+- `examples/testmodel/system.py`: 是当前最重要的技术债集中区
   这里承载了下游流向切换、焓混合、压力投影等近似逻辑，后续演进应主要落在这里。
-- `scripts/run_testmodel.py`: 正常
+- `examples/testmodel/run.py`: 正常
   已不是“最小打印脚本”，而是当前结果导出和对比入口。
-- `baselines/`: 是当前稳定基线，不应该随着日常运行频繁改动。
+- `tests/baselines/simulation/`: 是当前稳定基线，不应该随着日常运行频繁改动。
-- `runs/`: 是当前默认运行产物目录，不是手写源代码，也不应该当作提交基线使用。
+- `app/data/simulation-runs/`: 是默认运行产物目录，不是手写源代码，也不应该提交。
 
-## 当前主技术债
+## Testmodel 当前主技术债
 
 目前最主要的技术债，可以直接理解成下面 4 件事：
 
 1. 当前初始化虽然已经引入迭代诊断，但本质上仍是 ODE 入口近似，不是真正的 DAE 初始化器。
-2. `systems/testmodel.py` 还是承载了太多系统级闭合和初始化逻辑，只是主要端口的手写 stream 方向判断已经搬到组件 helper 里了，装配参数本身已经基本收口到配置对象。
+2. `examples/testmodel/system.py` 还是承载了太多系统级闭合和初始化逻辑，只是主要端口的手写 stream 方向判断已经搬到组件 helper 里了，装配参数本身已经基本收口到配置对象。
 3. 自动校验现在主要锁的是 Python 这一版自己的基线，还不是稳定的 Modelica 阈值回归。
 4. 当前空气物性已经完成首轮基线校准，但还不是 `SimpleAir` 的严格复刻。以后如果换工况，或者拿到更多 Modelica 原始结果，参数大概率还要继续调。

app/simulation/__init__.py

@@ -0,0 +1,2 @@
+"""Simulation domain models, solvers, system assembly, and result tools."""
+

app/simulation/benchmark_performance.py

@@ -0,0 +1,244 @@
+from __future__ import annotations
+
+import argparse
+import hashlib
+import importlib
+import json
+import os
+import platform
+import statistics
+import sys
+from datetime import UTC, datetime
+from math import ceil
+from pathlib import Path
+from time import perf_counter_ns, process_time_ns
+from typing import Any
+
+
+def _named_value(value: str, *, option: str) -> tuple[str, str]:
+    name, separator, target = value.partition("=")
+    if not separator or not name.strip() or not target.strip():
+        raise ValueError(
+            f"{option} must use NAME=VALUE syntax, received {value!r}."
+        )
+    return name.strip(), target.strip()
+
+
+def _percentile(values: list[float], percentile: float) -> float:
+    ordered = sorted(values)
+    index = max(0, min(len(ordered) - 1, ceil(percentile * len(ordered)) - 1))
+    return ordered[index]
+
+
+def _duration_summary(values: list[float]) -> dict[str, object]:
+    return {
+        "samplesMs": values,
+        "minimumMs": min(values),
+        "medianMs": statistics.median(values),
+        "p95Ms": _percentile(values, 0.95),
+        "maximumMs": max(values),
+    }
+
+
+def _load_factory_xml(specification: str) -> bytes:
+    module_name, separator, member_name = specification.partition(":")
+    if not separator or not module_name or not member_name:
+        raise ValueError(
+            "Factory specifications must use module.path:callable syntax."
+        )
+    factory = getattr(importlib.import_module(module_name), member_name)
+    value = factory()
+    if isinstance(value, bytes):
+        return value
+    if isinstance(value, str):
+        return value.encode("utf-8")
+
+    from app.main import build_reactflow_system_xml
+
+    return build_reactflow_system_xml(value)
+
+
+def _serialize_result_event(result: dict[str, object]) -> bytes:
+    """Render the final NDJSON payload shape used by the streaming endpoint."""
+
+    status = str(result.get("status", "completed"))
+    event = {
+        "event": "result",
+        "progress": 100 if status == "completed" else 0,
+        "phase": status,
+        "message": "仿真完成" if status == "completed" else "仿真任务结束",
+        "simulatedTime": result.get("simulatedUntil"),
+        "totalTime": result.get("requestedStopTime"),
+        "result": result,
+    }
+    return (
+        json.dumps(event, ensure_ascii=False, separators=(",", ":")) + "\n"
+    ).encode("utf-8")
+
+
+def _run_case(
+    name: str,
+    xml_bytes: bytes,
+    *,
+    warmups: int,
+    runs: int,
+    cancellable_path: bool,
+    allow_failures: bool,
+) -> dict[str, object]:
+    from app.main import run_system_xml_simulation
+
+    cancel_check = (lambda: False) if cancellable_path else None
+    for _ in range(warmups):
+        result = run_system_xml_simulation(xml_bytes, cancel_check=cancel_check)
+        if not bool(result.get("success")) and not allow_failures:
+            raise RuntimeError(f"Warmup for {name!r} failed: {result.get('message')}")
+
+    wall_samples_ms: list[float] = []
+    cpu_samples_ms: list[float] = []
+    serialization_samples_ms: list[float] = []
+    serialized_sizes: list[int] = []
+    profiles: list[dict[str, object]] = []
+    final_result: dict[str, object] | None = None
+    for _ in range(runs):
+        wall_start = perf_counter_ns()
+        cpu_start = process_time_ns()
+        result = run_system_xml_simulation(xml_bytes, cancel_check=cancel_check)
+        cpu_samples_ms.append((process_time_ns() - cpu_start) / 1_000_000.0)
+        wall_samples_ms.append((perf_counter_ns() - wall_start) / 1_000_000.0)
+        if not bool(result.get("success")) and not allow_failures:
+            raise RuntimeError(f"Benchmark for {name!r} failed: {result.get('message')}")
+        diagnostics = result.get("diagnostics")
+        if isinstance(diagnostics, dict):
+            performance = diagnostics.get("performance")
+            if isinstance(performance, dict):
+                profiles.append(performance)
+        serialization_start = perf_counter_ns()
+        serialized_event = _serialize_result_event(result)
+        serialization_samples_ms.append(
+            (perf_counter_ns() - serialization_start) / 1_000_000.0
+        )
+        serialized_sizes.append(len(serialized_event))
+        final_result = result
+
+    assert final_result is not None
+    return {
+        "name": name,
+        "success": bool(final_result.get("success")),
+        "message": final_result.get("message"),
+        "inputBytes": len(xml_bytes),
+        "inputSha256": hashlib.sha256(xml_bytes).hexdigest(),
+        "status": final_result.get("status"),
+        "simulatedUntil": final_result.get("simulatedUntil"),
+        "requestedStopTime": final_result.get("requestedStopTime"),
+        "wall": _duration_summary(wall_samples_ms),
+        "cpu": _duration_summary(cpu_samples_ms),
+        "resultSerialization": _duration_summary(serialization_samples_ms),
+        "resultEventBytes": serialized_sizes,
+        "performanceRuns": profiles,
+    }
+
+
+def _parse_arguments(argv: list[str] | None = None) -> argparse.Namespace:
+    parser = argparse.ArgumentParser(
+        description="Benchmark the real System XML simulation path with optional profiling."
+    )
+    parser.add_argument(
+        "--mode",
+        choices=("off", "standard", "audit"),
+        default="audit",
+        help="Instrumentation depth selected before importing the simulation modules.",
+    )
+    parser.add_argument("--warmups", type=int, default=1)
+    parser.add_argument("--runs", type=int, default=5)
+    parser.add_argument(
+        "--xml",
+        action="append",
+        default=[],
+        metavar="NAME=PATH",
+        help="Add an XML file benchmark case.",
+    )
+    parser.add_argument(
+        "--factory",
+        action="append",
+        default=[],
+        metavar="NAME=MODULE:CALLABLE",
+        help="Add a zero-argument factory returning XML or ReactFlowProjectPayload.",
+    )
+    parser.add_argument(
+        "--direct-path",
+        action="store_true",
+        help="Do not pass a cancel callback; use the one-shot SciPy path when eligible.",
+    )
+    parser.add_argument(
+        "--disable-property-cache",
+        action="store_true",
+        help="Disable the run-local exact property cache for an A/B comparison.",
+    )
+    parser.add_argument(
+        "--allow-failures",
+        action="store_true",
+        help="Record failed simulation runs instead of aborting the benchmark.",
+    )
+    parser.add_argument("--output", type=Path)
+    arguments = parser.parse_args(argv)
+    if arguments.warmups < 0:
+        parser.error("--warmups must not be negative.")
+    if arguments.runs <= 0:
+        parser.error("--runs must be positive.")
+    if not arguments.xml and not arguments.factory:
+        parser.error("At least one --xml or --factory case is required.")
+    return arguments
+
+
+def main(argv: list[str] | None = None) -> int:
+    arguments = _parse_arguments(argv)
+    os.environ["SIMULATIONAPP_PROFILE"] = arguments.mode
+    os.environ["SIMULATIONAPP_PROPERTY_CACHE"] = (
+        "off" if arguments.disable_property_cache else "on"
+    )
+
+    cases: list[tuple[str, bytes]] = []
+    for raw_case in arguments.xml:
+        name, raw_path = _named_value(raw_case, option="--xml")
+        cases.append((name, Path(raw_path).read_bytes()))
+    for raw_case in arguments.factory:
+        name, specification = _named_value(raw_case, option="--factory")
+        cases.append((name, _load_factory_xml(specification)))
+
+    report: dict[str, Any] = {
+        "generatedAt": datetime.now(UTC).isoformat(),
+        "profileMode": arguments.mode,
+        "cancellableSolverPath": not arguments.direct_path,
+        "propertyCacheEnabled": not arguments.disable_property_cache,
+        "allowFailures": bool(arguments.allow_failures),
+        "warmups": arguments.warmups,
+        "runs": arguments.runs,
+        "runtime": {
+            "python": sys.version,
+            "platform": platform.platform(),
+            "processor": platform.processor(),
+        },
+        "cases": [
+            _run_case(
+                name,
+                xml_bytes,
+                warmups=arguments.warmups,
+                runs=arguments.runs,
+                cancellable_path=not arguments.direct_path,
+                allow_failures=arguments.allow_failures,
+            )
+            for name, xml_bytes in cases
+        ],
+    }
+    text = json.dumps(report, ensure_ascii=False, indent=2)
+    if arguments.output is not None:
+        arguments.output.parent.mkdir(parents=True, exist_ok=True)
+        arguments.output.write_text(text + "\n", encoding="utf-8")
+        print(f"Performance report written to {arguments.output.resolve()}")
+    else:
+        print(text)
+    return 0
+
+
+if __name__ == "__main__":
+    raise SystemExit(main())

app/simulation/components/amesim/__init__.py

@@ -0,0 +1,3 @@
+from __future__ import annotations
+
+__all__: list[str] = []

app/simulation/components/amesim/boundary/__init__.py

@@ -0,0 +1 @@
+"""AMESim pneumatic boundary components."""

app/simulation/components/amesim/boundary/sources.py

@@ -0,0 +1,68 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.medium import IdealGasMedium
+from app.simulation.core.ports import PortDefinition
+
+
+class AmesimPnpl01(AlgebraicComponent):
+    """AMESim PNPL01 zero pneumatic flow source.
+
+    The component behaves as a sealed pneumatic boundary in the current acausal
+    solver: it does not prescribe pressure, and only constrains its port mass
+    flow to zero.
+    """
+
+    MODEL_TYPE = "amesim_pnpl01"
+    MODEL_VERSION = "0.1.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PORTS = (PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),)
+    PARAMETERS = ()
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="PNPL01 零气动流边界",
+        library_id="amesim",
+        category_id="boundary",
+        symbol="amesim_pnpl01",
+        ports=(PortDisplaySpec("port_1", "left", order=10),),
+        order=10,
+    )
+
+    def __init__(self, name: str) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({})
+        self.port_1 = self.register_declared_port("port_1")
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> AmesimPnpl01:
+        return cls(name=name)
+
+    def pressure_flow_equation_values(self) -> tuple[float, ...]:
+        return (self.port_1.m_flow,)
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        return (
+            EquationResidual(
+                id=f"{self.name}:zero_mass_flow",
+                owner="component",
+                owner_id=self.name,
+                relation="constitutive",
+                variables=(f"{self.name}.port_1.m_flow",),
+                role="flow",
+                value=self.port_1.m_flow,
+            ),
+        )
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        if "port_1" in connected_h:
+            self.port_1.h_outflow = connected_h["port_1"]

app/simulation/components/amesim/flow/__init__.py

@@ -0,0 +1 @@
+"""AMESim pneumatic flow components."""

app/simulation/components/amesim/gases.py

@@ -0,0 +1,264 @@
+from __future__ import annotations
+
+from collections.abc import Iterable, Mapping
+from dataclasses import dataclass
+from math import isclose, isfinite
+from types import MappingProxyType
+
+from app.simulation.core.metadata import ParameterDefinition
+from app.simulation.core.medium import GasMedium
+
+
+AMESIM_BUILTIN_AIR_GAS_INDEX = 0
+AMESIM_DEFAULT_GAS_INDEX = AMESIM_BUILTIN_AIR_GAS_INDEX
+AMESIM_MIN_GAS_INDEX = AMESIM_BUILTIN_AIR_GAS_INDEX
+AMESIM_MIN_DEFINED_GAS_INDEX = 1
+AMESIM_MAX_GAS_INDEX = 99
+
+AMESIM_GAS_INDEX_PARAMETER = ParameterDefinition(
+    "gi",
+    float(AMESIM_DEFAULT_GAS_INDEX),
+    label="介质物性模型（gi）",
+    quantity="dimensionless",
+    unit="",
+    minimum=float(AMESIM_MIN_GAS_INDEX),
+    maximum=float(AMESIM_MAX_GAS_INDEX),
+    editor="amesimGasReference",
+    description=(
+        "选择本元件使用的气体介质定义索引；0 表示内置空气，"
+        "1–99 引用画布中的介质定义组件。"
+    ),
+)
+
+AMESIM_GAS_DEFINITION_INDEX_PARAMETER = ParameterDefinition(
+    "gi",
+    float(AMESIM_MIN_DEFINED_GAS_INDEX),
+    label="介质定义索引（gi）",
+    quantity="dimensionless",
+    unit="",
+    minimum=float(AMESIM_MIN_DEFINED_GAS_INDEX),
+    maximum=float(AMESIM_MAX_GAS_INDEX),
+    description=(
+        "介质定义在当前模型中的唯一索引；由画布自动分配，"
+        "0 保留给内置空气。"
+    ),
+)
+
+
+def normalize_amesim_gas_index(value: float | int) -> int:
+    """Validate an AMESim gas reference.
+
+    Index 0 is reserved for the built-in ideal-gas air profile.  Positive
+    indices refer to medium-definition components placed in the project.
+    """
+
+    if isinstance(value, bool) or not isinstance(value, (int, float)):
+        raise ValueError("AMESim gas type index gi must be a number.")
+    numeric = float(value)
+    if not isfinite(numeric):
+        raise ValueError("AMESim gas type index gi must be finite.")
+    rounded = round(numeric)
+    if not isclose(numeric, rounded, rel_tol=0.0, abs_tol=1.0e-12):
+        raise ValueError("AMESim gas type index gi must be an integer value.")
+    index = int(rounded)
+    if not AMESIM_MIN_GAS_INDEX <= index <= AMESIM_MAX_GAS_INDEX:
+        raise ValueError(
+            "AMESim gas type index gi must be between "
+            f"{AMESIM_MIN_GAS_INDEX} and {AMESIM_MAX_GAS_INDEX}."
+        )
+    return index
+
+
+def normalize_amesim_defined_gas_index(value: float | int) -> int:
+    """Validate a positive index owned by a project medium definition."""
+
+    index = normalize_amesim_gas_index(value)
+    if index < AMESIM_MIN_DEFINED_GAS_INDEX:
+        raise ValueError(
+            "AMESim medium definition index gi must be between "
+            f"{AMESIM_MIN_DEFINED_GAS_INDEX} and {AMESIM_MAX_GAS_INDEX}; "
+            "gi=0 is reserved for built-in ideal-gas air."
+        )
+    return index
+
+
+@dataclass(frozen=True)
+class AmesimGasDefinition:
+    """One AMESim PNGD-style gas-definition slot.
+
+    ``fluid_type`` and ``eos_type`` are intentionally optional today.  They
+    reserve the metadata needed to map a future PNGD00 helium definition while
+    the executable behavior is supplied by ``medium``.
+    """
+
+    gi: int
+    label: str
+    medium: GasMedium
+    fluid_type: int | None = None
+    eos_type: int | None = None
+
+    def __post_init__(self) -> None:
+        normalized = normalize_amesim_gas_index(self.gi)
+        object.__setattr__(self, "gi", normalized)
+        if not self.label.strip():
+            raise ValueError("AMESim gas definition label must not be empty.")
+
+
+class AmesimGasRegistry:
+    """Resolve AMESim component ``gi`` references to thermodynamic media."""
+
+    def __init__(
+        self,
+        definitions: Iterable[AmesimGasDefinition] = (),
+        *,
+        default_gi: int = AMESIM_DEFAULT_GAS_INDEX,
+    ) -> None:
+        from app.simulation.components.amesim.media.mediums import (
+            AmesimIdealAirMedium,
+        )
+
+        self.default_gi = normalize_amesim_gas_index(default_gi)
+        self._definitions: dict[int, AmesimGasDefinition] = {
+            AMESIM_BUILTIN_AIR_GAS_INDEX: AmesimGasDefinition(
+                gi=AMESIM_BUILTIN_AIR_GAS_INDEX,
+                label="空气（理想气体，内置默认）",
+                medium=AmesimIdealAirMedium(),
+            )
+        }
+        for definition in definitions:
+            self.register(definition)
+
+    @property
+    def definitions(self) -> Mapping[int, AmesimGasDefinition]:
+        return MappingProxyType(self._definitions)
+
+    def register(self, definition: AmesimGasDefinition) -> None:
+        if not isinstance(definition, AmesimGasDefinition):
+            raise TypeError("AMESim gas registry entries must use AmesimGasDefinition.")
+        if definition.gi == AMESIM_BUILTIN_AIR_GAS_INDEX:
+            raise ValueError(
+                "AMESim gas type index gi=0 is reserved for built-in "
+                "ideal-gas air and cannot be replaced."
+            )
+        if definition.gi in self._definitions:
+            raise ValueError(
+                f"AMESim gas type index gi={definition.gi} is already defined."
+            )
+        self._definitions[definition.gi] = definition
+
+    def copy(self) -> AmesimGasRegistry:
+        """Return an independent registry for one project compilation."""
+
+        copied = AmesimGasRegistry(
+            (
+                definition
+                for index, definition in self._definitions.items()
+                if index != AMESIM_BUILTIN_AIR_GAS_INDEX
+            ),
+            default_gi=self.default_gi,
+        )
+        copied._definitions[AMESIM_BUILTIN_AIR_GAS_INDEX] = self._definitions[
+            AMESIM_BUILTIN_AIR_GAS_INDEX
+        ]
+        return copied
+
+    def resolve(
+        self,
+        gi: float | int,
+        *,
+        component_name: str | None = None,
+    ) -> GasMedium:
+        index = normalize_amesim_gas_index(gi)
+        try:
+            return self._definitions[index].medium
+        except KeyError as exc:
+            owner = f" for component '{component_name}'" if component_name else ""
+            available = ", ".join(str(index) for index in sorted(self._definitions))
+            available_message = available or "none"
+            raise ValueError(
+                f"AMESim gas type index gi={index}{owner} is not defined. "
+                "Register a PNGD-style gas definition before using this index. "
+                f"Available indices: {available_message}."
+            ) from exc
+
+    @property
+    def default_medium(self) -> GasMedium:
+        return self.resolve(self.default_gi)
+
+    def resolve_network_media(
+        self,
+        component_gas_indices: Mapping[str, float | int | None],
+        pneumatic_connections: Iterable[tuple[str, str]],
+    ) -> dict[str, GasMedium]:
+        """Assign one medium to every connected pneumatic circuit.
+
+        Components without ``gi`` inherit the explicit index used by their
+        circuit.  Conflicting indices inside one circuit are rejected instead
+        of silently mixing different gases.
+        """
+
+        parents = {component_id: component_id for component_id in component_gas_indices}
+
+        def find(component_id: str) -> str:
+            parent = parents[component_id]
+            while parent != parents[parent]:
+                parent = parents[parent]
+            while component_id != parent:
+                next_component = parents[component_id]
+                parents[component_id] = parent
+                component_id = next_component
+            return parent
+
+        def union(left: str, right: str) -> None:
+            left_root = find(left)
+            right_root = find(right)
+            if left_root != right_root:
+                parents[right_root] = left_root
+
+        for source, target in pneumatic_connections:
+            if source in parents and target in parents:
+                union(source, target)
+
+        members_by_root: dict[str, list[str]] = {}
+        for component_id in component_gas_indices:
+            members_by_root.setdefault(find(component_id), []).append(component_id)
+
+        media: dict[str, GasMedium] = {}
+        for members in members_by_root.values():
+            indexed_components: dict[int, list[str]] = {}
+            for component_id in members:
+                raw_index = component_gas_indices[component_id]
+                if raw_index is None:
+                    continue
+                index = normalize_amesim_gas_index(raw_index)
+                indexed_components.setdefault(index, []).append(component_id)
+
+            if len(indexed_components) > 1:
+                details = ", ".join(
+                    f"gi={index} ({', '.join(sorted(component_ids))})"
+                    for index, component_ids in sorted(indexed_components.items())
+                )
+                raise ValueError(
+                    "Connected pneumatic circuit contains conflicting AMESim "
+                    f"gas definitions: {details}."
+                )
+
+            index = (
+                next(iter(indexed_components))
+                if indexed_components
+                else self.default_gi
+            )
+            indexed_members = indexed_components.get(index, members)
+            medium = self.resolve(
+                index,
+                component_name=", ".join(sorted(indexed_members)),
+            )
+            for component_id in members:
+                media[component_id] = medium
+        return media
+
+
+def default_amesim_gas_registry() -> AmesimGasRegistry:
+    """Create a registry containing only built-in gi=0 ideal-gas air."""
+
+    return AmesimGasRegistry()

app/simulation/components/amesim/junctions/__init__.py

@@ -0,0 +1,5 @@
+from __future__ import annotations
+
+from app.simulation.components.amesim.junctions.nodes import AmesimP4Node2, AmesimPn3Node2
+
+__all__ = ["AmesimP4Node2", "AmesimPn3Node2"]

app/simulation/components/amesim/junctions/nodes.py

@@ -0,0 +1,239 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.medium import IdealGasMedium
+from app.simulation.core.ports import PortDefinition, PortState
+
+
+_REFERENCE_OUTFLOW_REGULARIZATION_RATIO = 0.05
+
+
+def _regularized_inverse_outflow(flow: float, transition_flow: float) -> float:
+    """Return a C1 inverse that tends to zero as a negative flow vanishes."""
+
+    if flow >= 0.0:
+        return 0.0
+    transition_flow = max(float(transition_flow), 1.0e-12)
+    if -flow >= transition_flow:
+        return 1.0 / flow
+    return (
+        flow
+        * (2.0 * transition_flow * transition_flow - flow * flow)
+        / transition_flow**4
+    )
+
+
+class _AmesimPneumaticNode(AlgebraicComponent):
+    """Shared implementation for AMESim pneumatic junction submodels.
+
+    PN3NODE2/P4NODE2 use port 2 as their pressure and temperature reference.
+    Non-reference outlet ports use that reference temperature. When port 2 is
+    an outlet, its enthalpy is the residual that closes the junction energy
+    balance, matching the AMESim dh2 causality.
+    """
+
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    REFERENCE_PORT = "port_2"
+
+    def __init__(self, name: str) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({})
+        self.temperature_reference_h = 0.0
+        for definition in self.PORTS:
+            setattr(self, definition.name, self.register_declared_port(definition.name))
+
+    def pressure_flow_equation_values(self) -> tuple[float, ...]:
+        reference = self.get_port(self.REFERENCE_PORT)
+        return tuple(
+            self.get_port(definition.name).p - reference.p
+            for definition in self.PORTS
+            if definition.name != self.REFERENCE_PORT
+        ) + (
+            sum(
+                self.get_port(definition.name).m_flow
+                for definition in self.PORTS
+            ),
+        )
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        reference = self.get_port(self.REFERENCE_PORT)
+        residuals: list[EquationResidual] = []
+        for definition in self.PORTS:
+            if definition.name == self.REFERENCE_PORT:
+                continue
+            port = self.get_port(definition.name)
+            residuals.append(
+                EquationResidual(
+                    id=f"{self.name}:{definition.name}_pressure_reference",
+                    owner="component",
+                    owner_id=self.name,
+                    relation="equal",
+                    variables=(
+                        f"{self.name}.{definition.name}.p",
+                        f"{self.name}.{self.REFERENCE_PORT}.p",
+                    ),
+                    role="effort",
+                    value=port.p - reference.p,
+                )
+            )
+        residuals.append(
+            EquationResidual(
+                id=f"{self.name}:mass_flow_balance",
+                owner="component",
+                owner_id=self.name,
+                relation="sumToZero",
+                variables=tuple(
+                    f"{self.name}.{definition.name}.m_flow"
+                    for definition in self.PORTS
+                ),
+                role="flow",
+                value=sum(self.get_port(definition.name).m_flow for definition in self.PORTS),
+            )
+        )
+        return tuple(residuals)
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        self.temperature_reference_h = connected_h.get(
+            self.REFERENCE_PORT,
+            sum(connected_h.values()) / len(connected_h) if connected_h else 0.0,
+        )
+        incoming = [
+            (port.m_flow, connected_h[name])
+            for name, port in self.ports.items()
+            if port.m_flow > 1e-12
+        ]
+        total_flow = sum(m_flow for m_flow, _ in incoming)
+        if total_flow > 1e-12:
+            mixed_h = sum(m_flow * h for m_flow, h in incoming) / total_flow
+        else:
+            mixed_h = self.temperature_reference_h
+
+        reference_port = self.get_port(self.REFERENCE_PORT)
+        for name, port in self.ports.items():
+            port.h_outflow = (
+                mixed_h
+                if name == self.REFERENCE_PORT
+                else self.temperature_reference_h
+            )
+
+        if reference_port.m_flow < 0.0:
+            energy_without_reference = sum(
+                port.m_flow
+                * (
+                    connected_h[name]
+                    if port.m_flow > 1e-12
+                    else self.temperature_reference_h
+                )
+                for name, port in self.ports.items()
+                if name != self.REFERENCE_PORT
+            )
+            non_reference_flow_scale = sum(
+                abs(port.m_flow)
+                for name, port in self.ports.items()
+                if name != self.REFERENCE_PORT
+            )
+            transition_flow = (
+                _REFERENCE_OUTFLOW_REGULARIZATION_RATIO
+                * non_reference_flow_scale
+            )
+            # Port 2 carries AMESim's residual-energy causality.  Exact
+            # division is singular when its outflow reverses through zero, so
+            # use a C1 band that matches the exact balance at its boundary and
+            # tends to the mixed enthalpy at zero flow.
+            inverse_flow = _regularized_inverse_outflow(
+                reference_port.m_flow,
+                transition_flow,
+            )
+            energy_residual_at_mixed_h = (
+                energy_without_reference
+                + reference_port.m_flow * mixed_h
+            )
+            reference_port.h_outflow = (
+                mixed_h - energy_residual_at_mixed_h * inverse_flow
+            )
+
+
+class AmesimPn3Node2(_AmesimPneumaticNode):
+    """AMESim PN3NODE2 pneumatic three-port junction."""
+
+    MODEL_TYPE = "amesim_pn3node2"
+    MODEL_VERSION = "0.3.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
+        ("mass_flow_balance",)
+    )
+    PORTS = (
+        PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
+    )
+    PARAMETERS = ()
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="PN3NODE2 三端气动节点",
+        library_id="amesim",
+        category_id="junctions",
+        symbol="amesim_pn3node2",
+        ports=(
+            PortDisplaySpec("port_1", "left", order=10),
+            PortDisplaySpec("port_2", "right", order=20),
+            PortDisplaySpec("port_3", "right", order=30),
+        ),
+        order=10,
+    )
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> AmesimPn3Node2:
+        return cls(name=name)
+
+
+class AmesimP4Node2(_AmesimPneumaticNode):
+    """AMESim P4NODE2 pneumatic four-port junction."""
+
+    MODEL_TYPE = "amesim_p4node2"
+    MODEL_VERSION = "0.3.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
+        ("mass_flow_balance",)
+    )
+    PORTS = (
+        PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_4", nominal_role="bidirectional"),
+    )
+    PARAMETERS = ()
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="P4NODE2 四端气动节点",
+        library_id="amesim",
+        category_id="junctions",
+        symbol="amesim_p4node2",
+        ports=(
+            PortDisplaySpec("port_1", "left", order=10),
+            PortDisplaySpec("port_2", "right", order=20),
+            PortDisplaySpec("port_3", "right", order=30),
+            PortDisplaySpec("port_4", "right", order=40),
+        ),
+        order=20,
+    )
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> AmesimP4Node2:
+        return cls(name=name)

app/simulation/components/amesim/library.py

@@ -0,0 +1,49 @@
+"""AMESim-compatible public component library."""
+
+from app.simulation.core.catalog import (
+    ComponentCategorySpec,
+    ComponentLibrarySpec,
+)
+
+
+LIBRARY = ComponentLibrarySpec(
+    id="amesim",
+    label="AMESim 组件库",
+    version="0.3.0",
+    source_package="app.simulation.components.amesim",
+    temporary=True,
+    order=200,
+    categories=(
+        ComponentCategorySpec(id="media", label="介质物性", order=5),
+        ComponentCategorySpec(id="storage", label="储能元件", order=10),
+        ComponentCategorySpec(id="flow", label="流动元件", order=20),
+        ComponentCategorySpec(id="junctions", label="连接元件", order=30),
+        ComponentCategorySpec(id="boundary", label="边界元件", order=40),
+        ComponentCategorySpec(id="signals", label="信号元件", order=50),
+        ComponentCategorySpec(id="mechanical", label="机械元件", order=60),
+    ),
+    models=(
+        "app.simulation.components.amesim.media.properties:AmesimIdealAirMediumDefinition",
+        "app.simulation.components.amesim.media.properties:AmesimHeliumMediumDefinition",
+        "app.simulation.components.amesim.boundary.sources:AmesimPnpl01",
+        "app.simulation.components.amesim.signals.sources:AmesimStep0",
+        "app.simulation.components.amesim.signals.sources:AmesimUd00",
+        "app.simulation.components.amesim.mechanical.translational:AmesimF000",
+        "app.simulation.components.amesim.mechanical.translational:AmesimForc",
+        "app.simulation.components.amesim.mechanical.translational:AmesimMecmas21",
+        "app.simulation.components.amesim.mechanical.translational:AmesimLstp00a",
+        "app.simulation.components.amesim.mechanical.translational:AmesimLmechn1",
+        "app.simulation.components.amesim.mechanical.pistons:AmesimPnrp17",
+        "app.simulation.components.amesim.storage.chambers:AmesimPnch023",
+        "app.simulation.components.amesim.storage.chambers:AmesimPnch012",
+        "app.simulation.components.amesim.flow.orifices:AmesimPnor001",
+        "app.simulation.components.amesim.flow.orifices:AmesimPnvo001FixedOpening",
+        "app.simulation.components.amesim.flow.orifices:AmesimPnvo001SignalOpening",
+        "app.simulation.components.amesim.flow.pipes:AmesimPnl00r",
+        "app.simulation.components.amesim.flow.pipes:AmesimPnl0001",
+        "app.simulation.components.amesim.flow.pipes:AmesimPnl0002",
+        "app.simulation.components.amesim.flow.pipes:AmesimPnl0003",
+        "app.simulation.components.amesim.junctions.nodes:AmesimPn3Node2",
+        "app.simulation.components.amesim.junctions.nodes:AmesimP4Node2",
+    ),
+)

app/simulation/components/amesim/mechanical/__init__.py

@@ -0,0 +1 @@
+"""AMESim mechanical components."""

app/simulation/components/amesim/mechanical/pistons.py

@@ -0,0 +1,305 @@
+from __future__ import annotations
+
+from collections.abc import Mapping, Sequence
+from dataclasses import dataclass
+from math import isfinite, pi
+
+from app.simulation.components.amesim.gases import (
+    AMESIM_GAS_INDEX_PARAMETER,
+    normalize_amesim_gas_index,
+)
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import ParameterDefinition, ResultVariableDefinition
+from app.simulation.core.medium import GasMedium
+from app.simulation.core.ports import PortDefinition
+
+
+AMESIM_REFERENCE_PRESSURE_PA = 101300.0
+
+
+@dataclass(frozen=True)
+class Pnrp17Linearization:
+    volume: float
+    volume_flow: float
+    pressure_force: float
+    volume_tangent: tuple[float, ...]
+    volume_flow_tangent: tuple[float, ...]
+    pressure_force_tangent: tuple[float, ...]
+    valid: bool = True
+    reason: str | None = None
+
+
+class AmesimPnrp17(AlgebraicComponent):
+    """AMESim PNRP17 pneumatic piston with two mechanical faces.
+
+    Mechanical ports 2/5 share the piston-side motion and ports 3/4 share the
+    cylinder-side motion. The pneumatic port contributes its swept volume and
+    volume rate to the connected variable-volume chamber.
+    """
+
+    MODEL_TYPE = "amesim_pnrp17"
+    MODEL_VERSION = "0.1.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PORTS = (
+        PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
+        PortDefinition.mechanical_translational("port_2"),
+        PortDefinition.mechanical_translational("port_3"),
+        PortDefinition.mechanical_translational("port_4"),
+        PortDefinition.mechanical_translational("port_5"),
+    )
+    PARAMETERS = (
+        AMESIM_GAS_INDEX_PARAMETER,
+        ParameterDefinition(
+            "dp",
+            0.2,
+            label="活塞直径",
+            quantity="length",
+            unit="m",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="活塞外径；与活塞杆直径共同确定有效受压面积。",
+        ),
+        ParameterDefinition(
+            "dr",
+            0.001,
+            label="活塞杆直径",
+            quantity="length",
+            unit="m",
+            minimum=0.0,
+            description="穿过气室一侧的活塞杆直径，必须不大于活塞直径。",
+        ),
+        ParameterDefinition(
+            "x0",
+            0.0,
+            label="初始腔长",
+            quantity="length",
+            unit="m",
+            description="机械端位移均为零时的气动腔长度。",
+        ),
+    )
+    RESULT_VARIABLES = (
+        ResultVariableDefinition("volume", "扫掠容积", "volume", "m3", "derived", 10),
+        ResultVariableDefinition(
+            "volume_flow",
+            "扫掠容积变化率",
+            "volume_flow",
+            "m3/s",
+            "derived",
+            20,
+        ),
+        ResultVariableDefinition("length", "气动腔长度", "length", "m", "derived", 30),
+        ResultVariableDefinition(
+            "pressure_force",
+            "气压力",
+            "force",
+            "N",
+            "derived",
+            40,
+        ),
+    )
+    DISPLAY = ComponentDisplaySpec(
+        label="PNRP17 气动活塞",
+        library_id="amesim",
+        category_id="mechanical",
+        symbol="amesim_pnrp17",
+        ports=(
+            PortDisplaySpec("port_1", "left", order=10),
+            PortDisplaySpec("port_3", "left", order=20),
+            PortDisplaySpec("port_2", "left", order=30),
+            PortDisplaySpec("port_4", "right", order=40),
+            PortDisplaySpec("port_5", "right", order=50),
+        ),
+        order=60,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: GasMedium,
+        *,
+        gi: float = 0.0,
+        dp: float = 0.2,
+        dr: float = 0.001,
+        x0: float = 0.0,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({"gi": gi, "dp": dp, "dr": dr, "x0": x0})
+        self.medium = medium
+        self.gi = normalize_amesim_gas_index(gi)
+        self.dp = float(dp)
+        self.dr = float(dr)
+        self.x0 = float(x0)
+        if self.dr > self.dp:
+            raise ValueError("PNRP17 rod diameter dr must not exceed piston diameter dp.")
+        for definition in self.PORTS:
+            port = self.register_declared_port(definition.name)
+            setattr(self, definition.name, port)
+        self.port_1.h_outflow = medium.specific_enthalpy(medium.T_ref)
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: GasMedium,
+        parameters: Mapping[str, float],
+    ) -> "AmesimPnrp17":
+        return cls(name=name, medium=medium, **dict(parameters))
+
+    @property
+    def effective_area(self) -> float:
+        return pi * (self.dp * self.dp - self.dr * self.dr) / 4.0
+
+    @property
+    def chamber_length(self) -> float:
+        return self.x0 + self.port_5.x - self.port_4.x
+
+    @property
+    def chamber_volume(self) -> float:
+        return self.effective_area * self.chamber_length
+
+    @property
+    def chamber_volume_flow(self) -> float:
+        return self.effective_area * (self.port_5.v - self.port_4.v)
+
+    @property
+    def pressure_force(self) -> float:
+        return (self.port_1.p - AMESIM_REFERENCE_PRESSURE_PA) * self.effective_area
+
+    def pressure_flow_equation_values(self) -> tuple[float, ...]:
+        values = [self.port_1.m_flow]
+        effort_pairs = (("port_2", "port_5"), ("port_3", "port_4"))
+        for first_name, second_name in effort_pairs:
+            first = self.get_port(first_name)
+            second = self.get_port(second_name)
+            values.extend((first.x - second.x, first.v - second.v))
+        force = self.pressure_force
+        values.extend(
+            (
+                self.port_2.f + self.port_5.f + force,
+                self.port_3.f + self.port_4.f - force,
+            )
+        )
+        return tuple(values)
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        effort_pairs = (("port_2", "port_5"), ("port_3", "port_4"))
+        residuals: list[EquationResidual] = [
+            EquationResidual(
+                id=f"{self.name}:pneumatic_zero_mass_flow",
+                owner="component",
+                owner_id=self.name,
+                relation="constitutive",
+                variables=(f"{self.name}.port_1.m_flow",),
+                role="flow",
+                value=self.port_1.m_flow,
+            )
+        ]
+        for first_name, second_name in effort_pairs:
+            first = self.get_port(first_name)
+            second = self.get_port(second_name)
+            for variable in ("x", "v"):
+                residuals.append(
+                    EquationResidual(
+                        id=f"{self.name}:{first_name}_{second_name}_{variable}_equal",
+                        owner="component",
+                        owner_id=self.name,
+                        relation="equal",
+                        variables=(
+                            f"{self.name}.{first_name}.{variable}",
+                            f"{self.name}.{second_name}.{variable}",
+                        ),
+                        role="effort",
+                        value=getattr(first, variable) - getattr(second, variable),
+                    )
+                )
+        force = self.pressure_force
+        residuals.extend(
+            (
+                EquationResidual(
+                    id=f"{self.name}:piston_side_force_balance",
+                    owner="component",
+                    owner_id=self.name,
+                    relation="constitutive",
+                    variables=(f"{self.name}.port_2.f", f"{self.name}.port_5.f", f"{self.name}.port_1.p"),
+                    role="flow",
+                    value=self.port_2.f + self.port_5.f + force,
+                ),
+                EquationResidual(
+                    id=f"{self.name}:cylinder_side_force_balance",
+                    owner="component",
+                    owner_id=self.name,
+                    relation="constitutive",
+                    variables=(f"{self.name}.port_3.f", f"{self.name}.port_4.f", f"{self.name}.port_1.p"),
+                    role="flow",
+                    value=self.port_3.f + self.port_4.f - force,
+                ),
+            )
+        )
+        return tuple(residuals)
+
+    def pneumatic_volume_outputs(self) -> Mapping[str, tuple[float, float]]:
+        return {"port_1": (self.chamber_volume, self.chamber_volume_flow)}
+
+    def linearize_geometry_and_force(
+        self,
+        port_4_x_tangent: Sequence[float],
+        port_5_x_tangent: Sequence[float],
+        port_4_v_tangent: Sequence[float],
+        port_5_v_tangent: Sequence[float],
+        port_1_pressure_tangent: Sequence[float],
+    ) -> Pnrp17Linearization:
+        """Return exact piston geometry and pressure-force tangents."""
+
+        vectors = tuple(
+            tuple(float(value) for value in values)
+            for values in (
+                port_4_x_tangent,
+                port_5_x_tangent,
+                port_4_v_tangent,
+                port_5_v_tangent,
+                port_1_pressure_tangent,
+            )
+        )
+        widths = {len(values) for values in vectors}
+        if len(widths) != 1:
+            raise ValueError("PNRP17 tangent vectors must have equal lengths.")
+        valid = all(isfinite(value) for values in vectors for value in values)
+        area = self.effective_area
+        volume_tangent = tuple(
+            area * (right - left)
+            for left, right in zip(vectors[0], vectors[1], strict=True)
+        )
+        volume_flow_tangent = tuple(
+            area * (right - left)
+            for left, right in zip(vectors[2], vectors[3], strict=True)
+        )
+        pressure_force_tangent = tuple(
+            area * value for value in vectors[4]
+        )
+        return Pnrp17Linearization(
+            volume=self.chamber_volume,
+            volume_flow=self.chamber_volume_flow,
+            pressure_force=self.pressure_force,
+            volume_tangent=volume_tangent,
+            volume_flow_tangent=volume_flow_tangent,
+            pressure_force_tangent=pressure_force_tangent,
+            valid=valid,
+            reason=None if valid else "non_finite_tangent_input",
+        )
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        self.port_1.h_outflow = connected_h.get(
+            "port_1",
+            self.medium.specific_enthalpy(self.medium.T_ref),
+        )
+
+    def component_result_values(self) -> Mapping[str, float]:
+        return {
+            "volume": self.chamber_volume,
+            "volume_flow": self.chamber_volume_flow,
+            "length": self.chamber_length,
+            "pressure_force": self.pressure_force,
+        }

app/simulation/components/amesim/media/__init__.py

@@ -0,0 +1,33 @@
+"""AMESim medium-property definition components."""
+
+from app.simulation.components.amesim.media.mediums import (
+    AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL,
+    AMESIM_AIR_PROPERTY_MODELS,
+    AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL,
+    AMESIM_HELIUM_PROPERTY_MODELS,
+    AmesimGasPropertyModelSpec,
+    AmesimHeliumPengRobinsonMedium,
+    AmesimIdealAirMedium,
+)
+from app.simulation.components.amesim.media.properties import (
+    AMESIM_AIR_PROPERTY_MODEL_PARAMETER,
+    AMESIM_HELIUM_PROPERTY_MODEL_PARAMETER,
+    AmesimGasMediumDefinitionComponent,
+    AmesimHeliumMediumDefinition,
+    AmesimIdealAirMediumDefinition,
+)
+
+__all__ = (
+    "AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL",
+    "AMESIM_AIR_PROPERTY_MODELS",
+    "AMESIM_AIR_PROPERTY_MODEL_PARAMETER",
+    "AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL",
+    "AMESIM_HELIUM_PROPERTY_MODELS",
+    "AMESIM_HELIUM_PROPERTY_MODEL_PARAMETER",
+    "AmesimGasMediumDefinitionComponent",
+    "AmesimGasPropertyModelSpec",
+    "AmesimHeliumMediumDefinition",
+    "AmesimHeliumPengRobinsonMedium",
+    "AmesimIdealAirMedium",
+    "AmesimIdealAirMediumDefinition",
+)

app/simulation/components/amesim/media/mediums.py

@@ -0,0 +1,517 @@
+from __future__ import annotations
+
+from collections.abc import Callable, Sequence
+from dataclasses import dataclass
+from math import exp, isfinite, log
+from typing import ClassVar
+
+from app.simulation.core.errors import RecoverableTrialStateError
+from app.simulation.core.medium import (
+    GasMedium,
+    IdealGasMedium,
+    ThermodynamicProperties,
+    ThermodynamicPropertiesLinearization,
+    ThermodynamicPropertyTangents,
+)
+from app.simulation.core.peng_robinson import HELIUM_PR, PengRobinsonFluid
+from app.simulation.performance import profile_property, record_property_iterations
+from app.simulation.property_cache import cache_property_calculation
+
+
+@dataclass(frozen=True)
+class AmesimIdealAirMedium(IdealGasMedium):
+    """AMESim air properties evaluated with the ideal-gas method.
+
+    Substance identity and property method are part of the concrete Python
+    type.  A future air correlation or helium Peng-Robinson implementation can
+    therefore coexist as a sibling type without turning ``gi`` into a fluid
+    enumeration.
+    """
+
+    SUBSTANCE_ID: ClassVar[str] = "air"
+    PROPERTY_METHOD_ID: ClassVar[str] = "ideal_gas"
+
+    name: str = "AMESimAirIdealGas"
+    R_gas: float = 287.0
+    cp_ref: float = 1005.0
+    T_ref: float = 300.0
+    cp_slope: float = 0.0
+    viscosity_ref: float = 1.82e-5
+    viscosity_T_ref: float = 293.15
+    sutherland_constant: float = 110.4
+
+
+@dataclass(frozen=True)
+class AmesimHeliumPengRobinsonMedium(IdealGasMedium):
+    """AMESim helium with a Peng-Robinson mechanical equation of state.
+
+    The pressure-density-temperature relation is evaluated by the shared
+    ``HELIUM_PR`` fluid.  The caloric reference follows the constant NASA
+    polynomial from Simcenter Amesim 2404 ``helium_cp_h_s.data``.
+    """
+
+    SUBSTANCE_ID: ClassVar[str] = "helium"
+    PROPERTY_METHOD_ID: ClassVar[str] = "peng_robinson"
+    fluid: ClassVar[PengRobinsonFluid] = HELIUM_PR
+    nasa_cp_over_R: ClassVar[float] = 2.5
+    nasa_enthalpy_constant_K: ClassVar[float] = -745.375
+    nasa_viscosity_coefficients: ClassVar[tuple[float, float, float, float]] = (
+        0.7501594,
+        35.76324,
+        -2212.129,
+        0.9212635,
+    )
+
+    name: str = "AMESimHeliumPengRobinson"
+    R_gas: float = HELIUM_PR.specific_gas_constant
+    cp_ref: float = nasa_cp_over_R * HELIUM_PR.specific_gas_constant
+    T_ref: float = 293.15
+    cp_slope: float = 0.0
+    viscosity_ref: float = 1.96e-5
+    viscosity_T_ref: float = 293.15
+    sutherland_constant: float = 79.4
+
+    @property
+    def cv(self) -> float:
+        return (self.nasa_cp_over_R - 1.0) * self.R_gas
+
+    def cv_at_temperature(self, T: float) -> float:
+        del T
+        return self.cv
+
+    def diagnostic_dynamic_viscosity(self, T: float) -> float:
+        """Return the AMESim NASA-table viscosity used by pipe diagnostics.
+
+        pn2pipefr reports Reynolds number with sagum viscosity. Keep this
+        separate from dynamic_viscosity so matching that diagnostic cannot
+        alter the already-validated pipe flow or friction dynamics.
+        """
+
+        if T <= 0.0:
+            raise ValueError("Temperature must be positive.")
+        a, b, c, d = self.nasa_viscosity_coefficients
+        return 1.0e-7 * exp(a * log(T) + b / T + c / (T * T) + d)
+
+    @profile_property("density")
+    @cache_property_calculation("density")
+    def density(self, p: float, T: float) -> float:
+        return self.fluid.density(p, T)
+
+    def _real_heat_capacities(
+        self,
+        p: float,
+        T: float,
+    ) -> tuple[float, float, float, float, float]:
+        density = self.density(p, T)
+        pressure_density_derivative = (
+            self.fluid.pressure_density_derivative_at_temperature(
+                T,
+                density,
+            )
+        )
+        pressure_temperature_derivative = (
+            self.fluid.pressure_temperature_derivative_at_density(
+                T,
+                density,
+            )
+        )
+        cv = (
+            self.cv_at_temperature(T)
+            + self.fluid.residual_isochoric_heat_capacity_at_density(T, density)
+        )
+        cp = (
+            cv
+            + T
+            * pressure_temperature_derivative
+            * pressure_temperature_derivative
+            / (density * density * pressure_density_derivative)
+        )
+        if cp <= 0.0 or cv <= 0.0:
+            raise ValueError("Real-gas heat capacities must be positive.")
+        return (
+            cp,
+            cv,
+            density,
+            pressure_density_derivative,
+            pressure_temperature_derivative,
+        )
+
+    def _local_isentropic_density_pressure_factor(
+        self,
+        p: float,
+        T: float,
+    ) -> tuple[float, float]:
+        cp, cv, density, pressure_density_derivative, pressure_temperature_derivative = (
+            self._real_heat_capacities(p, T)
+        )
+        heat_capacity_ratio = cp / cv
+        factor = p / (
+            density * pressure_density_derivative * heat_capacity_ratio
+        )
+        exponent = (
+            p
+            * (heat_capacity_ratio - 1.0)
+            / (
+                heat_capacity_ratio
+                * T
+                * pressure_temperature_derivative
+            )
+        )
+        return factor, exponent
+
+    @profile_property("isentropic_density_pressure_factor")
+    @cache_property_calculation("isentropic_density_pressure_factor")
+    def isentropic_density_pressure_factor(
+        self,
+        p: float,
+        T: float,
+        downstream_pressure: float | None = None,
+    ) -> float:
+        upstream_factor, isentropic_temperature_exponent = (
+            self._local_isentropic_density_pressure_factor(p, T)
+        )
+        if downstream_pressure is None or downstream_pressure >= p:
+            return upstream_factor
+
+        pressure_ratio = max(downstream_pressure / p, 1.0e-12)
+        isentropic_temperature = max(
+            T * pressure_ratio**isentropic_temperature_exponent,
+            2.2,
+        )
+        downstream_factor, _unused_exponent = (
+            self._local_isentropic_density_pressure_factor(
+                max(downstream_pressure, 1.0),
+                isentropic_temperature,
+            )
+        )
+        # AMESim 2404 saggs_ evaluates the local factor at the upstream
+        # state and at an approximate isentropic downstream state.
+        return 0.5 * (upstream_factor + downstream_factor)
+
+    def pressure(self, m: float, T: float, V: float) -> float:
+        if V <= 0.0:
+            raise ValueError("Volume must stay positive.")
+        return self.fluid.pressure_from_density(T, m / V)
+
+    @profile_property("specific_internal_energy")
+    def specific_internal_energy(self, T: float) -> float:
+        return self.R_gas * (
+            (self.nasa_cp_over_R - 1.0) * T
+            + self.nasa_enthalpy_constant_K
+        )
+
+    @profile_property("specific_internal_energy_at_pressure")
+    def specific_internal_energy_at_pressure(self, p: float, T: float) -> float:
+        density = self.density(p, T)
+        return (
+            self.specific_internal_energy(T)
+            + self.fluid.residual_specific_internal_energy_at_density(T, density)
+        )
+
+    @profile_property("specific_enthalpy")
+    def specific_enthalpy(self, T: float) -> float:
+        return self.R_gas * (
+            self.nasa_cp_over_R * T
+            + self.nasa_enthalpy_constant_K
+        )
+
+    @profile_property("specific_enthalpy_at_pressure")
+    def specific_enthalpy_at_pressure(self, p: float, T: float) -> float:
+        return self.specific_enthalpy(T) + self.fluid.residual_specific_enthalpy(p, T)
+
+    def temperature_from_internal_energy(self, u: float) -> float:
+        return (
+            u / self.R_gas - self.nasa_enthalpy_constant_K
+        ) / (self.nasa_cp_over_R - 1.0)
+
+    def temperature_from_enthalpy(self, h: float) -> float:
+        return (
+            h / self.R_gas - self.nasa_enthalpy_constant_K
+        ) / self.nasa_cp_over_R
+
+    @profile_property("temperature_from_pressure_enthalpy")
+    @cache_property_calculation("temperature_from_pressure_enthalpy")
+    def temperature_from_pressure_enthalpy(self, p: float, h: float) -> float:
+        temperature = max(self.temperature_from_enthalpy(h), 2.2)
+        for _iteration in range(16):
+            residual_enthalpy = self.fluid.residual_specific_enthalpy(p, temperature)
+            next_temperature = max(
+                self.temperature_from_enthalpy(h - residual_enthalpy),
+                2.2,
+            )
+            if abs(next_temperature - temperature) <= 1.0e-10 * max(
+                temperature,
+                1.0,
+            ):
+                record_property_iterations(
+                    "temperature_from_pressure_enthalpy",
+                    _iteration + 1,
+                    True,
+                )
+                return next_temperature
+            temperature = next_temperature
+        record_property_iterations(
+            "temperature_from_pressure_enthalpy",
+            16,
+            False,
+        )
+        return temperature
+
+    def temperature_from_mass_internal_energy(self, m: float, U: float) -> float:
+        if m <= 0.0:
+            raise RecoverableTrialStateError(
+                "Mass must stay positive when recovering temperature."
+            )
+        return self.temperature_from_internal_energy(U / m)
+
+    @profile_property("properties_from_mU")
+    @cache_property_calculation("properties_from_mU")
+    def properties_from_mU(
+        self,
+        m: float,
+        U: float,
+        V: float,
+    ) -> ThermodynamicProperties:
+        """Recover a real-gas state, reusing exact repeated evaluations.
+
+        Implicit integration asks several component interfaces for the same
+        ``(m, U, V)`` state while closing one RHS evaluation and while building
+        finite-difference Jacobians. The calculation is pure and its result is
+        immutable, so an exact-key bounded cache avoids repeating the
+        Peng-Robinson temperature iteration without changing model semantics.
+        """
+        if m <= 0.0:
+            raise RecoverableTrialStateError(
+                "Mass must stay positive when recovering temperature."
+            )
+        if V <= 0.0:
+            raise ValueError("Volume must stay positive.")
+        density = m / V
+        target_internal_energy = U / m
+        temperature = max(
+            self.temperature_from_internal_energy(target_internal_energy),
+            2.2,
+        )
+        converged = False
+        for _iteration in range(16):
+            residual_internal_energy = (
+                self.fluid.residual_specific_internal_energy_at_density(
+                    temperature,
+                    density,
+                )
+            )
+            next_temperature = max(
+                self.temperature_from_internal_energy(
+                    target_internal_energy - residual_internal_energy
+                ),
+                2.2,
+            )
+            if abs(next_temperature - temperature) <= 1.0e-10 * max(
+                temperature,
+                1.0,
+            ):
+                temperature = next_temperature
+                converged = True
+                break
+            temperature = next_temperature
+        record_property_iterations(
+            "properties_from_mU",
+            _iteration + 1,
+            converged,
+        )
+        pressure = self.fluid.pressure_from_density(temperature, density)
+        return ThermodynamicProperties(
+            p=pressure,
+            T=temperature,
+            rho=density,
+            u=target_internal_energy,
+            h=self.specific_enthalpy_at_pressure(
+                pressure,
+                temperature,
+            ),
+        )
+
+    def linearize_properties_from_mU(
+        self,
+        m: float,
+        U: float,
+        V: float,
+        dm: Sequence[float],
+        dU: Sequence[float],
+        dV: Sequence[float],
+        *,
+        properties: ThermodynamicProperties | None = None,
+    ) -> ThermodynamicPropertiesLinearization:
+        """Implicitly differentiate the Peng-Robinson m/U/V recovery."""
+
+        dm_values = tuple(float(value) for value in dm)
+        dU_values = tuple(float(value) for value in dU)
+        dV_values = tuple(float(value) for value in dV)
+        if not (len(dm_values) == len(dU_values) == len(dV_values)):
+            raise ValueError("Thermodynamic tangent vectors must have equal lengths.")
+        props = properties or self.properties_from_mU(m, U, V)
+        width = len(dm_values)
+
+        def invalid(reason: str) -> ThermodynamicPropertiesLinearization:
+            return ThermodynamicPropertiesLinearization(
+                properties=props,
+                tangents=ThermodynamicPropertyTangents.zeros(width),
+                valid=False,
+                reason=reason,
+            )
+
+        expected_density = m / V
+        expected_internal_energy = U / m
+        if (
+            abs(props.rho - expected_density)
+            > 1.0e-12 * max(abs(expected_density), 1.0)
+            or abs(props.u - expected_internal_energy)
+            > 1.0e-12 * max(abs(expected_internal_energy), 1.0)
+        ):
+            return invalid("properties_primal_mismatch")
+        if not all(
+            isfinite(value)
+            for values in (dm_values, dU_values, dV_values)
+            for value in values
+        ):
+            return invalid("non_finite_tangent_input")
+        if props.T <= 2.2 * (1.0 + 1.0e-10):
+            return invalid("temperature_floor_boundary")
+
+        pressure_temperature_derivative = (
+            self.fluid.pressure_temperature_derivative_at_density(
+                props.T,
+                props.rho,
+            )
+        )
+        pressure_density_derivative = (
+            self.fluid.pressure_density_derivative_at_temperature(
+                props.T,
+                props.rho,
+            )
+        )
+        cv = (
+            self.cv_at_temperature(props.T)
+            + self.fluid.residual_isochoric_heat_capacity_at_density(
+                props.T,
+                props.rho,
+            )
+        )
+        recovered_internal_energy = (
+            self.specific_internal_energy(props.T)
+            + self.fluid.residual_specific_internal_energy_at_density(
+                props.T,
+                props.rho,
+            )
+        )
+        recovery_scale = max(
+            abs(props.u),
+            abs(cv * props.T) if isfinite(cv) else 0.0,
+            1.0,
+        )
+        if (
+            not all(
+                isfinite(value)
+                for value in (
+                    pressure_temperature_derivative,
+                    pressure_density_derivative,
+                    cv,
+                    recovered_internal_energy,
+                )
+            )
+            or cv <= 0.0
+        ):
+            return invalid("invalid_peng_robinson_derivative")
+        if abs(recovered_internal_energy - props.u) > 1.0e-8 * recovery_scale:
+            return invalid("properties_recovery_not_converged")
+
+        internal_energy_density_derivative = (
+            props.p - props.T * pressure_temperature_derivative
+        ) / (props.rho * props.rho)
+        drho: list[float] = []
+        du: list[float] = []
+        dT: list[float] = []
+        dp: list[float] = []
+        dh: list[float] = []
+        for mass_tangent, energy_tangent, volume_tangent in zip(
+            dm_values,
+            dU_values,
+            dV_values,
+            strict=True,
+        ):
+            density_tangent = (
+                mass_tangent / V - m * volume_tangent / (V * V)
+            )
+            internal_energy_tangent = (
+                energy_tangent / m - U * mass_tangent / (m * m)
+            )
+            temperature_tangent = (
+                internal_energy_tangent
+                - internal_energy_density_derivative * density_tangent
+            ) / cv
+            pressure_tangent = (
+                pressure_temperature_derivative * temperature_tangent
+                + pressure_density_derivative * density_tangent
+            )
+            enthalpy_tangent = (
+                internal_energy_tangent
+                + pressure_tangent / props.rho
+                - props.p * density_tangent / (props.rho * props.rho)
+            )
+            drho.append(density_tangent)
+            du.append(internal_energy_tangent)
+            dT.append(temperature_tangent)
+            dp.append(pressure_tangent)
+            dh.append(enthalpy_tangent)
+
+        tangent_values = (*drho, *du, *dT, *dp, *dh)
+        if not all(isfinite(value) for value in tangent_values):
+            return invalid("non_finite_property_tangent")
+        return ThermodynamicPropertiesLinearization(
+            properties=props,
+            tangents=ThermodynamicPropertyTangents(
+                p=tuple(dp),
+                T=tuple(dT),
+                rho=tuple(drho),
+                u=tuple(du),
+                h=tuple(dh),
+            ),
+        )
+
+
+@dataclass(frozen=True)
+class AmesimGasPropertyModelSpec:
+    """A selectable calculation method for one AMESim gas substance."""
+
+    value: int
+    label: str
+    method_id: str
+    factory: Callable[[], GasMedium]
+    eos_type: int
+
+    def build_medium(self) -> GasMedium:
+        return self.factory()
+
+
+AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL = 0
+AMESIM_AIR_PROPERTY_MODELS = (
+    AmesimGasPropertyModelSpec(
+        value=AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL,
+        label="理想气体",
+        method_id=AmesimIdealAirMedium.PROPERTY_METHOD_ID,
+        factory=AmesimIdealAirMedium,
+        eos_type=1,
+    ),
+)
+
+
+AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL = 0
+AMESIM_HELIUM_PROPERTY_MODELS = (
+    AmesimGasPropertyModelSpec(
+        value=AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL,
+        label="Peng–Robinson",
+        method_id=AmesimHeliumPengRobinsonMedium.PROPERTY_METHOD_ID,
+        factory=AmesimHeliumPengRobinsonMedium,
+        eos_type=6,
+    ),
+)

app/simulation/components/amesim/media/properties.py

@@ -0,0 +1,196 @@
+from __future__ import annotations
+
+from abc import ABC
+from collections.abc import Mapping
+
+from app.simulation.components.amesim.gases import (
+    AMESIM_GAS_DEFINITION_INDEX_PARAMETER,
+    AmesimGasDefinition,
+    normalize_amesim_defined_gas_index,
+)
+from app.simulation.components.amesim.media.mediums import (
+    AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL,
+    AMESIM_AIR_PROPERTY_MODELS,
+    AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL,
+    AMESIM_HELIUM_PROPERTY_MODELS,
+    AmesimGasPropertyModelSpec,
+)
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec
+from app.simulation.core.medium import GasMedium
+from app.simulation.core.metadata import ParameterDefinition, ParameterOption
+
+
+AMESIM_AIR_PROPERTY_MODEL_PARAMETER = ParameterDefinition(
+    "property_model",
+    float(AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL),
+    label="物性计算模型",
+    quantity="dimensionless",
+    unit="",
+    minimum=float(min(model.value for model in AMESIM_AIR_PROPERTY_MODELS)),
+    maximum=float(max(model.value for model in AMESIM_AIR_PROPERTY_MODELS)),
+    editor="amesimGasPropertyModel",
+    options=tuple(
+        ParameterOption(value=model.value, label=model.label)
+        for model in AMESIM_AIR_PROPERTY_MODELS
+    ),
+    description="选择空气介质的物性计算方法；当前首版提供理想气体模型。",
+)
+
+AMESIM_HELIUM_PROPERTY_MODEL_PARAMETER = ParameterDefinition(
+    "property_model",
+    float(AMESIM_HELIUM_PENG_ROBINSON_PROPERTY_MODEL),
+    label="物性计算模型",
+    quantity="dimensionless",
+    unit="",
+    minimum=float(min(model.value for model in AMESIM_HELIUM_PROPERTY_MODELS)),
+    maximum=float(max(model.value for model in AMESIM_HELIUM_PROPERTY_MODELS)),
+    editor="amesimGasPropertyModel",
+    options=tuple(
+        ParameterOption(value=model.value, label=model.label)
+        for model in AMESIM_HELIUM_PROPERTY_MODELS
+    ),
+    description=(
+        "选择氦气介质的物性计算方法；当前首版提供 "
+        "Peng–Robinson 状态方程模型。"
+    ),
+)
+
+
+class AmesimGasMediumDefinitionComponent(AlgebraicComponent, ABC):
+    """Compile-time definition of one project-scoped AMESim gas medium.
+
+    Concrete subclasses declare one substance and its available calculation
+    methods; each instance selects a method through ``property_model``.  They
+    deliberately expose no physical ports or equations: the compiler consumes
+    them before it creates the simulation network.
+    """
+
+    IS_AMESIM_GAS_MEDIUM_DEFINITION = True
+    MEDIUM_LABEL = ""
+    FLUID_TYPE: int | None = None
+    PROPERTY_MODELS: tuple[AmesimGasPropertyModelSpec, ...] = ()
+
+    def __init__(
+        self,
+        name: str,
+        gi: float,
+        property_model: float = float(AMESIM_AIR_IDEAL_GAS_PROPERTY_MODEL),
+    ) -> None:
+        super().__init__(name)
+        self.gi = normalize_amesim_defined_gas_index(gi)
+        self.property_model = self._resolve_property_model(property_model).value
+        self.set_parameter_values(
+            {
+                "gi": self.gi,
+                "property_model": self.property_model,
+            }
+        )
+
+    def _resolve_property_model(
+        self,
+        value: float | int,
+    ) -> AmesimGasPropertyModelSpec:
+        for model in self.PROPERTY_MODELS:
+            if float(model.value) == float(value):
+                return model
+        available = ", ".join(str(model.value) for model in self.PROPERTY_MODELS)
+        raise ValueError(
+            f"AMESim medium definition '{self.name}' does not support property "
+            f"model {value:g}; available models: {available or 'none'}."
+        )
+
+    def build_medium(self) -> GasMedium:
+        """Create the executable property model selected by this instance."""
+
+        return self._resolve_property_model(self.property_model).build_medium()
+
+    def gas_definition(self) -> AmesimGasDefinition:
+        model = self._resolve_property_model(self.property_model)
+        return AmesimGasDefinition(
+            gi=self.gi,
+            label=f"{self.MEDIUM_LABEL}（{model.label}）",
+            medium=self.build_medium(),
+            fluid_type=self.FLUID_TYPE,
+            eos_type=model.eos_type,
+        )
+
+
+class AmesimIdealAirMediumDefinition(AmesimGasMediumDefinitionComponent):
+    """Project gas slot using the built-in ideal-gas air property method."""
+
+    MODEL_TYPE = "amesim_ideal_air_medium"
+    MODEL_VERSION = "0.2.0"
+    PORTS = ()
+    PARAMETERS = (
+        AMESIM_GAS_DEFINITION_INDEX_PARAMETER,
+        AMESIM_AIR_PROPERTY_MODEL_PARAMETER,
+    )
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="空气介质定义",
+        library_id="amesim",
+        category_id="media",
+        symbol="amesim_ideal_air_medium",
+        ports=(),
+        order=10,
+        role="amesimGasMediumDefinition",
+    )
+    MEDIUM_LABEL = "空气"
+    FLUID_TYPE = 2
+    PROPERTY_MODELS = AMESIM_AIR_PROPERTY_MODELS
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: GasMedium,
+        parameters: Mapping[str, float],
+    ) -> AmesimIdealAirMediumDefinition:
+        del medium
+        return cls(
+            name=name,
+            gi=parameters["gi"],
+            property_model=parameters["property_model"],
+        )
+
+
+class AmesimHeliumMediumDefinition(AmesimGasMediumDefinitionComponent):
+    """Project gas slot using the AMESim helium Peng-Robinson method."""
+
+    MODEL_TYPE = "amesim_helium_medium"
+    MODEL_VERSION = "0.1.0"
+    PORTS = ()
+    PARAMETERS = (
+        AMESIM_GAS_DEFINITION_INDEX_PARAMETER,
+        AMESIM_HELIUM_PROPERTY_MODEL_PARAMETER,
+    )
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="氦气介质定义",
+        library_id="amesim",
+        category_id="media",
+        symbol="amesim_helium_medium",
+        ports=(),
+        order=20,
+        role="amesimGasMediumDefinition",
+    )
+    MEDIUM_LABEL = "氦气"
+    FLUID_TYPE = 12
+    PROPERTY_MODELS = AMESIM_HELIUM_PROPERTY_MODELS
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: GasMedium,
+        parameters: Mapping[str, float],
+    ) -> AmesimHeliumMediumDefinition:
+        del medium
+        return cls(
+            name=name,
+            gi=parameters["gi"],
+            property_model=parameters["property_model"],
+        )

app/simulation/components/amesim/signals/sources.py

@@ -0,0 +1,355 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+from math import floor
+
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import (
+    ComponentDisplaySpec,
+    ParameterGroupDisplaySpec,
+    PortDisplaySpec,
+)
+from app.simulation.core.metadata import (
+    ParameterCondition,
+    ParameterDefinition,
+    ParameterOption,
+    ResultVariableDefinition,
+)
+from app.simulation.core.medium import IdealGasMedium
+from app.simulation.core.ports import PortDefinition
+
+
+def _ud00_stage_parameters(index: int) -> tuple[ParameterDefinition, ...]:
+    visible_when = (
+        ()
+        if index == 1
+        else (
+            ParameterCondition(
+                "nstages",
+                tuple(float(stage_count) for stage_count in range(index, 9)),
+            ),
+        )
+    )
+    return (
+        ParameterDefinition(
+            f"start{index}",
+            0.0 if index == 1 else 1.0,
+            label=f"第 {index} 段起点",
+            quantity="dimensionless",
+            unit="",
+            description=f"第 {index} 段开始时的输出值。",
+            visible_when=visible_when,
+        ),
+        ParameterDefinition(
+            f"end{index}",
+            1.0,
+            label=f"第 {index} 段终点",
+            quantity="dimensionless",
+            unit="",
+            description=f"第 {index} 段结束时的输出值。",
+            visible_when=visible_when,
+        ),
+        ParameterDefinition(
+            f"t{index}",
+            1.0 if index == 1 else 0.0,
+            label=f"第 {index} 段时长",
+            quantity="time",
+            unit="s",
+            minimum=0.0,
+            description=f"第 {index} 段的持续时间。",
+            visible_when=visible_when,
+        ),
+    )
+
+
+_UD00_STAGE_PARAMETERS = tuple(
+    parameter
+    for stage_index in range(1, 9)
+    for parameter in _ud00_stage_parameters(stage_index)
+)
+
+
+class AmesimStep0(AlgebraicComponent):
+    """AMESim STEP0 scalar step signal source."""
+
+    MODEL_TYPE = "amesim_step0"
+    MODEL_VERSION = "0.1.0"
+    PORTS = (PortDefinition.signal("out", nominal_role="output"),)
+    PARAMETERS = (
+        ParameterDefinition("initial", 0.0, label="初始值", quantity="dimensionless", unit=""),
+        ParameterDefinition("final", 1.0, label="阶跃后值", quantity="dimensionless", unit=""),
+        ParameterDefinition("time", 0.0, label="阶跃时间", quantity="time", unit="s"),
+    )
+    RESULT_VARIABLES = (
+        ResultVariableDefinition("y", "输出", "dimensionless", "", "signal", 10),
+    )
+    DISPLAY = ComponentDisplaySpec(
+        label="STEP0 阶跃信号",
+        library_id="amesim",
+        category_id="signals",
+        symbol="amesim_step0",
+        ports=(PortDisplaySpec("out", "right", order=10),),
+        order=10,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: IdealGasMedium,
+        *,
+        initial: float = 0.0,
+        final: float = 1.0,
+        time: float = 0.0,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({"initial": initial, "final": final, "time": time})
+        self.initial = float(initial)
+        self.final = float(final)
+        self.time = float(time)
+        self.out = self.register_declared_port("out")
+        self.out.signal = self.output_at(0.0)
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> "AmesimStep0":
+        return cls(
+            name=name,
+            medium=medium,
+            initial=parameters["initial"],
+            final=parameters["final"],
+            time=parameters["time"],
+        )
+
+    def output_at(self, time: float) -> float:
+        return self.final if time >= self.time else self.initial
+
+    def signal_output_values(self, time: float) -> dict[str, float]:
+        return {"out": self.output_at(time)}
+
+    def signal_event_times(
+        self,
+        start_time: float,
+        stop_time: float,
+    ) -> tuple[float, ...]:
+        """Expose the exact STEP0 switch time as an integration split point."""
+
+        return (self.time,) if start_time < self.time < stop_time else ()
+
+    def component_result_values(self) -> Mapping[str, float]:
+        return {"y": self.out.signal}
+
+
+class AmesimUd00(AlgebraicComponent):
+    """AMESim UD00 piecewise-linear scalar signal source."""
+
+    MODEL_TYPE = "amesim_ud00"
+    MODEL_VERSION = "0.2.0"
+    PORTS = (PortDefinition.signal("out", nominal_role="output"),)
+    PARAMETERS = (
+        ParameterDefinition(
+            "tstart",
+            0.0,
+            label="启动时间",
+            quantity="time",
+            unit="s",
+            description="分段信号开始输出第一段之前的等待时间。",
+        ),
+        *_UD00_STAGE_PARAMETERS,
+        ParameterDefinition(
+            "nstages",
+            1.0,
+            label="段数",
+            quantity="dimensionless",
+            unit="",
+            minimum=1.0,
+            maximum=8.0,
+            editor="choice",
+            options=tuple(
+                ParameterOption(float(stage_count), str(stage_count))
+                for stage_count in range(1, 9)
+            ),
+            description="参与输出计算的有效线性分段数量。",
+        ),
+        ParameterDefinition(
+            "iscyclic",
+            0.0,
+            label="循环",
+            quantity="dimensionless",
+            unit="",
+            minimum=0.0,
+            maximum=1.0,
+            editor="choice",
+            options=(
+                ParameterOption(0.0, "否"),
+                ParameterOption(1.0, "是"),
+            ),
+            description="当前公共协议编码：0 表示单次输出，1 表示循环输出。",
+        ),
+    )
+    RESULT_VARIABLES = (
+        ResultVariableDefinition("y", "输出", "dimensionless", "", "signal", 10),
+    )
+    DISPLAY = ComponentDisplaySpec(
+        label="UD00 分段线性信号",
+        library_id="amesim",
+        category_id="signals",
+        symbol="amesim_ud00",
+        ports=(PortDisplaySpec("out", "right", order=10),),
+        order=20,
+        parameter_groups=(
+            ParameterGroupDisplaySpec(
+                id="stages",
+                label="分段参数",
+                parameters=tuple(
+                    parameter.name for parameter in _UD00_STAGE_PARAMETERS
+                ),
+                order=10,
+            ),
+        ),
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: IdealGasMedium,
+        *,
+        tstart: float = 0.0,
+        starts: tuple[float, ...] = (0.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0),
+        ends: tuple[float, ...] = (1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0, 1.0),
+        durations: tuple[float, ...] = (1.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0),
+        nstages: int = 1,
+        iscyclic: bool = False,
+    ) -> None:
+        super().__init__(name=name)
+        if len(starts) != 8 or len(ends) != 8 or len(durations) != 8:
+            raise ValueError("UD00 requires exactly eight start, end, and duration values.")
+        if nstages < 1 or nstages > 8:
+            raise ValueError("UD00 nstages must be between 1 and 8.")
+        self.tstart = float(tstart)
+        self.starts = tuple(float(value) for value in starts)
+        self.ends = tuple(float(value) for value in ends)
+        self.durations = tuple(float(value) for value in durations)
+        self.nstages = int(nstages)
+        self.iscyclic = bool(iscyclic)
+        values: dict[str, float] = {"tstart": self.tstart, "nstages": float(self.nstages), "iscyclic": float(int(self.iscyclic))}
+        for index in range(1, 9):
+            values[f"start{index}"] = self.starts[index - 1]
+            values[f"end{index}"] = self.ends[index - 1]
+            values[f"t{index}"] = self.durations[index - 1]
+        self.set_parameter_values(values)
+        self.out = self.register_declared_port("out")
+        self.out.signal = self.output_at(0.0)
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> "AmesimUd00":
+        nstages = parameters["nstages"]
+        iscyclic = parameters["iscyclic"]
+        definitions = {definition.name: definition for definition in cls.PARAMETERS}
+        for parameter_name, value in (
+            ("nstages", nstages),
+            ("iscyclic", iscyclic),
+        ):
+            numeric_value = float(value)
+            if not numeric_value.is_integer():
+                raise ValueError(f"UD00 {parameter_name} must be an integer.")
+            message = definitions[parameter_name].validation_message(numeric_value)
+            if message is not None:
+                raise ValueError(f"UD00 {parameter_name} {message}.")
+        return cls(
+            name=name,
+            medium=medium,
+            tstart=parameters["tstart"],
+            starts=tuple(parameters[f"start{index}"] for index in range(1, 9)),
+            ends=tuple(parameters[f"end{index}"] for index in range(1, 9)),
+            durations=tuple(parameters[f"t{index}"] for index in range(1, 9)),
+            nstages=int(nstages),
+            iscyclic=bool(int(iscyclic)),
+        )
+
+    def output_at(self, time: float) -> float:
+        elapsed = max(float(time) - self.tstart, 0.0)
+        active_durations = self.durations[: self.nstages]
+        total_duration = sum(active_durations)
+        if self.iscyclic and total_duration > 0.0:
+            elapsed = elapsed % total_duration
+
+        stage_start_time = 0.0
+        for index, duration in enumerate(active_durations):
+            stage_end_time = stage_start_time + duration
+            if elapsed < stage_end_time or index == self.nstages - 1:
+                if duration <= 0.0:
+                    return self.ends[index]
+                fraction = (elapsed - stage_start_time) / duration
+                return self.starts[index] + fraction * (self.ends[index] - self.starts[index])
+            stage_start_time = stage_end_time
+        return self.ends[self.nstages - 1]
+
+    def signal_output_values(self, time: float) -> dict[str, float]:
+        return {"out": self.output_at(time)}
+
+    def signal_event_times(
+        self,
+        start_time: float,
+        stop_time: float,
+    ) -> tuple[float, ...]:
+        """Return UD00 start, stage, and repeated cycle boundaries.
+
+        The final non-cyclic stage is intentionally not given an end event:
+        ``output_at`` continues that stage's slope after its configured duration.
+        """
+
+        if stop_time <= start_time:
+            return ()
+
+        active_durations = self.durations[: self.nstages]
+        stage_offsets = [0.0]
+        elapsed = 0.0
+        for duration in active_durations[:-1]:
+            elapsed += duration
+            stage_offsets.append(elapsed)
+
+        if not self.iscyclic:
+            return tuple(
+                sorted(
+                    {
+                        event_time
+                        for offset in stage_offsets
+                        if start_time
+                        < (event_time := self.tstart + offset)
+                        < stop_time
+                    }
+                )
+            )
+
+        cycle_duration = sum(active_durations)
+        if cycle_duration <= 0.0:
+            return ()
+
+        events: set[float] = set()
+        for offset in stage_offsets:
+            first_boundary = self.tstart + offset
+            cycle_index = max(
+                0,
+                floor((start_time - first_boundary) / cycle_duration) + 1,
+            )
+            event_time = first_boundary + cycle_index * cycle_duration
+            while event_time < stop_time:
+                if event_time > start_time:
+                    events.add(event_time)
+                cycle_index += 1
+                event_time = first_boundary + cycle_index * cycle_duration
+        return tuple(sorted(events))
+
+    def component_result_values(self) -> Mapping[str, float]:
+        return {"y": self.out.signal}

app/simulation/components/amesim/storage/__init__.py

@@ -0,0 +1 @@
+"""AMESim pneumatic storage components."""

app/simulation/components/amesim/storage/chambers.py

@@ -0,0 +1,690 @@
+from __future__ import annotations
+
+from collections.abc import Mapping, Sequence
+from dataclasses import dataclass
+from math import isfinite
+
+from app.simulation.components.amesim.gases import (
+    AMESIM_GAS_INDEX_PARAMETER,
+    normalize_amesim_gas_index,
+)
+from app.simulation.core.base import ThermodynamicVolumeComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import (
+    ParameterDefinition,
+    ResultVariableDefinition,
+    THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
+)
+from app.simulation.core.medium import (
+    GasMedium,
+    ThermodynamicProperties,
+    ThermodynamicPropertiesLinearization,
+)
+from app.simulation.core.ports import PortDefinition
+from app.simulation.core.state import VolumeState
+
+
+@dataclass(frozen=True)
+class Pnch012DerivativeLinearization:
+    derivative: tuple[float, float]
+    tangents: tuple[tuple[float, ...], tuple[float, ...]]
+    properties: ThermodynamicPropertiesLinearization
+    valid: bool = True
+    reason: str | None = None
+
+
+class AmesimPnch023(ThermodynamicVolumeComponent):
+    """AMESim PNCH023 simple pneumatic chamber with heat exchange.
+
+    The AMESim submodel owns pressure and temperature states and exposes two
+    pneumatic flow ports. This public component maps those states onto the
+    framework's mass/internal-energy volume state and keeps the AMESim
+    heat-transfer contract `kth * sth * (extemp - T)`.
+    """
+
+    MODEL_TYPE = "amesim_pnch023"
+    MODEL_VERSION = "0.1.0"
+    PORTS = (
+        PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
+    )
+    PARAMETERS = (
+        AMESIM_GAS_INDEX_PARAMETER,
+        ParameterDefinition(
+            "cvol",
+            0.057,
+            label="气室容积",
+            quantity="volume",
+            unit="m3",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="气室内部用于储存气体的固定有效容积。",
+        ),
+        ParameterDefinition(
+            "kth",
+            0.0,
+            label="换热系数",
+            quantity="heat_transfer_coefficient",
+            unit="W/(m2*K)",
+            minimum=0.0,
+            description="气室与环境之间的对流换热系数，与换热面积共同决定换热功率。",
+        ),
+        ParameterDefinition(
+            "sth",
+            0.1,
+            label="换热面积",
+            quantity="area",
+            unit="m2",
+            minimum=0.0,
+            description="气室与环境进行热交换的有效表面积。",
+        ),
+        ParameterDefinition(
+            "extemp",
+            293.15,
+            label="外部温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="气室外部环境的绝对温度，用于计算气体与环境之间的换热。",
+        ),
+        ParameterDefinition(
+            "p0",
+            100000.0,
+            label="初始压力",
+            quantity="pressure",
+            unit="Pa",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="仿真开始时气室内气体的绝对压力。",
+        ),
+        ParameterDefinition(
+            "T0",
+            293.15,
+            label="初始温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="仿真开始时气室内气体的绝对温度。",
+        ),
+    )
+    RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
+    DISPLAY = ComponentDisplaySpec(
+        label="PNCH023 固定容积气室",
+        library_id="amesim",
+        category_id="storage",
+        symbol="amesim_pnch023",
+        ports=(
+            PortDisplaySpec("port_1", "left", order=10),
+            PortDisplaySpec("port_2", "right", order=20),
+        ),
+        order=10,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: GasMedium,
+        *,
+        cvol: float = 0.057,
+        kth: float = 0.0,
+        sth: float = 0.1,
+        extemp: float = 293.15,
+        gi: float = 1.0,
+        p0: float = 100000.0,
+        T0: float = 293.15,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values(
+            {
+                "cvol": cvol,
+                "kth": kth,
+                "sth": sth,
+                "extemp": extemp,
+                "gi": gi,
+                "p0": p0,
+                "T0": T0,
+            }
+        )
+        self.medium = medium
+        self.cvol = float(cvol)
+        self.kth = float(kth)
+        self.sth = float(sth)
+        self.extemp = float(extemp)
+        self.gi = normalize_amesim_gas_index(gi)
+        self.p0 = float(p0)
+        self.T0 = float(T0)
+        m0 = medium.density(self.p0, self.T0) * self.cvol
+        U0 = m0 * medium.specific_internal_energy_at_pressure(self.p0, self.T0)
+        self.state = VolumeState(m=m0, U=U0)
+        initial_h = medium.specific_enthalpy_at_pressure(self.p0, self.T0)
+        self.port_1 = self.register_declared_port("port_1")
+        self.port_1.p = self.p0
+        self.port_1.h_outflow = initial_h
+        self.port_2 = self.register_declared_port("port_2")
+        self.port_2.p = self.p0
+        self.port_2.h_outflow = initial_h
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: GasMedium,
+        parameters: Mapping[str, float],
+    ) -> AmesimPnch023:
+        return cls(
+            name=name,
+            medium=medium,
+            cvol=parameters["cvol"],
+            kth=parameters["kth"],
+            sth=parameters["sth"],
+            extemp=parameters["extemp"],
+            gi=parameters["gi"],
+            p0=parameters["p0"],
+            T0=parameters["T0"],
+        )
+
+    def get_state_vector(self) -> list[float]:
+        return self.state.as_vector()
+
+    def set_state_vector(self, values: list[float]) -> None:
+        self.state = VolumeState.from_vector(values)
+
+    def properties(self) -> ThermodynamicProperties:
+        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.cvol)
+        self.port_1.p = props.p
+        self.port_1.h_outflow = props.h
+        self.port_2.p = props.p
+        self.port_2.h_outflow = props.h
+        return props
+
+    def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
+        return self.properties()
+
+    def thermal_energy_flow_w(self, temperature: float) -> float:
+        return self.kth * self.sth * (self.extemp - temperature)
+
+    def state_derivative_from_ports(
+        self,
+        connected_h: Mapping[str, float],
+    ) -> list[float]:
+        props = self.properties()
+        inlet_h_1 = self.connection_inlet_enthalpy(
+            port_m_flow=self.port_1.m_flow,
+            connected_h=connected_h["port_1"],
+            internal_h=props.h,
+        )
+        inlet_h_2 = self.connection_inlet_enthalpy(
+            port_m_flow=self.port_2.m_flow,
+            connected_h=connected_h["port_2"],
+            internal_h=props.h,
+        )
+        derivative = VolumeState(
+            m=self.port_1.m_flow + self.port_2.m_flow,
+            U=(
+                self.port_1.m_flow * inlet_h_1
+                + self.port_2.m_flow * inlet_h_2
+                + self.thermal_energy_flow_w(props.T)
+            ),
+        )
+        return derivative.as_vector()
+
+    def pressure_flow_equation_values(self) -> tuple[float, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.cvol,
+        ).p
+        return (
+            self.port_1.p - pressure,
+            self.port_2.p - pressure,
+        )
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.cvol,
+        ).p
+        return (
+            EquationResidual(
+                id=f"{self.name}:port_1_pressure_state",
+                owner="component",
+                owner_id=self.name,
+                relation="state",
+                variables=(f"{self.name}.port_1.p", f"{self.name}.state"),
+                role="effort",
+                value=self.port_1.p - pressure,
+            ),
+            EquationResidual(
+                id=f"{self.name}:port_2_pressure_state",
+                owner="component",
+                owner_id=self.name,
+                relation="state",
+                variables=(f"{self.name}.port_2.p", f"{self.name}.state"),
+                role="effort",
+                value=self.port_2.p - pressure,
+            ),
+        )
+
+
+class AmesimPnch012(ThermodynamicVolumeComponent):
+    """AMESim PNCH012 variable-volume pneumatic chamber.
+
+    AMESim supplies four external volume and volume-rate inputs through the
+    chamber ports. Fixed/prescribed contributions remain available as SI
+    parameters, while connected moving-boundary components can now add live
+    volume and volume-rate values through the pneumatic connector contract.
+    """
+
+    MODEL_TYPE = "amesim_pnch012"
+    MODEL_VERSION = "0.1.0"
+    PORTS = (
+        PortDefinition.pneumatic("port_1", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_2", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_3", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_4", nominal_role="bidirectional"),
+    )
+    PARAMETERS = (
+        AMESIM_GAS_INDEX_PARAMETER,
+        ParameterDefinition(
+            "cvol0",
+            0.015,
+            label="死容积",
+            quantity="volume",
+            unit="m3",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="变容气室在所有外部容积为零时仍保留的基础容积。",
+        ),
+        ParameterDefinition(
+            "kth",
+            0.0,
+            label="换热系数",
+            quantity="heat_transfer_coefficient",
+            unit="W/(m2*K)",
+            minimum=0.0,
+            description="气室与环境之间的对流换热系数，与换热面积共同决定换热功率。",
+        ),
+        ParameterDefinition(
+            "sth",
+            0.1,
+            label="换热面积",
+            quantity="area",
+            unit="m2",
+            minimum=0.0,
+            description="气室与环境进行热交换的有效表面积。",
+        ),
+        ParameterDefinition(
+            "extemp",
+            293.15,
+            label="外部温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="气室外部环境的绝对温度，用于计算气体与环境之间的换热。",
+        ),
+        ParameterDefinition(
+            "p0",
+            100000.0,
+            label="初始压力",
+            quantity="pressure",
+            unit="Pa",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="仿真开始时气室内气体的绝对压力。",
+        ),
+        ParameterDefinition(
+            "T0",
+            293.15,
+            label="初始温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+            description="仿真开始时气室内气体的绝对温度。",
+        ),
+        ParameterDefinition("vol1", 0.0, label="端口 1 外部容积", quantity="volume", unit="m3"),
+        ParameterDefinition("vol2", 0.0, label="端口 2 外部容积", quantity="volume", unit="m3"),
+        ParameterDefinition("vol3", 0.0, label="端口 3 外部容积", quantity="volume", unit="m3"),
+        ParameterDefinition("vol4", 0.0, label="端口 4 外部容积", quantity="volume", unit="m3"),
+        ParameterDefinition("dvol1", 0.0, label="端口 1 容积变化率", quantity="volume_flow", unit="m3/s"),
+        ParameterDefinition("dvol2", 0.0, label="端口 2 容积变化率", quantity="volume_flow", unit="m3/s"),
+        ParameterDefinition("dvol3", 0.0, label="端口 3 容积变化率", quantity="volume_flow", unit="m3/s"),
+        ParameterDefinition("dvol4", 0.0, label="端口 4 容积变化率", quantity="volume_flow", unit="m3/s"),
+    )
+    RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES + (
+        ResultVariableDefinition("vol", "气室总容积", "volume", "m3", "derived", 100),
+        ResultVariableDefinition("dvol", "总容积变化率", "volume_flow", "m3/s", "derived", 110),
+    )
+    DISPLAY = ComponentDisplaySpec(
+        label="PNCH012 变容气室",
+        library_id="amesim",
+        category_id="storage",
+        symbol="amesim_pnch012",
+        ports=(
+            PortDisplaySpec("port_1", "left", order=10),
+            PortDisplaySpec("port_2", "right", order=20),
+            PortDisplaySpec("port_3", "left", order=30),
+            PortDisplaySpec("port_4", "right", order=40),
+        ),
+        order=20,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: GasMedium,
+        *,
+        cvol0: float = 0.015,
+        kth: float = 0.0,
+        sth: float = 0.1,
+        extemp: float = 293.15,
+        gi: float = 1.0,
+        p0: float = 100000.0,
+        T0: float = 293.15,
+        vol1: float = 0.0,
+        vol2: float = 0.0,
+        vol3: float = 0.0,
+        vol4: float = 0.0,
+        dvol1: float = 0.0,
+        dvol2: float = 0.0,
+        dvol3: float = 0.0,
+        dvol4: float = 0.0,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values(
+            {
+                "cvol0": cvol0,
+                "kth": kth,
+                "sth": sth,
+                "extemp": extemp,
+                "gi": gi,
+                "p0": p0,
+                "T0": T0,
+                "vol1": vol1,
+                "vol2": vol2,
+                "vol3": vol3,
+                "vol4": vol4,
+                "dvol1": dvol1,
+                "dvol2": dvol2,
+                "dvol3": dvol3,
+                "dvol4": dvol4,
+            }
+        )
+        self.medium = medium
+        self.cvol0 = float(cvol0)
+        self.kth = float(kth)
+        self.sth = float(sth)
+        self.extemp = float(extemp)
+        self.gi = normalize_amesim_gas_index(gi)
+        self.p0 = float(p0)
+        self.T0 = float(T0)
+        self.external_volumes = {
+            "port_1": float(vol1),
+            "port_2": float(vol2),
+            "port_3": float(vol3),
+            "port_4": float(vol4),
+        }
+        self.external_volume_rates = {
+            "port_1": float(dvol1),
+            "port_2": float(dvol2),
+            "port_3": float(dvol3),
+            "port_4": float(dvol4),
+        }
+        if self.total_volume() <= 0.0:
+            raise ValueError("PNCH012 total volume must be positive.")
+        m0 = medium.density(self.p0, self.T0) * self.total_volume()
+        U0 = m0 * medium.specific_internal_energy_at_pressure(self.p0, self.T0)
+        self.state = VolumeState(m=m0, U=U0)
+        initial_h = medium.specific_enthalpy_at_pressure(self.p0, self.T0)
+        for port_name in ("port_1", "port_2", "port_3", "port_4"):
+            port = self.register_declared_port(port_name)
+            port.p = self.p0
+            port.h_outflow = initial_h
+            setattr(self, port_name, port)
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: GasMedium,
+        parameters: Mapping[str, float],
+    ) -> "AmesimPnch012":
+        return cls(name=name, medium=medium, **dict(parameters))
+
+    def connected_external_volume(self) -> float:
+        return sum(
+            getattr(getattr(self, port_name, None), "volume", 0.0)
+            for port_name in self.external_volumes
+        )
+
+    def connected_external_volume_rate(self) -> float:
+        return sum(
+            getattr(getattr(self, port_name, None), "volume_flow", 0.0)
+            for port_name in self.external_volume_rates
+        )
+
+    def total_volume(self) -> float:
+        minimum_volume = self.cvol0 / 100.0
+        return max(
+            self.cvol0 + sum(self.external_volumes.values()) + self.connected_external_volume(),
+            minimum_volume,
+        )
+
+    def total_volume_rate(self) -> float:
+        if self.total_volume() <= self.cvol0 / 100.0:
+            return 0.0
+        return sum(self.external_volume_rates.values()) + self.connected_external_volume_rate()
+
+    def get_state_vector(self) -> list[float]:
+        return self.state.as_vector()
+
+    def set_state_vector(self, values: list[float]) -> None:
+        self.state = VolumeState.from_vector(values)
+
+    def properties(self) -> ThermodynamicProperties:
+        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.total_volume())
+        for port_name in ("port_1", "port_2", "port_3", "port_4"):
+            port = self.get_port(port_name)
+            port.p = props.p
+            port.h_outflow = props.h
+        return props
+
+    def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
+        return self.properties()
+
+    def thermal_energy_flow_w(self, temperature: float) -> float:
+        return self.kth * self.sth * (self.extemp - temperature)
+
+    def component_result_values(self) -> Mapping[str, float]:
+        props = self.properties()
+        return {
+            "m": self.state.m,
+            "U": self.state.U,
+            "p": props.p,
+            "T": props.T,
+            "rho": props.rho,
+            "u": props.u,
+            "h": props.h,
+            "vol": self.total_volume(),
+            "dvol": self.total_volume_rate(),
+        }
+
+    def state_derivative_from_ports(self, connected_h: Mapping[str, float]) -> list[float]:
+        props = self.properties()
+        mass_derivative = 0.0
+        energy_derivative = 0.0
+        for port_name in ("port_1", "port_2", "port_3", "port_4"):
+            port = self.get_port(port_name)
+            inlet_h = self.connection_inlet_enthalpy(
+                port_m_flow=port.m_flow,
+                connected_h=connected_h[port_name],
+                internal_h=props.h,
+            )
+            mass_derivative += port.m_flow
+            energy_derivative += port.m_flow * inlet_h
+        energy_derivative += self.thermal_energy_flow_w(props.T)
+        energy_derivative -= props.p * self.total_volume_rate()
+        return VolumeState(m=mass_derivative, U=energy_derivative).as_vector()
+
+    def linearize_state_derivative(
+        self,
+        connected_h: Mapping[str, float],
+        *,
+        state_mass_tangent: Sequence[float],
+        state_energy_tangent: Sequence[float],
+        external_volume_tangent: Sequence[float],
+        external_volume_rate_tangent: Sequence[float],
+        port_mass_flow_tangents: Mapping[str, Sequence[float]],
+        connected_h_tangents: Mapping[str, Sequence[float]],
+        property_linearization: ThermodynamicPropertiesLinearization | None = None,
+        flow_boundary_tolerance: float = 1.0e-12,
+    ) -> Pnch012DerivativeLinearization:
+        """Linearize the chamber balance while keeping stream modes fixed."""
+
+        port_names = ("port_1", "port_2", "port_3", "port_4")
+        vectors = {
+            "state_mass": tuple(float(value) for value in state_mass_tangent),
+            "state_energy": tuple(float(value) for value in state_energy_tangent),
+            "volume": tuple(float(value) for value in external_volume_tangent),
+            "volume_rate": tuple(
+                float(value) for value in external_volume_rate_tangent
+            ),
+        }
+        for port_name in port_names:
+            vectors[f"flow:{port_name}"] = tuple(
+                float(value) for value in port_mass_flow_tangents[port_name]
+            )
+            vectors[f"enthalpy:{port_name}"] = tuple(
+                float(value) for value in connected_h_tangents[port_name]
+            )
+        widths = {len(values) for values in vectors.values()}
+        if len(widths) != 1:
+            raise ValueError("PNCH012 tangent vectors must have equal lengths.")
+        width = len(vectors["state_mass"])
+        invalid_reason: str | None = None
+        if not all(isfinite(value) for values in vectors.values() for value in values):
+            invalid_reason = "non_finite_tangent_input"
+
+        raw_volume = (
+            self.cvol0
+            + sum(self.external_volumes.values())
+            + self.connected_external_volume()
+        )
+        minimum_volume = self.cvol0 / 100.0
+        volume_scale = max(abs(raw_volume), abs(minimum_volume), 1.0e-18)
+        on_volume_boundary = (
+            abs(raw_volume - minimum_volume) <= 1.0e-12 * volume_scale
+        )
+        supplied_volume_tangent = vectors["volume"]
+        if raw_volume < minimum_volume or on_volume_boundary:
+            used_volume_tangent = (0.0,) * width
+            used_volume_rate_tangent = (0.0,) * width
+            if on_volume_boundary and any(
+                value != 0.0
+                for value in (
+                    *supplied_volume_tangent,
+                    *vectors["volume_rate"],
+                )
+            ):
+                invalid_reason = invalid_reason or "volume_floor_boundary"
+        else:
+            used_volume_tangent = supplied_volume_tangent
+            used_volume_rate_tangent = vectors["volume_rate"]
+
+        properties = property_linearization or self.medium.linearize_properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.total_volume(),
+            vectors["state_mass"],
+            vectors["state_energy"],
+            used_volume_tangent,
+        )
+        if properties.tangents.width != width:
+            raise ValueError(
+                "PNCH012 property tangent width must match balance tangents."
+            )
+        props = properties.properties
+        if not properties.valid:
+            invalid_reason = invalid_reason or properties.reason
+
+        mass_derivative = sum(
+            self.get_port(port_name).m_flow for port_name in port_names
+        )
+        volume_rate = self.total_volume_rate()
+        energy_derivative = self.thermal_energy_flow_w(props.T) - props.p * volume_rate
+        mass_tangent = [0.0] * width
+        energy_tangent = [
+            -self.kth * self.sth * properties.tangents.T[index]
+            - volume_rate * properties.tangents.p[index]
+            - props.p * used_volume_rate_tangent[index]
+            for index in range(width)
+        ]
+
+        for port_name in port_names:
+            port = self.get_port(port_name)
+            flow_tangent = vectors[f"flow:{port_name}"]
+            if (
+                abs(port.m_flow) <= flow_boundary_tolerance
+                and any(value != 0.0 for value in flow_tangent)
+            ):
+                invalid_reason = invalid_reason or (
+                    f"flow_direction_boundary:{port_name}"
+                )
+            if port.m_flow > 0.0:
+                inlet_h = connected_h[port_name]
+                inlet_h_tangent = vectors[f"enthalpy:{port_name}"]
+            else:
+                inlet_h = props.h
+                inlet_h_tangent = properties.tangents.h
+            energy_derivative += port.m_flow * inlet_h
+            for index in range(width):
+                mass_tangent[index] += flow_tangent[index]
+                energy_tangent[index] += (
+                    inlet_h * flow_tangent[index]
+                    + port.m_flow * inlet_h_tangent[index]
+                )
+
+        return Pnch012DerivativeLinearization(
+            derivative=(mass_derivative, energy_derivative),
+            tangents=(tuple(mass_tangent), tuple(energy_tangent)),
+            properties=properties,
+            valid=invalid_reason is None,
+            reason=invalid_reason,
+        )
+
+    def pressure_flow_equation_values(self) -> tuple[float, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.total_volume(),
+        ).p
+        return tuple(
+            self.get_port(port_name).p - pressure
+            for port_name in ("port_1", "port_2", "port_3", "port_4")
+        )
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.total_volume(),
+        ).p
+        return tuple(
+            EquationResidual(
+                id=f"{self.name}:{port_name}_pressure_state",
+                owner="component",
+                owner_id=self.name,
+                relation="state",
+                variables=(f"{self.name}.{port_name}.p", f"{self.name}.state"),
+                role="effort",
+                value=self.get_port(port_name).p - pressure,
+            )
+            for port_name in ("port_1", "port_2", "port_3", "port_4")
+        )

app/simulation/components/example.md

@@ -0,0 +1,282 @@
+# 元件建模规范与示例
+
+规范的权威版本位于
+[`docs/standard/component-model-authoring-spec-v1.md`](../../../docs/standard/component-model-authoring-spec-v1.md)。
+本文档保留在组件目录中，作为离模型源码最近的完整示例；若两者不一致，应在同一次
+修改中同步，不能让示例形成另一套规则。
+
+本文档是 `app/simulation/components` 下新增元件的最小开发规范。当前
+`experimental` 是用于验证规范的临时组件库；后续正式模型应建立独立组件库，
+不要继续堆放在 `experimental` 中。
+
+目标是让元件的端口、输入参数和可展示结果都由元件类显式声明，避免 XML
+校验、求解器和前端分别维护同一份含义。
+
+## 一、元件类必须声明的内容
+
+每个对外注册的元件类至少需要声明以下六个类属性：
+
+```python
+MODEL_TYPE = "example_component"
+MODEL_VERSION = "1.0.0"
+PORTS = (...)
+PARAMETERS = (...)
+RESULT_VARIABLES = (...)
+DISPLAY = ...
+```
+
+- `MODEL_TYPE`：稳定的模型类型标识，对应 System XML 中的 `Component/@type`。发布后不要随意改名。
+- `MODEL_VERSION`：模型契约版本，采用 `主版本.次版本.修订版本`。
+- `PORTS`：端口契约，包括端口名、物理域、变量和正流量方向。
+- `PARAMETERS`：用户可配置的输入参数，包括默认值、物理量、SI 单位和取值范围。
+- `RESULT_VARIABLES`：允许写入仿真结果并显示在结果页的组件级变量。端口结果由 `PORTS` 中的端口变量定义自动生成。
+- `DISPLAY`：组件库名称、分类、图标、排序和端口画布位置，不参与物理求解。
+
+元件构造函数还必须：
+
+1. 调用 `super().__init__(name)`。
+2. 使用 `set_parameter_values()` 保存规范化后的输入参数。
+3. 使用 `register_declared_port()` 创建已声明端口。
+4. 若声明了组件结果变量，实现 `component_result_values()` 并返回对应数值；标准热力学容腔可以直接继承 `ThermodynamicVolumeComponent` 的实现。
+5. 实现统一的类方法 `create()`，接收规范化后的 SI 参数。
+
+## 二、输入参数与结果变量
+
+输入参数和仿真结果必须分开声明：
+
+- 输入参数描述一次仿真开始前由用户配置的量，例如 `volume`、`p0`、`T0`。
+- 结果变量描述随时间变化、允许绘图的量，例如 `p`、`T`、`m`、`m_flow`。
+- 求解器缓存、中间残差和调试字段不得自动暴露为结果变量。
+- 参数名和结果变量名使用稳定的英文机器标识；`label` 专门用于界面显示。
+
+参数定义示例：
+
+```python
+ParameterDefinition(
+    name="volume",
+    label="容积",
+    quantity="volume",
+    unit="m3",
+    default=0.1,
+    minimum=0.0,
+    minimum_exclusive=True,
+)
+```
+
+结果变量定义示例：
+
+```python
+ResultVariableDefinition(
+    name="p",
+    label="压力",
+    quantity="pressure",
+    unit="Pa",
+    category="thermodynamic",
+    order=30,
+)
+```
+
+## 三、命名和单位约定
+
+- 模型类型、参数、端口和变量名使用 `snake_case`，已有热力学惯例 `T`、`U` 可以保留。
+- 输入参数保存和计算统一使用 SI 基准值；界面单位换算不能改变后端存储值。
+- 无量纲参数的 `unit` 使用空字符串。
+- `quantity` 表示稳定的物理量类型，例如 `pressure`、`temperature`、`mass_flow`，不能使用界面文案代替。
+- 正质量流量统一定义为流入元件，即 `positiveFlowDirection="intoComponent"`。
+- 端口变量 `p`、`m_flow`、`h_outflow` 的连接规则由 `PortDefinition.pneumatic()` 统一提供。
+
+## 四、完整示例：单端口储气容腔
+
+下面的示例展示一个可直接接入当前框架的动态元件。真实新增元件时应放入独立的 `.py` 文件，并补充对应测试。
+
+```python
+from __future__ import annotations
+
+from collections.abc import Mapping
+
+from app.simulation.core.base import ThermodynamicVolumeComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import (
+    ParameterDefinition,
+    THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
+)
+from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
+from app.simulation.core.ports import PortDefinition
+from app.simulation.core.state import VolumeState
+
+
+class ExampleVolume(ThermodynamicVolumeComponent):
+    MODEL_TYPE = "example_volume"
+    MODEL_VERSION = "1.0.0"
+    PORTS = (
+        PortDefinition.pneumatic("port_a", nominal_role="bidirectional"),
+    )
+    PARAMETERS = (
+        ParameterDefinition(
+            name="volume",
+            label="容积",
+            quantity="volume",
+            unit="m3",
+            default=0.1,
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            name="p0",
+            label="初始压力",
+            quantity="pressure",
+            unit="Pa",
+            default=100000.0,
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            name="T0",
+            label="初始温度",
+            quantity="temperature",
+            unit="K",
+            default=300.0,
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+    )
+    RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
+    DISPLAY = ComponentDisplaySpec(
+        label="示例容腔",
+        library_id="experimental",
+        category_id="storage",
+        symbol="generic",
+        ports=(PortDisplaySpec("port_a", "left"),),
+        order=90,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: IdealGasMedium,
+        volume: float = 0.1,
+        p0: float = 100000.0,
+        T0: float = 300.0,
+    ) -> None:
+        super().__init__(name)
+        self.set_parameter_values(
+            {"volume": volume, "p0": p0, "T0": T0}
+        )
+        self.medium = medium
+        self.V = volume
+        initial_mass = p0 * volume / (medium.R_gas * T0)
+        initial_energy = initial_mass * medium.specific_internal_energy(T0)
+        self.state = VolumeState(m=initial_mass, U=initial_energy)
+        self.port_a = self.register_declared_port("port_a")
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> ExampleVolume:
+        return cls(
+            name=name,
+            medium=medium,
+            volume=parameters["volume"],
+            p0=parameters["p0"],
+            T0=parameters["T0"],
+        )
+
+    def get_state_vector(self) -> list[float]:
+        return self.state.as_vector()
+
+    def set_state_vector(self, values: list[float]) -> None:
+        self.state = VolumeState.from_vector(values)
+
+    def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
+        properties = self.medium.properties_from_mU(
+            self.state.m, self.state.U, self.V
+        )
+        self.port_a.p = properties.p
+        self.port_a.h_outflow = properties.h
+        return properties
+
+    def state_derivative_from_ports(
+        self,
+        connected_h: Mapping[str, float],
+    ) -> list[float]:
+        properties = self.refresh_thermodynamic_ports()
+        inlet_h = self.connection_inlet_enthalpy(
+            port_m_flow=self.port_a.m_flow,
+            connected_h=connected_h["port_a"],
+            internal_h=properties.h,
+        )
+        return [self.port_a.m_flow, self.port_a.m_flow * inlet_h]
+
+    def pressure_flow_equation_residuals(
+        self,
+    ) -> tuple[EquationResidual, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m, self.state.U, self.V
+        ).p
+        return (
+            EquationResidual(
+                id=f"{self.name}:port_a_pressure_state",
+                owner="component",
+                owner_id=self.name,
+                relation="state",
+                variables=(f"{self.name}.port_a.p", f"{self.name}.state"),
+                role="effort",
+                value=self.port_a.p - pressure,
+            ),
+        )
+```
+
+模型文件不再直接修改全局注册表。完成模型类后，只把类路径加入所属库
+`library.py` 的 `models` 清单：
+
+```python
+models=(
+    # ...已有模型
+    "app.simulation.components.experimental.storage.example_volume:ExampleVolume",
+)
+```
+
+后端会受控导入清单中的类，校验版本、分类、端口、参数、单位、显示信息和默认实例，
+再自动建立注册表。校验通过后，`GET /api/components/catalog` 会输出该元件，
+前端刷新时即可加载。
+当前 `experimental` 仅用于规范验证；正式模型应先建立新的库声明，再把
+`library_id` 指向正式库。
+
+完成仿真后，每个已声明结果都会得到一条结构化元数据。前端应按字段筛选，不能再拆解 `key` 猜测含义：
+
+```json
+{
+  "key": "example_volume_1.port_a.m_flow",
+  "componentId": "example_volume_1",
+  "componentType": "example_volume",
+  "scope": "port",
+  "portName": "port_a",
+  "name": "m_flow",
+  "label": "质量流量",
+  "quantity": "mass_flow",
+  "unit": "kg/s",
+  "category": "flow",
+  "order": 20
+}
+```
+
+## 五、新增元件检查清单
+
+1. `MODEL_TYPE` 是否唯一，并与 XML 的模型类型一致。
+2. 所有构造参数是否在 `PARAMETERS` 中声明并保存。
+3. 所有端口是否在 `PORTS` 中声明并通过 `register_declared_port()` 创建。
+4. `RESULT_VARIABLES` 与 `component_result_values()` 的键是否完全一致。
+5. 结果变量是否包含明确的 `quantity`、`label`、`unit` 和显示顺序。
+6. 是否只暴露有工程意义的结果，而非内部计算变量。
+7. `MODEL_VERSION` 和 `DISPLAY` 是否完整，显示端口是否与物理端口完全一致。
+8. 是否实现统一的 `create()`，并能用默认参数创建模型。
+9. 模型类路径是否只加入所属库的 `library.py` 清单。
+10. 是否补充参数边界、端口契约、目录输出、结果元数据和最小仿真的自动测试。
+
+组件库、分类和自动发现的完整规则参见
+[`组件库分类、发现与读取规范 v1`](../../../docs/standard/component-library-spec-v1.md)。

app/simulation/components/experimental/__init__.py

@@ -0,0 +1,3 @@
+"""Temporary component library used to validate the model authoring contract."""
+
+from app.simulation.components.experimental.library import LIBRARY

app/simulation/components/experimental/flow/__init__.py

@@ -0,0 +1 @@
+"""Flow-path and resistance components."""

app/simulation/components/experimental/flow/orifice.py

@@ -0,0 +1,121 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+from math import sqrt
+
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import ParameterDefinition
+from app.simulation.core.medium import IdealGasMedium
+from app.simulation.core.ports import PortDefinition
+
+
+class Orifice(AlgebraicComponent):
+    """Python port of ModelicaModels.Myorifice."""
+
+    MODEL_TYPE = "orifice"
+    MODEL_VERSION = "1.0.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
+        ("mass_flow_balance",)
+    )
+    PORTS = (
+        PortDefinition.pneumatic("port_a", nominal_role="inlet"),
+        PortDefinition.pneumatic("port_b", nominal_role="outlet"),
+    )
+    PARAMETERS = (
+        ParameterDefinition(
+            "K",
+            1e-5,
+            label="流量系数",
+            quantity="flow_coefficient",
+            unit="kg/(s*Pa^0.5)",
+            minimum=0.0,
+        ),
+        ParameterDefinition(
+            "opening",
+            1.0,
+            label="开度",
+            minimum=0.0,
+            maximum=1.0,
+        ),
+    )
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="孔板/阀门",
+        library_id="experimental",
+        category_id="flow",
+        symbol="orifice",
+        ports=(
+            PortDisplaySpec("port_a", "left", order=10),
+            PortDisplaySpec("port_b", "right", order=20),
+        ),
+        order=40,
+    )
+
+    def __init__(self, name: str, opening: float = 1.0, K: float = 1e-5) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({"K": K, "opening": opening})
+        self.opening = opening
+        self.K = K
+        self.port_a = self.register_declared_port("port_a")
+        self.port_b = self.register_declared_port("port_b")
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> Orifice:
+        return cls(
+            name=name,
+            opening=parameters["opening"],
+            K=parameters["K"],
+        )
+
+    @property
+    def K_eff(self) -> float:
+        return self.K * max(self.opening, 0.001)
+
+    def mass_flow(self, p_a: float, p_b: float) -> float:
+        dp = p_a - p_b
+        if dp == 0.0:
+            return 0.0
+        return self.K_eff * sqrt(abs(dp)) * (1.0 if dp > 0.0 else -1.0)
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        return (
+            EquationResidual(
+                id=f"{self.name}:mass_flow_balance",
+                owner="component",
+                owner_id=self.name,
+                relation="sumToZero",
+                variables=(
+                    f"{self.name}.port_a.m_flow",
+                    f"{self.name}.port_b.m_flow",
+                ),
+                role="flow",
+                value=self.port_a.m_flow + self.port_b.m_flow,
+            ),
+            EquationResidual(
+                id=f"{self.name}:pressure_flow_relation",
+                owner="component",
+                owner_id=self.name,
+                relation="constitutive",
+                variables=(
+                    f"{self.name}.port_a.p",
+                    f"{self.name}.port_b.p",
+                    f"{self.name}.port_a.m_flow",
+                ),
+                role="flow",
+                value=self.port_a.m_flow
+                - self.mass_flow(self.port_a.p, self.port_b.p),
+            ),
+        )
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        self.port_a.h_outflow = connected_h["port_b"]
+        self.port_b.h_outflow = connected_h["port_a"]

app/simulation/components/experimental/flow/pipe.py

@@ -0,0 +1,10 @@
+"""Compatibility import for the TestModel-only dynamic pipe.
+
+The public ``pipe`` catalog model is ``ResistivePipe``. New code should import
+this legacy dynamic model from ``app.simulation.examples.testmodel.dynamic_pipe``.
+"""
+
+from app.simulation.examples.testmodel.dynamic_pipe import Pipe
+
+
+__all__ = ("Pipe",)

app/simulation/components/experimental/flow/resistive_pipe.py

@@ -0,0 +1,189 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+from math import pi
+
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import ParameterDefinition
+from app.simulation.core.medium import IdealGasMedium
+from app.simulation.core.ports import PortDefinition
+
+
+class ResistivePipe(AlgebraicComponent):
+    """Quasi-steady Darcy resistance used by topology-driven simulation."""
+
+    MODEL_TYPE = "pipe"
+    MODEL_VERSION = "1.0.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
+        ("mass_flow_balance",)
+    )
+    PORTS = (
+        PortDefinition.pneumatic("port_a", nominal_role="inlet"),
+        PortDefinition.pneumatic("port_b", nominal_role="outlet"),
+    )
+    PARAMETERS = (
+        ParameterDefinition(
+            "length",
+            5.0,
+            label="长度",
+            quantity="length",
+            unit="m",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "diameter",
+            0.02,
+            label="直径",
+            quantity="length",
+            unit="m",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "lambda_darcy",
+            0.02,
+            label="摩阻系数",
+            minimum=0.0,
+        ),
+        ParameterDefinition(
+            "p0",
+            1e5,
+            label="初始压力",
+            quantity="pressure",
+            unit="Pa",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "T0",
+            300.0,
+            label="初始温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+    )
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="管段",
+        library_id="experimental",
+        category_id="flow",
+        symbol="pipe",
+        ports=(
+            PortDisplaySpec("port_a", "left", order=10),
+            PortDisplaySpec("port_b", "right", order=20),
+        ),
+        order=30,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: IdealGasMedium,
+        L: float = 5.0,
+        D: float = 0.02,
+        lambda_darcy: float = 0.02,
+        p0: float = 1e5,
+        T0: float = 300.0,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values(
+            {
+                "length": L,
+                "diameter": D,
+                "lambda_darcy": lambda_darcy,
+                "p0": p0,
+                "T0": T0,
+            }
+        )
+        self.medium = medium
+        self.L = L
+        self.D = D
+        self.lambda_darcy = lambda_darcy
+        self.p0 = p0
+        self.T0 = T0
+        self.area = pi * D * D / 4.0
+        initial_h = medium.specific_enthalpy(T0)
+
+        self.port_a = self.register_declared_port("port_a")
+        self.port_a.p = p0
+        self.port_a.h_outflow = initial_h
+
+        self.port_b = self.register_declared_port("port_b")
+        self.port_b.p = p0
+        self.port_b.h_outflow = initial_h
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> ResistivePipe:
+        return cls(
+            name=name,
+            medium=medium,
+            L=parameters["length"],
+            D=parameters["diameter"],
+            lambda_darcy=parameters["lambda_darcy"],
+            p0=parameters["p0"],
+            T0=parameters["T0"],
+        )
+
+    def pressure_drop(self, m_flow_a: float, p_a: float, p_b: float) -> float:
+        average_pressure = max(0.5 * (p_a + p_b), 1.0)
+        density = max(self.medium.density(average_pressure, self.T0), 1e-12)
+        resistance = self.lambda_darcy * (self.L / self.D)
+        return (
+            resistance
+            * m_flow_a
+            * abs(m_flow_a)
+            / (2.0 * density * self.area * self.area)
+        )
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        return (
+            EquationResidual(
+                id=f"{self.name}:mass_flow_balance",
+                owner="component",
+                owner_id=self.name,
+                relation="sumToZero",
+                variables=(
+                    f"{self.name}.port_a.m_flow",
+                    f"{self.name}.port_b.m_flow",
+                ),
+                role="flow",
+                value=self.port_a.m_flow + self.port_b.m_flow,
+            ),
+            EquationResidual(
+                id=f"{self.name}:darcy_pressure_loss",
+                owner="component",
+                owner_id=self.name,
+                relation="constitutive",
+                variables=(
+                    f"{self.name}.port_a.p",
+                    f"{self.name}.port_b.p",
+                    f"{self.name}.port_a.m_flow",
+                ),
+                role="effort",
+                value=(
+                    self.port_a.p
+                    - self.port_b.p
+                    - self.pressure_drop(
+                        self.port_a.m_flow,
+                        self.port_a.p,
+                        self.port_b.p,
+                    )
+                ),
+            ),
+        )
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        self.port_a.h_outflow = connected_h["port_b"]
+        self.port_b.h_outflow = connected_h["port_a"]

app/simulation/components/experimental/junctions/__init__.py

@@ -0,0 +1 @@
+"""Flow junction components."""

app/simulation/components/experimental/junctions/tee.py

@@ -1,17 +1,115 @@
 from __future__ import annotations
 
-from PythonModels.core.base import AlgebraicComponent
+from collections.abc import Mapping
-from PythonModels.core.ports import PortState
+
+from app.simulation.core.base import AlgebraicComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.medium import IdealGasMedium
+from app.simulation.core.ports import PortDefinition
 
 
 class Tee(AlgebraicComponent):
     """Python port of ModelicaModels.Mytee."""
 
+    MODEL_TYPE = "tee"
+    MODEL_VERSION = "1.0.0"
+    PRESSURE_FLOW_DEPENDS_ON_STREAM = False
+    PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES = frozenset(
+        ("mass_flow_balance",)
+    )
+    PORTS = (
+        PortDefinition.pneumatic("port_in", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_out1", nominal_role="bidirectional"),
+        PortDefinition.pneumatic("port_out2", nominal_role="bidirectional"),
+    )
+    PARAMETERS = ()
+    RESULT_VARIABLES = ()
+    DISPLAY = ComponentDisplaySpec(
+        label="三通",
+        library_id="experimental",
+        category_id="junctions",
+        symbol="tee",
+        ports=(
+            PortDisplaySpec("port_in", "left", order=10),
+            PortDisplaySpec("port_out1", "right", order=20),
+            PortDisplaySpec("port_out2", "right", order=30),
+        ),
+        order=50,
+    )
+
     def __init__(self, name: str) -> None:
         super().__init__(name=name)
-        self.port_in = PortState()
+        self.set_parameter_values({})
-        self.port_out1 = PortState()
+        self.port_in = self.register_declared_port("port_in")
-        self.port_out2 = PortState()
+        self.port_out1 = self.register_declared_port("port_out1")
+        self.port_out2 = self.register_declared_port("port_out2")
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> Tee:
+        return cls(name=name)
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        return (
+            EquationResidual(
+                id=f"{self.name}:common_pressure_out1",
+                owner="component",
+                owner_id=self.name,
+                relation="equal",
+                variables=(f"{self.name}.port_in.p", f"{self.name}.port_out1.p"),
+                role="effort",
+                value=self.port_in.p - self.port_out1.p,
+            ),
+            EquationResidual(
+                id=f"{self.name}:common_pressure_out2",
+                owner="component",
+                owner_id=self.name,
+                relation="equal",
+                variables=(f"{self.name}.port_in.p", f"{self.name}.port_out2.p"),
+                role="effort",
+                value=self.port_in.p - self.port_out2.p,
+            ),
+            EquationResidual(
+                id=f"{self.name}:mass_flow_balance",
+                owner="component",
+                owner_id=self.name,
+                relation="sumToZero",
+                variables=(
+                    f"{self.name}.port_in.m_flow",
+                    f"{self.name}.port_out1.m_flow",
+                    f"{self.name}.port_out2.m_flow",
+                ),
+                role="flow",
+                value=(
+                    self.port_in.m_flow
+                    + self.port_out1.m_flow
+                    + self.port_out2.m_flow
+                ),
+            ),
+        )
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        incoming = [
+            (port.m_flow, connected_h[name])
+            for name, port in self.ports.items()
+            if port.m_flow > 1e-12
+        ]
+        total_flow = sum(m_flow for m_flow, _ in incoming)
+        if total_flow > 1e-12:
+            mixed_h = sum(
+                m_flow * enthalpy for m_flow, enthalpy in incoming
+            ) / total_flow
+        else:
+            values = list(connected_h.values())
+            mixed_h = sum(values) / len(values) if values else 0.0
+        for port in self.ports.values():
+            port.h_outflow = mixed_h
 
     def mixed_inlet_enthalpy(
         self,

app/simulation/components/experimental/library.py

@@ -0,0 +1,28 @@
+"""Manifest for the temporary library used to validate component authoring."""
+
+from app.simulation.core.catalog import (
+    ComponentCategorySpec,
+    ComponentLibrarySpec,
+)
+
+
+LIBRARY = ComponentLibrarySpec(
+    id="experimental",
+    label="临时测试组件库",
+    version="0.1.0",
+    source_package="app.simulation.components.experimental",
+    temporary=True,
+    order=100,
+    categories=(
+        ComponentCategorySpec(id="storage", label="储能元件", order=10),
+        ComponentCategorySpec(id="flow", label="流动元件", order=20),
+        ComponentCategorySpec(id="junctions", label="连接元件", order=30),
+    ),
+    models=(
+        "app.simulation.components.experimental.storage.cylinder:Cylinder",
+        "app.simulation.components.experimental.storage.tank:Tank",
+        "app.simulation.components.experimental.flow.resistive_pipe:ResistivePipe",
+        "app.simulation.components.experimental.flow.orifice:Orifice",
+        "app.simulation.components.experimental.junctions.tee:Tee",
+    ),
+)

app/simulation/components/experimental/storage/__init__.py

@@ -0,0 +1 @@
+"""Storage and thermodynamic volume components."""

app/simulation/components/experimental/storage/cylinder.py

@@ -0,0 +1,155 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+
+from app.simulation.core.base import ThermodynamicVolumeComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import (
+    ParameterDefinition,
+    THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
+)
+from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
+from app.simulation.core.ports import PortDefinition
+from app.simulation.core.state import VolumeState
+
+
+class Cylinder(ThermodynamicVolumeComponent):
+    """Python port of ModelicaModels.Mycylinder."""
+
+    MODEL_TYPE = "cylinder"
+    MODEL_VERSION = "1.0.0"
+    PORTS = (PortDefinition.pneumatic("port_b", nominal_role="outlet"),)
+    PARAMETERS = (
+        ParameterDefinition(
+            "volume",
+            0.01,
+            label="容积",
+            quantity="volume",
+            unit="m3",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "p0",
+            35e6,
+            label="初始压力",
+            quantity="pressure",
+            unit="Pa",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "T0",
+            300.0,
+            label="初始温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+    )
+    RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
+    DISPLAY = ComponentDisplaySpec(
+        label="气瓶",
+        library_id="experimental",
+        category_id="storage",
+        symbol="cylinder",
+        ports=(PortDisplaySpec("port_b", "right"),),
+        order=10,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: IdealGasMedium,
+        V: float = 0.01,
+        p0: float = 35e6,
+        T0: float = 300.0,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({"volume": V, "p0": p0, "T0": T0})
+        self.medium = medium
+        self.V = V
+        m0 = p0 * V / (medium.R_gas * T0)
+        U0 = m0 * medium.specific_internal_energy(T0)
+        self.state = VolumeState(m=m0, U=U0)
+        self.port_b = self.register_declared_port("port_b")
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> Cylinder:
+        return cls(
+            name=name,
+            medium=medium,
+            V=parameters["volume"],
+            p0=parameters["p0"],
+            T0=parameters["T0"],
+        )
+
+    def get_state_vector(self) -> list[float]:
+        return self.state.as_vector()
+
+    def set_state_vector(self, values: list[float]) -> None:
+        self.state = VolumeState.from_vector(values)
+
+    def properties(self) -> ThermodynamicProperties:
+        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
+        self.port_b.p = props.p
+        self.port_b.h_outflow = props.h
+        return props
+
+    def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
+        return self.properties()
+
+    def state_derivative_from_ports(
+        self,
+        connected_h: Mapping[str, float],
+    ) -> list[float]:
+        properties = self.properties()
+        derivative = self.derivatives_from_connection(
+            connected_h=connected_h["port_b"],
+            port_m_flow=self.port_b.m_flow,
+            internal_h=properties.h,
+        )
+        return derivative.as_vector()
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.V,
+        ).p
+        return (
+            EquationResidual(
+                id=f"{self.name}:port_b_pressure_state",
+                owner="component",
+                owner_id=self.name,
+                relation="state",
+                variables=(f"{self.name}.port_b.p", f"{self.name}.state"),
+                role="effort",
+                value=self.port_b.p - pressure,
+            ),
+        )
+
+    def derivatives_from_connection(
+        self,
+        *,
+        connected_h: float,
+        port_m_flow: float,
+        internal_h: float,
+    ) -> VolumeState:
+        inlet_h = self.connection_inlet_enthalpy(
+            port_m_flow=port_m_flow,
+            connected_h=connected_h,
+            internal_h=internal_h,
+        )
+        return self.derivatives(inlet_h, port_m_flow)
+
+    def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
+        return VolumeState(m=m_flow, U=m_flow * inlet_h)

app/simulation/components/experimental/storage/tank.py

@@ -0,0 +1,155 @@
+from __future__ import annotations
+
+from collections.abc import Mapping
+
+from app.simulation.core.base import ThermodynamicVolumeComponent
+from app.simulation.core.catalog import ComponentDisplaySpec, PortDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import (
+    ParameterDefinition,
+    THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
+)
+from app.simulation.core.medium import IdealGasMedium, ThermodynamicProperties
+from app.simulation.core.ports import PortDefinition
+from app.simulation.core.state import VolumeState
+
+
+class Tank(ThermodynamicVolumeComponent):
+    """Python port of ModelicaModels.Mytank."""
+
+    MODEL_TYPE = "tank"
+    MODEL_VERSION = "1.0.0"
+    PORTS = (PortDefinition.pneumatic("port_a", nominal_role="inlet"),)
+    PARAMETERS = (
+        ParameterDefinition(
+            "volume",
+            0.1,
+            label="容积",
+            quantity="volume",
+            unit="m3",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "p0",
+            1e5,
+            label="初始压力",
+            quantity="pressure",
+            unit="Pa",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+        ParameterDefinition(
+            "T0",
+            300.0,
+            label="初始温度",
+            quantity="temperature",
+            unit="K",
+            minimum=0.0,
+            minimum_exclusive=True,
+        ),
+    )
+    RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
+    DISPLAY = ComponentDisplaySpec(
+        label="贮箱",
+        library_id="experimental",
+        category_id="storage",
+        symbol="tank",
+        ports=(PortDisplaySpec("port_a", "left"),),
+        order=20,
+    )
+
+    def __init__(
+        self,
+        name: str,
+        medium: IdealGasMedium,
+        V: float = 0.1,
+        p0: float = 1e5,
+        T0: float = 300.0,
+    ) -> None:
+        super().__init__(name=name)
+        self.set_parameter_values({"volume": V, "p0": p0, "T0": T0})
+        self.medium = medium
+        self.V = V
+        m0 = p0 * V / (medium.R_gas * T0)
+        U0 = m0 * medium.specific_internal_energy(T0)
+        self.state = VolumeState(m=m0, U=U0)
+        self.port_a = self.register_declared_port("port_a")
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: IdealGasMedium,
+        parameters: Mapping[str, float],
+    ) -> Tank:
+        return cls(
+            name=name,
+            medium=medium,
+            V=parameters["volume"],
+            p0=parameters["p0"],
+            T0=parameters["T0"],
+        )
+
+    def get_state_vector(self) -> list[float]:
+        return self.state.as_vector()
+
+    def set_state_vector(self, values: list[float]) -> None:
+        self.state = VolumeState.from_vector(values)
+
+    def properties(self) -> ThermodynamicProperties:
+        props = self.medium.properties_from_mU(self.state.m, self.state.U, self.V)
+        self.port_a.p = props.p
+        self.port_a.h_outflow = props.h
+        return props
+
+    def refresh_thermodynamic_ports(self) -> ThermodynamicProperties:
+        return self.properties()
+
+    def state_derivative_from_ports(
+        self,
+        connected_h: Mapping[str, float],
+    ) -> list[float]:
+        properties = self.properties()
+        derivative = self.derivatives_from_connection(
+            connected_h=connected_h["port_a"],
+            port_m_flow=self.port_a.m_flow,
+            internal_h=properties.h,
+        )
+        return derivative.as_vector()
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        pressure = self.medium.properties_from_mU(
+            self.state.m,
+            self.state.U,
+            self.V,
+        ).p
+        return (
+            EquationResidual(
+                id=f"{self.name}:port_a_pressure_state",
+                owner="component",
+                owner_id=self.name,
+                relation="state",
+                variables=(f"{self.name}.port_a.p", f"{self.name}.state"),
+                role="effort",
+                value=self.port_a.p - pressure,
+            ),
+        )
+
+    def derivatives_from_connection(
+        self,
+        *,
+        connected_h: float,
+        port_m_flow: float,
+        internal_h: float,
+    ) -> VolumeState:
+        inlet_h = self.connection_inlet_enthalpy(
+            port_m_flow=port_m_flow,
+            connected_h=connected_h,
+            internal_h=internal_h,
+        )
+        return self.derivatives(inlet_h, port_m_flow)
+
+    def derivatives(self, inlet_h: float, m_flow: float) -> VolumeState:
+        return VolumeState(m=m_flow, U=m_flow * inlet_h)

app/simulation/core/base.py

@@ -0,0 +1,365 @@
+from __future__ import annotations
+
+from abc import ABC, abstractmethod
+from collections.abc import Callable, Mapping
+from typing import TYPE_CHECKING, Any, ClassVar
+
+from app.simulation.core.catalog import ComponentDisplaySpec
+from app.simulation.core.equations import EquationResidual
+from app.simulation.core.metadata import (
+    ParameterDefinition,
+    ResultVariableDefinition,
+    ResultVariableMetadata,
+    THERMODYNAMIC_VOLUME_RESULT_VARIABLES,
+)
+from app.simulation.core.ports import PortDefinition, PortState
+
+if TYPE_CHECKING:
+    from app.simulation.core.medium import GasMedium
+
+
+class Component(ABC):
+    MODEL_TYPE: ClassVar[str | None] = None
+    MODEL_VERSION: ClassVar[str | None] = None
+    # ``True`` means that pressure/flow residuals read values written by
+    # ``update_stream_outflows`` or ``update_flow_temperature_references``.
+    # ``False`` is an explicit promise that those residuals are independent of
+    # stream propagation.  ``None`` keeps custom components conservative: when
+    # they override either stream hook, the closure planner retains the legacy
+    # full-network thermofluid fixed point.
+    PRESSURE_FLOW_DEPENDS_ON_STREAM: ClassVar[bool | None] = None
+    # Exact residual suffixes whose declared variables are summed, in order,
+    # to form a ``sumToZero`` flow equation.  The causal solver deliberately
+    # reads this capability from the concrete class ``__dict__``: subclasses
+    # must repeat the promise after changing any equation semantics.
+    PRESSURE_FLOW_EXACT_SUM_TO_ZERO_EQUATION_SUFFIXES: ClassVar[
+        frozenset[str]
+    ] = frozenset()
+    PORTS: ClassVar[tuple[PortDefinition, ...]] = ()
+    PARAMETERS: ClassVar[tuple[ParameterDefinition, ...]] = ()
+    RESULT_VARIABLES: ClassVar[tuple[ResultVariableDefinition, ...]] = ()
+    DISPLAY: ClassVar[ComponentDisplaySpec | None] = None
+
+    def __init__(self, name: str) -> None:
+        self.name = name
+        self.model_type = self.MODEL_TYPE or self.__class__.__name__.lower()
+        self._ports: dict[str, PortState] = {}
+        self._parameter_values: dict[str, float] = {}
+
+    @property
+    def ports(self) -> dict[str, PortState]:
+        return dict(self._ports)
+
+    @property
+    def port_definitions(self) -> tuple[PortDefinition, ...]:
+        return tuple(
+            port.definition
+            for port in self._ports.values()
+            if port.definition is not None
+        )
+
+    @classmethod
+    def active_port_definitions_for_parameters(
+        cls,
+        parameters: Mapping[str, float],
+    ) -> tuple[PortDefinition, ...]:
+        """Declared ports enabled by one normalized parameter set."""
+
+        return cls.PORTS
+
+    @property
+    def active_port_definitions(self) -> tuple[PortDefinition, ...]:
+        """Instance ports that participate in execution and result reporting."""
+
+        return self.port_definitions
+
+    @property
+    def required_connection_ports(self) -> tuple[str, ...]:
+        """Physical ports that must have an external connection before simulation."""
+
+        return tuple(
+            definition.name
+            for definition in self.active_port_definitions
+            if definition.kind == "physical"
+        )
+
+    def register_port(self, port: PortState) -> PortState:
+        definition = port.definition
+        if definition is None:
+            raise ValueError(f"Component {self.name} cannot register an undefined port.")
+        if definition.name in self._ports:
+            raise ValueError(f"Duplicate port {self.name}.{definition.name}.")
+        self._ports[definition.name] = port
+        return port
+
+    def register_declared_port(self, name: str) -> PortState:
+        try:
+            definition = next(item for item in self.PORTS if item.name == name)
+        except StopIteration as exc:
+            raise ValueError(
+                f"Component model {self.model_type} does not declare port {name}."
+            ) from exc
+        return self.register_port(PortState(definition=definition))
+
+    def set_parameter_values(self, values: Mapping[str, float]) -> None:
+        definitions = {definition.name: definition for definition in self.PARAMETERS}
+        unknown = sorted(set(values) - set(definitions))
+        if unknown:
+            raise ValueError(
+                f"Component {self.name} contains unsupported parameters: "
+                + ", ".join(unknown)
+                + "."
+            )
+        missing = sorted(set(definitions) - set(values))
+        if missing:
+            raise ValueError(
+                f"Component {self.name} is missing parameters: "
+                + ", ".join(missing)
+                + "."
+            )
+
+        resolved: dict[str, float] = {}
+        for name, definition in definitions.items():
+            value = float(values[name])
+            message = definition.validation_message(value)
+            if message is not None:
+                raise ValueError(
+                    f"Parameter '{name}' on component '{self.name}' {message}."
+                )
+            resolved[name] = value
+        self._parameter_values = resolved
+
+    @property
+    def parameter_values(self) -> dict[str, float]:
+        return dict(self._parameter_values)
+
+    def get_port(self, name: str) -> PortState:
+        try:
+            return self._ports[name]
+        except KeyError as exc:
+            raise ValueError(f"Component {self.name} has no port named {name}.") from exc
+
+    def component_result_values(self) -> Mapping[str, float]:
+        return {}
+
+    def result_values(self) -> dict[str, float]:
+        component_values = dict(self.component_result_values())
+        declared = {definition.name: definition for definition in self.RESULT_VARIABLES}
+        unknown = sorted(set(component_values) - set(declared))
+        if unknown:
+            raise ValueError(
+                f"Component {self.name} returned undeclared result variables: "
+                + ", ".join(unknown)
+                + "."
+            )
+
+        values: dict[str, float] = {}
+        for name, definition in declared.items():
+            if not definition.visible:
+                continue
+            if name not in component_values:
+                raise ValueError(
+                    f"Component {self.name} did not provide declared result variable {name}."
+                )
+            values[name] = float(component_values[name])
+
+        for port_definition in self.active_port_definitions:
+            port = self.get_port(port_definition.name)
+            for variable in port_definition.variables:
+                if not variable.result_visible:
+                    continue
+                values[f"{port_definition.name}.{variable.name}"] = float(
+                    getattr(port, variable.name)
+                )
+        return values
+
+    def result_variable_metadata(self) -> tuple[ResultVariableMetadata, ...]:
+        metadata = [
+            ResultVariableMetadata(
+                key=f"{self.name}.{definition.name}",
+                component_id=self.name,
+                component_type=self.model_type,
+                scope="component",
+                name=definition.name,
+                label=definition.label,
+                quantity=definition.quantity,
+                unit=definition.unit,
+                category=definition.category,
+                order=definition.order,
+            )
+            for definition in self.RESULT_VARIABLES
+            if definition.visible
+        ]
+        for port_definition in self.active_port_definitions:
+            for variable in port_definition.variables:
+                if not variable.result_visible:
+                    continue
+                metadata.append(
+                    ResultVariableMetadata(
+                        key=f"{self.name}.{port_definition.name}.{variable.name}",
+                        component_id=self.name,
+                        component_type=self.model_type,
+                        scope="port",
+                        port_name=port_definition.name,
+                        name=variable.name,
+                        label=variable.label or variable.name,
+                        quantity=variable.quantity or variable.name,
+                        unit=variable.unit,
+                        category=variable.role,
+                        order=variable.order,
+                    )
+                )
+        return tuple(metadata)
+
+    def parameter_interface_dicts(self) -> list[dict[str, object]]:
+        return [
+            definition.as_interface_dict(
+                value=self._parameter_values.get(definition.name)
+            )
+            for definition in self.PARAMETERS
+        ]
+
+    @classmethod
+    def create(
+        cls,
+        *,
+        name: str,
+        medium: GasMedium,
+        parameters: Mapping[str, float],
+    ) -> Component:
+        """Create a catalog model from normalized SI parameters."""
+
+        raise NotImplementedError(
+            f"Component model {cls.__name__} must implement create()."
+        )
+
+    def pressure_flow_equation_residuals(self) -> tuple[EquationResidual, ...]:
+        """Return algebraic residuals after the network assigns port states."""
+
+        return ()
+
+    def pressure_flow_equation_values(self) -> tuple[float, ...]:
+        """Return live residual values in the declared equation order.
+
+        Components with frequently evaluated equations can override this
+        method to avoid rebuilding immutable equation metadata during closure.
+        The default keeps third-party components compatible with the public
+        residual API.
+        """
+
+        return tuple(
+            float(equation.value)
+            for equation in self.pressure_flow_equation_residuals()
+        )
+
+    def pressure_flow_equation_value_readers(
+        self,
+    ) -> Mapping[str, Callable[[], float]]:
+        """Return explicitly separable scalar residual readers.
+
+        The solver consumes this optional capability only when the concrete
+        component class declares the method itself.  Subclasses therefore
+        cannot accidentally inherit an equation-purity promise.
+        """
+
+        return {}
+
+    def update_stream_outflows(self, connected_h: Mapping[str, float]) -> None:
+        """Update connector outflow properties from current flow directions."""
+
+        return None
+
+    def update_flow_temperature_references(
+        self,
+        connected_h: Mapping[str, float],
+    ) -> None:
+        """Update enthalpy references used only by pressure-flow laws.
+
+        Most components use the normal stream enthalpy for both energy
+        transport and upstream-property evaluation. AMESim node submodels can
+        expose a distinct temperature reference, so the default is a no-op.
+        """
+
+        return None
+
+    def pneumatic_volume_outputs(self) -> Mapping[str, tuple[float, float]]:
+        """Return directed ``volume``/``volume_flow`` values by pneumatic port.
+
+        Most pneumatic components contribute no external chamber volume. Moving
+        boundaries such as PNRP17 override this hook; the network resolver then
+        propagates the pair to the component connected at the same physical port.
+        """
+
+        return {}
+
+
+class DynamicComponent(Component):
+    state_size = 2
+
+    @staticmethod
+    def actual_stream_enthalpy(
+        port_m_flow: float,
+        connected_h: float,
+        internal_h: float,
+    ) -> float:
+        """Approximate `actualStream(port.h_outflow)` for a mixed control volume port."""
+
+        return connected_h if port_m_flow > 0.0 else internal_h
+
+    def connection_inlet_enthalpy(
+        self,
+        port_m_flow: float,
+        connected_h: float,
+        internal_h: float,
+    ) -> float:
+        """Resolve the enthalpy convected into this control volume through one port."""
+
+        return self.actual_stream_enthalpy(
+            port_m_flow=port_m_flow,
+            connected_h=connected_h,
+            internal_h=internal_h,
+        )
+
+    @abstractmethod
+    def get_state_vector(self) -> list[float]:
+        raise NotImplementedError
+
+    @abstractmethod
+    def set_state_vector(self, values: list[float]) -> None:
+        raise NotImplementedError
+
+    def refresh_thermodynamic_ports(self) -> Any:
+        raise NotImplementedError
+
+    def state_derivative_from_ports(
+        self,
+        connected_h: Mapping[str, float],
+    ) -> list[float]:
+        raise NotImplementedError
+
+
+class ThermodynamicVolumeComponent(DynamicComponent):
+    """Two-state gas volume exposing the shared thermodynamic result contract."""
+
+    RESULT_VARIABLES = THERMODYNAMIC_VOLUME_RESULT_VARIABLES
+
+    def component_result_values(self) -> Mapping[str, float]:
+        state = self.get_state_vector()
+        if len(state) < 2:
+            raise ValueError(
+                f"Thermodynamic component {self.name} must expose mass and energy states."
+            )
+        properties = self.refresh_thermodynamic_ports()
+        return {
+            "m": float(state[0]),
+            "U": float(state[1]),
+            "p": float(properties.p),
+            "T": float(properties.T),
+            "rho": float(properties.rho),
+            "u": float(properties.u),
+            "h": float(properties.h),
+        }
+
+
+class AlgebraicComponent(Component):
+    """Stateless element described by algebraic constraints only."""

app/simulation/core/catalog.py

@@ -0,0 +1,106 @@
+from __future__ import annotations
+
+from dataclasses import dataclass
+from typing import Literal
+
+
+PortDisplaySide = Literal["left", "right"]
+ComponentCatalogRole = Literal["amesimGasMediumDefinition"]
+
+
+@dataclass(frozen=True)
+class ComponentCategorySpec:
+    """A presentation-only category declared by one component library."""
+
+    id: str
+    label: str
+    order: int = 0
+
+    def as_catalog_dict(self) -> dict[str, object]:
+        return {
+            "id": self.id,
+            "label": self.label,
+            "order": self.order,
+        }
+
+
+@dataclass(frozen=True)
+class PortDisplaySpec:
+    """Canvas placement for one port without changing its physical contract."""
+
+    name: str
+    side: PortDisplaySide
+    order: int = 0
+
+
+@dataclass(frozen=True)
+class ParameterGroupDisplaySpec:
+    """Ordered, collapsible presentation group for component parameters."""
+
+    id: str
+    label: str
+    parameters: tuple[str, ...]
+    order: int = 0
+    default_expanded: bool = False
+
+    def as_catalog_dict(self) -> dict[str, object]:
+        return {
+            "id": self.id,
+            "label": self.label,
+            "parameters": list(self.parameters),
+            "order": self.order,
+            "defaultExpanded": self.default_expanded,
+        }
+
+
+@dataclass(frozen=True)
+class ComponentDisplaySpec:
+    """Frontend metadata co-located with a component implementation."""
+
+    label: str
+    library_id: str
+    category_id: str
+    symbol: str
+    ports: tuple[PortDisplaySpec, ...]
+    order: int = 0
+    role: ComponentCatalogRole | None = None
+    parameter_groups: tuple[ParameterGroupDisplaySpec, ...] = ()
+
+    @property
+    def port_by_name(self) -> dict[str, PortDisplaySpec]:
+        return {port.name: port for port in self.ports}
+
+
+@dataclass(frozen=True)
+class ComponentLibrarySpec:
+    """Manifest for one explicitly enabled component library."""
+
+    id: str
+    label: str
+    version: str
+    source_package: str
+    categories: tuple[ComponentCategorySpec, ...]
+    models: tuple[str, ...]
+    temporary: bool = False
+    order: int = 0
+
+    @property
+    def category_by_id(self) -> dict[str, ComponentCategorySpec]:
+        return {category.id: category for category in self.categories}
+
+    def as_catalog_dict(self) -> dict[str, object]:
+        return {
+            "id": self.id,
+            "label": self.label,
+            "version": self.version,
+            "sourcePackage": self.source_package,
+            "temporary": self.temporary,
+            "order": self.order,
+            "categories": [
+                category.as_catalog_dict()
+                for category in sorted(
+                    self.categories,
+                    key=lambda item: (item.order, item.id),
+                )
+            ],
+        }

app/simulation/core/equations.py

@@ -0,0 +1,36 @@
+from __future__ import annotations
+
+from dataclasses import dataclass
+from typing import Literal
+
+from app.simulation.core.ports import VariableRole
+
+
+EquationOwner = Literal["connection", "component"]
+EquationRelation = Literal["equal", "sumToZero", "constitutive", "state"]
+
+
+@dataclass(frozen=True, slots=True)
+class EquationResidual:
+    """One executable scalar equation in the pressure-flow subsystem."""
+
+    id: str
+    owner: EquationOwner
+    owner_id: str
+    relation: EquationRelation
+    variables: tuple[str, ...]
+    value: float
+    role: VariableRole | None = None
+
+    def as_definition_dict(self) -> dict[str, object]:
+        return {
+            "id": self.id,
+            "owner": self.owner,
+            "ownerId": self.owner_id,
+            "relation": self.relation,
+            "variables": list(self.variables),
+            "role": self.role,
+        }
+
+    def as_interface_dict(self) -> dict[str, object]:
+        return {**self.as_definition_dict(), "residual": self.value}

app/simulation/core/errors.py

@@ -0,0 +1,5 @@
+from __future__ import annotations
+
+
+class RecoverableTrialStateError(ValueError):
+    """A physical-domain failure caused by an integrator trial state."""

app/simulation/core/medium.py

@@ -0,0 +1,378 @@
+from __future__ import annotations
+
+from dataclasses import dataclass
+from math import isfinite
+from typing import Protocol, Sequence
+
+from app.simulation.core.errors import RecoverableTrialStateError
+from app.simulation.performance import profile_property
+
+
+@dataclass(frozen=True)
+class ThermodynamicProperties:
+    p: float
+    T: float
+    rho: float
+    u: float
+    h: float
+
+
+@dataclass(frozen=True)
+class ThermodynamicPropertyTangents:
+    """Directional derivatives of a recovered thermodynamic state."""
+
+    p: tuple[float, ...]
+    T: tuple[float, ...]
+    rho: tuple[float, ...]
+    u: tuple[float, ...]
+    h: tuple[float, ...]
+
+    @property
+    def width(self) -> int:
+        return len(self.p)
+
+    @classmethod
+    def zeros(cls, width: int) -> "ThermodynamicPropertyTangents":
+        values = (0.0,) * width
+        return cls(p=values, T=values, rho=values, u=values, h=values)
+
+
+@dataclass(frozen=True)
+class ThermodynamicPropertiesLinearization:
+    """Primal properties and a validity-checked directional linearization."""
+
+    properties: ThermodynamicProperties
+    tangents: ThermodynamicPropertyTangents
+    valid: bool = True
+    reason: str | None = None
+
+
+class GasMedium(Protocol):
+    """Thermodynamic contract required by pneumatic components.
+
+    ``IdealGasMedium`` is the default implementation.  Keeping the component
+    boundary structural allows a later helium/Peng-Robinson implementation to
+    be registered without changing every AMESim component constructor.
+    """
+
+    name: str
+    R_gas: float
+    cp_ref: float
+    T_ref: float
+
+    @property
+    def cv(self) -> float: ...
+
+    @property
+    def gamma(self) -> float: ...
+
+    def cp_at_temperature(self, T: float) -> float: ...
+
+    def cv_at_temperature(self, T: float) -> float: ...
+
+    def density(self, p: float, T: float) -> float: ...
+
+    def isentropic_density_pressure_factor(
+        self,
+        p: float,
+        T: float,
+        downstream_pressure: float | None = None,
+    ) -> float: ...
+
+    def dynamic_viscosity(self, T: float) -> float: ...
+
+    def diagnostic_dynamic_viscosity(self, T: float) -> float: ...
+
+    def specific_internal_energy(self, T: float) -> float: ...
+
+    def specific_internal_energy_at_pressure(self, p: float, T: float) -> float: ...
+
+    def specific_enthalpy(self, T: float) -> float: ...
+
+    def specific_enthalpy_at_pressure(self, p: float, T: float) -> float: ...
+
+    def temperature_from_internal_energy(self, u: float) -> float: ...
+
+    def temperature_from_enthalpy(self, h: float) -> float: ...
+
+    def temperature_from_pressure_enthalpy(self, p: float, h: float) -> float: ...
+
+    def temperature_from_mass_internal_energy(self, m: float, U: float) -> float: ...
+
+    def pressure(self, m: float, T: float, V: float) -> float: ...
+
+    def properties_from_mU(
+        self,
+        m: float,
+        U: float,
+        V: float,
+    ) -> ThermodynamicProperties: ...
+
+    def linearize_properties_from_mU(
+        self,
+        m: float,
+        U: float,
+        V: float,
+        dm: Sequence[float],
+        dU: Sequence[float],
+        dV: Sequence[float],
+        *,
+        properties: ThermodynamicProperties | None = None,
+    ) -> ThermodynamicPropertiesLinearization: ...
+
+
+@dataclass(frozen=True)
+class IdealGasMedium:
+    """Temperature-dependent ideal-gas air approximation.
+
+    This is still not a strict clone of `Modelica.Media.Air.SimpleAir`.
+    The small linear `cp(T)` term is kept configurable for calibration, but the
+    current default is calibrated against the committed Testmodel baseline and
+    therefore falls back to the constant-heat-capacity limit.
+    """
+
+    name: str = "SimpleAirApprox"
+    R_gas: float = 287.0
+    cp_ref: float = 1005.0
+    T_ref: float = 300.0
+    cp_slope: float = 0.0
+    viscosity_ref: float = 1.82e-5
+    viscosity_T_ref: float = 293.15
+    sutherland_constant: float = 110.4
+
+    @property
+    def cv(self) -> float:
+        return self.cv_at_temperature(self.T_ref)
+
+    @property
+    def gamma(self) -> float:
+        return self.cp_at_temperature(self.T_ref) / self.cv
+
+    def cp_at_temperature(self, T: float) -> float:
+        return self.cp_ref + self.cp_slope * (T - self.T_ref)
+
+    def cv_at_temperature(self, T: float) -> float:
+        return self.cp_at_temperature(T) - self.R_gas
+
+    @profile_property("density")
+    def density(self, p: float, T: float) -> float:
+        return p / (self.R_gas * T)
+
+    @profile_property("isentropic_density_pressure_factor")
+    def isentropic_density_pressure_factor(
+        self,
+        p: float,
+        T: float,
+        downstream_pressure: float | None = None,
+    ) -> float:
+        del p
+        del downstream_pressure
+        cp = self.cp_at_temperature(T)
+        cv = self.cv_at_temperature(T)
+        return cv / cp
+
+    @profile_property("dynamic_viscosity")
+    def dynamic_viscosity(self, T: float) -> float:
+        """Return dynamic viscosity using the default air Sutherland law."""
+
+        if T <= 0.0:
+            raise ValueError("Temperature must be positive.")
+        return (
+            self.viscosity_ref
+            * (T / self.viscosity_T_ref) ** 1.5
+            * (self.viscosity_T_ref + self.sutherland_constant)
+            / (T + self.sutherland_constant)
+        )
+
+    def diagnostic_dynamic_viscosity(self, T: float) -> float:
+        """Return the viscosity convention used by derived diagnostics.
+
+        Most media use the same transport property for dynamics and reported
+        diagnostics. Reference-library media may override this without
+        changing a calibrated constitutive flow relation.
+        """
+
+        return self.dynamic_viscosity(T)
+
+    @profile_property("specific_internal_energy")
+    def specific_internal_energy(self, T: float) -> float:
+        delta_T = T - self.T_ref
+        return (
+            self.cv * self.T_ref
+            + self.cv * delta_T
+            + 0.5 * self.cp_slope * delta_T * delta_T
+        )
+
+    @profile_property("specific_internal_energy_at_pressure")
+    def specific_internal_energy_at_pressure(self, p: float, T: float) -> float:
+        del p
+        return self.specific_internal_energy(T)
+
+    @profile_property("specific_enthalpy")
+    def specific_enthalpy(self, T: float) -> float:
+        delta_T = T - self.T_ref
+        return (
+            self.cp_ref * self.T_ref
+            + self.cp_ref * delta_T
+            + 0.5 * self.cp_slope * delta_T * delta_T
+        )
+
+    @profile_property("specific_enthalpy_at_pressure")
+    def specific_enthalpy_at_pressure(self, p: float, T: float) -> float:
+        del p
+        return self.specific_enthalpy(T)
+
+    def temperature_from_internal_energy(self, u: float) -> float:
+        reference_internal_energy = self.cv * self.T_ref
+        delta_u = u - reference_internal_energy
+
+        if abs(self.cp_slope) <= 1e-15:
+            return self.T_ref + delta_u / self.cv
+
+        a = 0.5 * self.cp_slope
+        b = self.cv
+        c = -delta_u
+        discriminant = max(b * b - 4.0 * a * c, 0.0)
+        positive_root = (-b + discriminant**0.5) / (2.0 * a)
+        negative_root = (-b - discriminant**0.5) / (2.0 * a)
+        delta_T = positive_root if abs(positive_root) <= abs(negative_root) else negative_root
+        return self.T_ref + delta_T
+
+    def temperature_from_enthalpy(self, h: float) -> float:
+        reference_enthalpy = self.cp_ref * self.T_ref
+        delta_h = h - reference_enthalpy
+
+        if abs(self.cp_slope) <= 1e-15:
+            return self.T_ref + delta_h / self.cp_ref
+
+        a = 0.5 * self.cp_slope
+        b = self.cp_ref
+        c = -delta_h
+        discriminant = max(b * b - 4.0 * a * c, 0.0)
+        positive_root = (-b + discriminant**0.5) / (2.0 * a)
+        negative_root = (-b - discriminant**0.5) / (2.0 * a)
+        delta_T = positive_root if abs(positive_root) <= abs(negative_root) else negative_root
+        return self.T_ref + delta_T
+
+    @profile_property("temperature_from_pressure_enthalpy")
+    def temperature_from_pressure_enthalpy(self, p: float, h: float) -> float:
+        del p
+        return self.temperature_from_enthalpy(h)
+
+    def temperature_from_mass_internal_energy(self, m: float, U: float) -> float:
+        if m <= 0.0:
+            raise RecoverableTrialStateError(
+                "Mass must stay positive when recovering temperature."
+            )
+        return self.temperature_from_internal_energy(U / m)
+
+    def pressure(self, m: float, T: float, V: float) -> float:
+        if V <= 0.0:
+            raise ValueError("Volume must stay positive.")
+        return m * self.R_gas * T / V
+
+    @profile_property("properties_from_mU")
+    def properties_from_mU(self, m: float, U: float, V: float) -> ThermodynamicProperties:
+        T = self.temperature_from_mass_internal_energy(m, U)
+        p = self.pressure(m, T, V)
+        rho = m / V
+        u = U / m
+        h = self.specific_enthalpy(T)
+        return ThermodynamicProperties(p=p, T=T, rho=rho, u=u, h=h)
+
+    def linearize_properties_from_mU(
+        self,
+        m: float,
+        U: float,
+        V: float,
+        dm: Sequence[float],
+        dU: Sequence[float],
+        dV: Sequence[float],
+        *,
+        properties: ThermodynamicProperties | None = None,
+    ) -> ThermodynamicPropertiesLinearization:
+        """Linearize properties_from_mU for several seed directions."""
+
+        dm_values = tuple(float(value) for value in dm)
+        dU_values = tuple(float(value) for value in dU)
+        dV_values = tuple(float(value) for value in dV)
+        if not (len(dm_values) == len(dU_values) == len(dV_values)):
+            raise ValueError("Thermodynamic tangent vectors must have equal lengths.")
+        props = properties or self.properties_from_mU(m, U, V)
+        width = len(dm_values)
+        expected_density = m / V
+        expected_internal_energy = U / m
+        if (
+            abs(props.rho - expected_density)
+            > 1.0e-12 * max(abs(expected_density), 1.0)
+            or abs(props.u - expected_internal_energy)
+            > 1.0e-12 * max(abs(expected_internal_energy), 1.0)
+        ):
+            return ThermodynamicPropertiesLinearization(
+                properties=props,
+                tangents=ThermodynamicPropertyTangents.zeros(width),
+                valid=False,
+                reason="properties_primal_mismatch",
+            )
+        if not all(
+            isfinite(value)
+            for values in (dm_values, dU_values, dV_values)
+            for value in values
+        ):
+            return ThermodynamicPropertiesLinearization(
+                properties=props,
+                tangents=ThermodynamicPropertyTangents.zeros(width),
+                valid=False,
+                reason="non_finite_tangent_input",
+            )
+
+        cv = self.cv_at_temperature(props.T)
+        cp = self.cp_at_temperature(props.T)
+        if not isfinite(cv) or not isfinite(cp) or cv <= 0.0 or cp <= 0.0:
+            return ThermodynamicPropertiesLinearization(
+                properties=props,
+                tangents=ThermodynamicPropertyTangents.zeros(width),
+                valid=False,
+                reason="non_positive_heat_capacity",
+            )
+
+        drho: list[float] = []
+        du: list[float] = []
+        dT: list[float] = []
+        dp: list[float] = []
+        dh: list[float] = []
+        for mass_tangent, energy_tangent, volume_tangent in zip(
+            dm_values,
+            dU_values,
+            dV_values,
+            strict=True,
+        ):
+            density_tangent = mass_tangent / V - m * volume_tangent / (V * V)
+            internal_energy_tangent = (
+                energy_tangent / m - U * mass_tangent / (m * m)
+            )
+            temperature_tangent = internal_energy_tangent / cv
+            pressure_tangent = self.R_gas * (
+                props.T * density_tangent + props.rho * temperature_tangent
+            )
+            enthalpy_tangent = cp * temperature_tangent
+            drho.append(density_tangent)
+            du.append(internal_energy_tangent)
+            dT.append(temperature_tangent)
+            dp.append(pressure_tangent)
+            dh.append(enthalpy_tangent)
+
+        tangent_values = (*drho, *du, *dT, *dp, *dh)
+        valid = all(isfinite(value) for value in tangent_values)
+        return ThermodynamicPropertiesLinearization(
+            properties=props,
+            tangents=ThermodynamicPropertyTangents(
+                p=tuple(dp),
+                T=tuple(dT),
+                rho=tuple(drho),
+                u=tuple(du),
+                h=tuple(dh),
+            ),
+            valid=valid,
+            reason=None if valid else "non_finite_property_tangent",
+        )

app/simulation/core/metadata.py

@@ -0,0 +1,240 @@
+from __future__ import annotations
+
+from dataclasses import dataclass
+from math import isfinite
+from typing import Literal
+
+
+ResultVariableScope = Literal["component", "port"]
+ParameterEditor = Literal[
+    "amesimGasReference",
+    "amesimGasPropertyModel",
+    "choice",
+]
+
+
+SI_UNIT_BY_QUANTITY: dict[str, str] = {
+    "acceleration": "m/s2",
+    "area": "m2",
+    "dimensionless": "",
+    "density": "kg/m³",
+    "flow_coefficient": "kg/(s*Pa^0.5)",
+    "force": "N",
+    "heat_transfer_coefficient": "W/(m2*K)",
+    "internal_energy": "J",
+    "length": "m",
+    "mass": "kg",
+    "mass_flow": "kg/s",
+    "pressure": "Pa",
+    "specific_enthalpy": "J/kg",
+    "specific_internal_energy": "J/kg",
+    "temperature": "K",
+    "translational_damping": "N/(m/s)",
+    "translational_stiffness": "N/m",
+    "time": "s",
+    "velocity": "m/s",
+    "volume": "m3",
+    "volume_flow": "m3/s",
+    "windage": "N/(m/s)^2",
+}
+
+
+@dataclass(frozen=True)
+class ParameterOption:
+    """One numeric choice exposed by a catalog-backed parameter editor."""
+
+    value: float
+    label: str
+
+    def as_interface_dict(self) -> dict[str, object]:
+        return {
+            "value": self.value,
+            "label": self.label,
+        }
+
+
+@dataclass(frozen=True)
+class ParameterCondition:
+    """Match when the controlling parameter equals any declared value."""
+
+    parameter: str
+    values: tuple[float, ...]
+
+    def as_interface_dict(self) -> dict[str, object]:
+        return {
+            "parameter": self.parameter,
+            "values": list(self.values),
+        }
+
+
+@dataclass(frozen=True)
+class ParameterDefinition:
+    """User-configurable model input expressed in the backend SI contract.
+
+    Every ``visible_when`` condition must match for the catalog parameter to
+    be visible; each individual condition matches any one of its ``values``.
+    """
+
+    name: str
+    default: float
+    label: str = ""
+    quantity: str = "dimensionless"
+    unit: str = ""
+    minimum: float | None = None
+    maximum: float | None = None
+    minimum_exclusive: bool = False
+    editor: ParameterEditor | None = None
+    options: tuple[ParameterOption, ...] = ()
+    description: str = ""
+    visible_when: tuple[ParameterCondition, ...] = ()
+
+    def validation_message(self, value: float) -> str | None:
+        if not isfinite(value):
+            return "must be finite"
+        if self.minimum is not None:
+            if self.minimum_exclusive and value <= self.minimum:
+                return f"must be greater than {self.minimum:g}"
+            if not self.minimum_exclusive and value < self.minimum:
+                return f"must be at least {self.minimum:g}"
+        if self.maximum is not None and value > self.maximum:
+            return f"must be at most {self.maximum:g}"
+        if self.options and value not in {
+            float(option.value) for option in self.options
+        }:
+            available = ", ".join(f"{option.value:g}" for option in self.options)
+            return f"must be one of {available}"
+        return None
+
+    def as_interface_dict(self, *, value: float | None = None) -> dict[str, object]:
+        payload: dict[str, object] = {
+            "name": self.name,
+            "label": self.label or self.name,
+            "quantity": self.quantity,
+            "unit": self.unit,
+            "default": self.default,
+            "minimumExclusive": self.minimum_exclusive,
+        }
+        if self.minimum is not None:
+            payload["minimum"] = self.minimum
+        if self.maximum is not None:
+            payload["maximum"] = self.maximum
+        if self.editor is not None:
+            payload["editor"] = self.editor
+        if self.options:
+            payload["options"] = [
+                option.as_interface_dict() for option in self.options
+            ]
+        if self.description:
+            payload["description"] = self.description
+        if self.visible_when:
+            payload["visibleWhen"] = [
+                condition.as_interface_dict() for condition in self.visible_when
+            ]
+        if value is not None:
+            payload["value"] = value
+        return payload
+
+
+@dataclass(frozen=True)
+class ResultVariableDefinition:
+    """Component-relative declaration of a user-visible simulation result."""
+
+    name: str
+    label: str
+    quantity: str
+    unit: str = ""
+    category: str = "derived"
+    order: int = 0
+    visible: bool = True
+
+
+@dataclass(frozen=True)
+class ResultVariableMetadata:
+    """A result declaration bound to one concrete component instance."""
+
+    key: str
+    component_id: str
+    component_type: str
+    scope: ResultVariableScope
+    name: str
+    label: str
+    quantity: str
+    unit: str
+    category: str
+    order: int
+    port_name: str | None = None
+
+    def as_dict(self) -> dict[str, object]:
+        return {
+            "key": self.key,
+            "componentId": self.component_id,
+            "componentType": self.component_type,
+            "scope": self.scope,
+            "portName": self.port_name,
+            "name": self.name,
+            "label": self.label,
+            "quantity": self.quantity,
+            "unit": self.unit,
+            "category": self.category,
+            "order": self.order,
+        }
+
+
+THERMODYNAMIC_VOLUME_RESULT_VARIABLES = (
+    ResultVariableDefinition(
+        name="m",
+        label="质量",
+        quantity="mass",
+        unit="kg",
+        category="state",
+        order=10,
+    ),
+    ResultVariableDefinition(
+        name="U",
+        label="内能",
+        quantity="internal_energy",
+        unit="J",
+        category="state",
+        order=20,
+    ),
+    ResultVariableDefinition(
+        name="p",
+        label="压力",
+        quantity="pressure",
+        unit="Pa",
+        category="thermodynamic",
+        order=30,
+    ),
+    ResultVariableDefinition(
+        name="T",
+        label="温度",
+        quantity="temperature",
+        unit="K",
+        category="thermodynamic",
+        order=40,
+    ),
+    ResultVariableDefinition(
+        name="rho",
+        label="密度",
+        quantity="density",
+        unit="kg/m³",
+        category="thermodynamic",
+        order=50,
+    ),
+    ResultVariableDefinition(
+        name="u",
+        label="比内能",
+        quantity="specific_internal_energy",
+        unit="J/kg",
+        category="thermodynamic",
+        order=60,
+    ),
+    ResultVariableDefinition(
+        name="h",
+        label="比焓",
+        quantity="specific_enthalpy",
+        unit="J/kg",
+        category="thermodynamic",
+        order=70,
+    ),
+)

app/simulation/core/peng_robinson.py

@@ -0,0 +1,424 @@
+from __future__ import annotations
+
+from app.simulation.core.errors import RecoverableTrialStateError
+
+from dataclasses import dataclass
+from math import acos, cos, isfinite, log, pi, sqrt
+
+from app.simulation.performance import profile_property
+
+UNIVERSAL_GAS_CONSTANT = 8.31446261815324
+# Simcenter Amesim 2404 ``sag_reinit_eos_`` keeps more digits than the
+# commonly printed Peng-Robinson constants 0.45724 and 0.07780.
+PENG_ROBINSON_A_COEFFICIENT = 0.457235583
+PENG_ROBINSON_B_COEFFICIENT = 0.07779607
+
+
+@dataclass(frozen=True)
+class PengRobinsonFluid:
+    """Pure-fluid Peng-Robinson equation-of-state helper.
+
+    The class covers the equation-of-state layer plus the enthalpy departure
+    needed to compare AMESim pneumatic ``pn2hpti`` reference enthalpy flows.
+    """
+
+    name: str
+    molar_mass: float
+    critical_temperature: float
+    critical_pressure: float
+    acentric_factor: float
+
+    @property
+    def specific_gas_constant(self) -> float:
+        return UNIVERSAL_GAS_CONSTANT / self.molar_mass
+
+    @property
+    def a_parameter(self) -> float:
+        return (
+            PENG_ROBINSON_A_COEFFICIENT
+            * UNIVERSAL_GAS_CONSTANT
+            * UNIVERSAL_GAS_CONSTANT
+            * self.critical_temperature
+            * self.critical_temperature
+            / self.critical_pressure
+        )
+
+    @property
+    def b_parameter(self) -> float:
+        return (
+            PENG_ROBINSON_B_COEFFICIENT
+            * UNIVERSAL_GAS_CONSTANT
+            * self.critical_temperature
+            / self.critical_pressure
+        )
+
+    @property
+    def kappa(self) -> float:
+        omega = self.acentric_factor
+        return 0.37464 + 1.54226 * omega - 0.26992 * omega * omega
+
+    def alpha(self, temperature: float) -> float:
+        self._validate_temperature(temperature)
+        reduced_temperature = temperature / self.critical_temperature
+        return (1.0 + self.kappa * (1.0 - sqrt(reduced_temperature))) ** 2.0
+
+    def alpha_temperature_derivative(self, temperature: float) -> float:
+        self._validate_temperature(temperature)
+        reduced_temperature = temperature / self.critical_temperature
+        sqrt_reduced_temperature = sqrt(reduced_temperature)
+        alpha_base = 1.0 + self.kappa * (1.0 - sqrt_reduced_temperature)
+        return -(
+            alpha_base
+            * self.kappa
+            / (self.critical_temperature * sqrt_reduced_temperature)
+        )
+
+    def alpha_temperature_second_derivative(self, temperature: float) -> float:
+        self._validate_temperature(temperature)
+        reduced_temperature = temperature / self.critical_temperature
+        sqrt_reduced_temperature = sqrt(reduced_temperature)
+        alpha_base = 1.0 + self.kappa * (1.0 - sqrt_reduced_temperature)
+        return (
+            self.kappa
+            / (2.0 * self.critical_temperature * self.critical_temperature)
+            * (
+                self.kappa / reduced_temperature
+                + alpha_base / (reduced_temperature * sqrt_reduced_temperature)
+            )
+        )
+
+    def attractive_parameter(self, temperature: float) -> float:
+        return self.a_parameter * self.alpha(temperature)
+
+    def attractive_parameter_temperature_derivative(self, temperature: float) -> float:
+        return self.a_parameter * self.alpha_temperature_derivative(temperature)
+
+    def attractive_parameter_temperature_second_derivative(
+        self,
+        temperature: float,
+    ) -> float:
+        return self.a_parameter * self.alpha_temperature_second_derivative(temperature)
+
+    @profile_property(
+        "pressure_from_molar_volume",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def pressure_from_molar_volume(self, temperature: float, molar_volume: float) -> float:
+        self._validate_temperature(temperature)
+        if molar_volume <= self.b_parameter:
+            raise RecoverableTrialStateError("Molar volume must be larger than Peng-Robinson b parameter.")
+        a_alpha = self.attractive_parameter(temperature)
+        b = self.b_parameter
+        repulsive = UNIVERSAL_GAS_CONSTANT * temperature / (molar_volume - b)
+        attractive = a_alpha / (molar_volume * (molar_volume + b) + b * (molar_volume - b))
+        return repulsive - attractive
+
+    @profile_property(
+        "pressure_from_density",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def pressure_from_density(self, temperature: float, density: float) -> float:
+        if density <= 0.0:
+            raise ValueError("Density must be positive.")
+        return self.pressure_from_molar_volume(temperature, self.molar_mass / density)
+
+    @profile_property(
+        "pressure_temperature_derivative_at_density",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def pressure_temperature_derivative_at_density(
+        self,
+        temperature: float,
+        density: float,
+    ) -> float:
+        self._validate_temperature(temperature)
+        if density <= 0.0:
+            raise ValueError("Density must be positive.")
+        molar_volume = self.molar_mass / density
+        if molar_volume <= self.b_parameter:
+            raise RecoverableTrialStateError(
+                "Molar volume must be larger than Peng-Robinson b parameter."
+            )
+        b = self.b_parameter
+        denominator = molar_volume * (molar_volume + b) + b * (molar_volume - b)
+        return (
+            UNIVERSAL_GAS_CONSTANT / (molar_volume - b)
+            - self.attractive_parameter_temperature_derivative(temperature) / denominator
+        )
+
+    @profile_property(
+        "pressure_density_derivative_at_temperature",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def pressure_density_derivative_at_temperature(
+        self,
+        temperature: float,
+        density: float,
+    ) -> float:
+        self._validate_temperature(temperature)
+        if density <= 0.0:
+            raise ValueError("Density must be positive.")
+        molar_volume = self.molar_mass / density
+        if molar_volume <= self.b_parameter:
+            raise RecoverableTrialStateError(
+                "Molar volume must be larger than Peng-Robinson b parameter."
+            )
+        b = self.b_parameter
+        denominator = molar_volume * (molar_volume + b) + b * (molar_volume - b)
+        pressure_molar_volume_derivative = (
+            -UNIVERSAL_GAS_CONSTANT * temperature / (molar_volume - b) ** 2
+            + self.attractive_parameter(temperature)
+            * 2.0
+            * (molar_volume + b)
+            / denominator**2
+        )
+        molar_volume_density_derivative = -self.molar_mass / (density * density)
+        return pressure_molar_volume_derivative * molar_volume_density_derivative
+
+    def reduced_parameters(self, pressure: float, temperature: float) -> tuple[float, float]:
+        self._validate_pressure_temperature(pressure, temperature)
+        a_alpha = self.attractive_parameter(temperature)
+        b = self.b_parameter
+        A = a_alpha * pressure / (UNIVERSAL_GAS_CONSTANT * UNIVERSAL_GAS_CONSTANT * temperature * temperature)
+        B = b * pressure / (UNIVERSAL_GAS_CONSTANT * temperature)
+        return A, B
+
+    @profile_property(
+        "compressibility_roots",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def compressibility_roots(self, pressure: float, temperature: float) -> tuple[float, ...]:
+        A, B = self.reduced_parameters(pressure, temperature)
+        coefficients = (
+            -(1.0 - B),
+            A - 3.0 * B * B - 2.0 * B,
+            -(A * B - B * B - B * B * B),
+        )
+        roots = _real_cubic_roots(*coefficients)
+        physical_roots = tuple(sorted(root for root in roots if root > B and isfinite(root)))
+        if not physical_roots:
+            raise ValueError("Peng-Robinson cubic produced no physical compressibility root.")
+        return physical_roots
+
+    @profile_property(
+        "compressibility_factor",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def compressibility_factor(
+        self,
+        pressure: float,
+        temperature: float,
+        phase: str = "vapor",
+    ) -> float:
+        roots = self.compressibility_roots(pressure, temperature)
+        if phase == "vapor":
+            return roots[-1]
+        if phase == "liquid":
+            return roots[0]
+        if phase == "stable-single-root":
+            return roots[-1]
+        raise ValueError(f"Unsupported phase selector: {phase!r}")
+
+    @profile_property(
+        "molar_volume",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def molar_volume(
+        self,
+        pressure: float,
+        temperature: float,
+        phase: str = "vapor",
+    ) -> float:
+        z = self.compressibility_factor(pressure, temperature, phase=phase)
+        return z * UNIVERSAL_GAS_CONSTANT * temperature / pressure
+
+    @profile_property("density", layer="kernel", minimum_mode="audit")
+    def density(
+        self,
+        pressure: float,
+        temperature: float,
+        phase: str = "vapor",
+    ) -> float:
+        return self.molar_mass / self.molar_volume(pressure, temperature, phase=phase)
+
+    @profile_property(
+        "residual_specific_enthalpy",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def residual_specific_enthalpy(
+        self,
+        pressure: float,
+        temperature: float,
+        phase: str = "vapor",
+    ) -> float:
+        """Return Peng-Robinson enthalpy departure from ideal gas, J/kg."""
+        self._validate_pressure_temperature(pressure, temperature)
+        z = self.compressibility_factor(pressure, temperature, phase=phase)
+        _, B = self.reduced_parameters(pressure, temperature)
+        b = self.b_parameter
+        attractive = self.attractive_parameter(temperature)
+        d_attractive_d_temperature = (
+            self.attractive_parameter_temperature_derivative(temperature)
+        )
+        log_argument = (z + (1.0 + sqrt(2.0)) * B) / (
+            z + (1.0 - sqrt(2.0)) * B
+        )
+        residual_molar_enthalpy = (
+            UNIVERSAL_GAS_CONSTANT * temperature * (z - 1.0)
+            + (
+                temperature * d_attractive_d_temperature
+                - attractive
+            )
+            * log(log_argument)
+            / (2.0 * sqrt(2.0) * b)
+        )
+        return residual_molar_enthalpy / self.molar_mass
+
+    @profile_property(
+        "residual_specific_internal_energy_at_density",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def residual_specific_internal_energy_at_density(
+        self,
+        temperature: float,
+        density: float,
+    ) -> float:
+        """Return Peng-Robinson internal-energy departure, J/kg."""
+        self._validate_temperature(temperature)
+        if density <= 0.0:
+            raise ValueError("Density must be positive.")
+        molar_volume = self.molar_mass / density
+        b = self.b_parameter
+        if molar_volume <= b:
+            raise RecoverableTrialStateError(
+                "Molar volume must be larger than Peng-Robinson b parameter."
+            )
+        attractive = self.attractive_parameter(temperature)
+        d_attractive_d_temperature = (
+            self.attractive_parameter_temperature_derivative(temperature)
+        )
+        log_argument = (
+            molar_volume + (1.0 + sqrt(2.0)) * b
+        ) / (
+            molar_volume + (1.0 - sqrt(2.0)) * b
+        )
+        residual_molar_internal_energy = (
+            temperature * d_attractive_d_temperature - attractive
+        ) * log(log_argument) / (2.0 * sqrt(2.0) * b)
+        return residual_molar_internal_energy / self.molar_mass
+
+    @profile_property(
+        "residual_isochoric_heat_capacity_at_density",
+        layer="kernel",
+        minimum_mode="audit",
+    )
+    def residual_isochoric_heat_capacity_at_density(
+        self,
+        temperature: float,
+        density: float,
+    ) -> float:
+        """Return the constant-volume heat-capacity departure, J/kg/K."""
+        self._validate_temperature(temperature)
+        if density <= 0.0:
+            raise ValueError("Density must be positive.")
+        molar_volume = self.molar_mass / density
+        b = self.b_parameter
+        if molar_volume <= b:
+            raise RecoverableTrialStateError(
+                "Molar volume must be larger than Peng-Robinson b parameter."
+            )
+        log_argument = (
+            molar_volume + (1.0 + sqrt(2.0)) * b
+        ) / (
+            molar_volume + (1.0 - sqrt(2.0)) * b
+        )
+        residual_molar_cv = (
+            temperature
+            * self.attractive_parameter_temperature_second_derivative(temperature)
+            * log(log_argument)
+            / (2.0 * sqrt(2.0) * b)
+        )
+        return residual_molar_cv / self.molar_mass
+
+    @staticmethod
+    def _validate_temperature(temperature: float) -> None:
+        if temperature <= 0.0:
+            raise RecoverableTrialStateError("Temperature must be positive.")
+
+    @classmethod
+    def _validate_pressure_temperature(cls, pressure: float, temperature: float) -> None:
+        if pressure <= 0.0:
+            raise RecoverableTrialStateError("Pressure must be positive.")
+        cls._validate_temperature(temperature)
+
+HELIUM_PR = PengRobinsonFluid(
+    name="helium",
+    molar_mass=0.004002602,
+    critical_temperature=5.1953,
+    critical_pressure=227_460.0,
+    # Simcenter Amesim 2404 helium_eos.data.
+    acentric_factor=-0.382,
+)
+
+NITROGEN_PR = PengRobinsonFluid(
+    name="nitrogen",
+    molar_mass=0.0280134,
+    critical_temperature=126.192,
+    critical_pressure=3.3958e6,
+    acentric_factor=0.0372,
+)
+
+AIR_PR = PengRobinsonFluid(
+    name="air",
+    molar_mass=0.02896513,
+    critical_temperature=132.5306,
+    critical_pressure=3.786e6,
+    acentric_factor=0.0335,
+)
+
+
+def _real_cubic_roots(a: float, b: float, c: float) -> tuple[float, ...]:
+    """Return real roots for x**3 + a*x**2 + b*x + c = 0."""
+
+    depressed_p = b - a * a / 3.0
+    depressed_q = 2.0 * a * a * a / 27.0 - a * b / 3.0 + c
+    discriminant = (depressed_q / 2.0) ** 2.0 + (depressed_p / 3.0) ** 3.0
+    offset = -a / 3.0
+    tolerance = 1e-14
+
+    if discriminant > tolerance:
+        sqrt_discriminant = sqrt(discriminant)
+        u = _real_cube_root(-depressed_q / 2.0 + sqrt_discriminant)
+        v = _real_cube_root(-depressed_q / 2.0 - sqrt_discriminant)
+        return (u + v + offset,)
+
+    if abs(discriminant) <= tolerance:
+        u = _real_cube_root(-depressed_q / 2.0)
+        return tuple(sorted({2.0 * u + offset, -u + offset}))
+
+    if depressed_p >= 0.0:
+        raise ValueError("Unexpected cubic state with three real roots and non-negative p.")
+    radius = 2.0 * sqrt(-depressed_p / 3.0)
+    argument = (3.0 * depressed_q / (2.0 * depressed_p)) * sqrt(-3.0 / depressed_p)
+    argument = max(-1.0, min(1.0, argument))
+    theta = acos(argument) / 3.0
+    roots = [
+        radius * cos(theta - 2.0 * pi * index / 3.0) + offset
+        for index in range(3)
+    ]
+    return tuple(sorted(roots))
+
+
+def _real_cube_root(value: float) -> float:
+    if value == 0.0:
+        return 0.0
+    return (1.0 if value > 0.0 else -1.0) * abs(value) ** (1.0 / 3.0)

app/simulation/core/ports.py

@@ -0,0 +1,232 @@
+from __future__ import annotations
+
+from dataclasses import dataclass, field
+from typing import Literal
+
+
+PortKind = Literal["physical", "signal"]
+PortNominalRole = Literal["inlet", "outlet", "bidirectional", "input", "output"]
+ActualFlowDirection = Literal["in", "out", "stagnant"]
+VariableRole = Literal["effort", "flow", "stream", "signal"]
+ConnectionRule = Literal["equal", "sumToZero", "streamMix", "directed"]
+
+
+@dataclass(frozen=True)
+class PortVariableDefinition:
+    name: str
+    role: VariableRole
+    connection_rule: ConnectionRule
+    label: str = field(default="", compare=False)
+    quantity: str = field(default="", compare=False)
+    unit: str = field(default="", compare=False)
+    result_visible: bool = field(default=True, compare=False)
+    order: int = field(default=0, compare=False)
+
+    def as_interface_dict(self) -> dict[str, object]:
+        return {
+            "name": self.name,
+            "role": self.role,
+            "connectionRule": self.connection_rule,
+            "label": self.label or self.name,
+            "quantity": self.quantity or self.name,
+            "unit": self.unit,
+            "resultVisible": self.result_visible,
+            "order": self.order,
+        }
+
+
+@dataclass(frozen=True)
+class PortDefinition:
+    """Stable connector contract shared by components, XML, and the compiler."""
+
+    name: str
+    kind: PortKind
+    domain: str
+    nominal_role: PortNominalRole
+    positive_flow_direction: Literal["intoComponent"] | None = None
+    variables: tuple[PortVariableDefinition, ...] = ()
+
+    @classmethod
+    def pneumatic(
+        cls,
+        name: str,
+        *,
+        nominal_role: Literal["inlet", "outlet", "bidirectional"] = "bidirectional",
+    ) -> PortDefinition:
+        return cls(
+            name=name,
+            kind="physical",
+            domain="pneumatic",
+            nominal_role=nominal_role,
+            positive_flow_direction="intoComponent",
+            variables=(
+                PortVariableDefinition(
+                    "p",
+                    "effort",
+                    "equal",
+                    label="压力",
+                    quantity="pressure",
+                    unit="Pa",
+                    order=10,
+                ),
+                PortVariableDefinition(
+                    "m_flow",
+                    "flow",
+                    "sumToZero",
+                    label="质量流量",
+                    quantity="mass_flow",
+                    unit="kg/s",
+                    order=20,
+                ),
+                PortVariableDefinition(
+                    "h_outflow",
+                    "stream",
+                    "streamMix",
+                    label="流出比焓",
+                    quantity="specific_enthalpy",
+                    unit="J/kg",
+                    order=30,
+                ),
+                PortVariableDefinition(
+                    "volume",
+                    "signal",
+                    "directed",
+                    label="外部容积",
+                    quantity="volume",
+                    unit="m3",
+                    result_visible=False,
+                    order=40,
+                ),
+                PortVariableDefinition(
+                    "volume_flow",
+                    "signal",
+                    "directed",
+                    label="外部容积变化率",
+                    quantity="volume_flow",
+                    unit="m3/s",
+                    result_visible=False,
+                    order=50,
+                ),
+            ),
+        )
+
+    @classmethod
+    def mechanical_translational(
+        cls,
+        name: str,
+        *,
+        nominal_role: Literal["inlet", "outlet", "bidirectional"] = "bidirectional",
+    ) -> PortDefinition:
+        return cls(
+            name=name,
+            kind="physical",
+            domain="mechanical",
+            nominal_role=nominal_role,
+            positive_flow_direction="intoComponent",
+            variables=(
+                PortVariableDefinition(
+                    "x",
+                    "effort",
+                    "equal",
+                    label="位移",
+                    quantity="length",
+                    unit="m",
+                    order=10,
+                ),
+                PortVariableDefinition(
+                    "v",
+                    "effort",
+                    "equal",
+                    label="速度",
+                    quantity="velocity",
+                    unit="m/s",
+                    order=20,
+                ),
+                PortVariableDefinition(
+                    "f",
+                    "flow",
+                    "sumToZero",
+                    label="力",
+                    quantity="force",
+                    unit="N",
+                    order=30,
+                ),
+            ),
+        )
+
+    @classmethod
+    def signal(
+        cls,
+        name: str,
+        *,
+        nominal_role: Literal["input", "output"],
+        domain: str = "signal",
+    ) -> PortDefinition:
+        return cls(
+            name=name,
+            kind="signal",
+            domain=domain,
+            nominal_role=nominal_role,
+            variables=(
+                PortVariableDefinition(
+                    "signal",
+                    "signal",
+                    "directed",
+                    label="信号值",
+                    quantity="dimensionless",
+                    unit="",
+                    order=10,
+                ),
+            ),
+        )
+
+    def as_interface_dict(self) -> dict[str, object]:
+        return {
+            "name": self.name,
+            "kind": self.kind,
+            "domain": self.domain,
+            "nominalRole": self.nominal_role,
+            "positiveFlowDirection": self.positive_flow_direction,
+            "variables": [variable.as_interface_dict() for variable in self.variables],
+        }
+
+
+@dataclass
+class PortState:
+    """Python-side analogue of a Modelica fluid port."""
+
+    p: float = 0.0
+    m_flow: float = 0.0
+    h_outflow: float = 0.0
+    volume: float = 0.0
+    volume_flow: float = 0.0
+    signal: float = 0.0
+    x: float = 0.0
+    v: float = 0.0
+    f: float = 0.0
+    definition: PortDefinition | None = field(default=None, repr=False, compare=False)
+
+    @classmethod
+    def pneumatic(
+        cls,
+        name: str,
+        *,
+        nominal_role: Literal["inlet", "outlet", "bidirectional"] = "bidirectional",
+    ) -> PortState:
+        return cls(definition=PortDefinition.pneumatic(name, nominal_role=nominal_role))
+
+    @property
+    def inflow_rate(self) -> float:
+        return max(self.m_flow, 0.0)
+
+    @property
+    def outflow_rate(self) -> float:
+        return max(-self.m_flow, 0.0)
+
+    def actual_direction(self, tolerance: float = 1e-12) -> ActualFlowDirection:
+        if self.m_flow > tolerance:
+            return "in"
+        if self.m_flow < -tolerance:
+            return "out"
+        return "stagnant"
+

app/simulation/examples/__init__.py

@@ -0,0 +1 @@
+"""Reference systems and regression examples."""