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Readme.md
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<div align=left><img src="PHengLEI\Documents/PHengLEI-LOGO.png" style="zoom: 15%;"/><br>
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# 风雷软件（PHengLEI2312.v975）
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备注：主分支为master分支，更稳定，更多新功能请切换到ActiveBranch分支。
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# 风雷NCCR(PHengLEI-StructureNCCR基于PHengLEI2312.v975版本开发)
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## 1.软件简介
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    风雷软件<sup>[1,2]</sup>（PHengLEI，Platform for Hybrid ENGineering simulation of flows）是中国空气动力研究与发展中心（CARDC）研发的面向流体工程的混合CFD平台。平台以面向对象的设计理念，采用C++语言编程。2020年12月，风雷软件正式面向全国开源，与其他开源CFD软件相比，风雷软件具有扩展能力强、开发难度低、计算效率高等特点。（更多介绍请阅读PHengLEI/Documents文件夹下的**《风雷软件应用与开发指南》**）
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    风雷软件<sup>[1,2]</sup>(PHengLEI,Platform for Hybrid ENGineering simulation of flows)是中国空气动力研究与发展中心(CARDC)研发的面向流体工程的混合CFD平台。平台以面向对象的设计理念,采用C++语言编程。2020年12月,风雷软件正式面向全国开源,与其他开源CFD软件相比,风雷软件具有扩展能力强、开发难度低、计算效率高等特点。(更多介绍请阅读PHengLEI/Documents文件夹下的**《风雷软件应用与开发指南》**)
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    风雷软件更多动态和Demo请登录以下网址查看：
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- 官网地址: https://www.cardc.cn/nnw/products.aspx?t=9
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- 代码库地址：https://forge.osredm.com/PHengLEI/PHengLEI
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- 算例库地址：https://forge.osredm.com/PHengLEI/PHengLEI-TestCases
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- 论坛（常见问题、算例展示、技术分享）地址：https://osredm.com/forums/theme/38
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    风雷软件用户录制视频教程地址：
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- 视频教程：https://www.bilibili.com/video/BV1eX4y1T7yW?from=search&seid=9482198996609923785
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[1] 赵钟,等.风雷（PHengLEI）通用CFD软件设计[J]. 计算机工程与科学, 2020, 42(2): 210-219.( ZHAO Zhong, et al. Design of general CFD software PHengLEI [J]. Computer Engineering & Science, 2020, 42(2): 210-219. (in Chinese) )
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[1] 赵钟,等.风雷(PHengLEI)通用CFD软件设计[J]. 计算机工程与科学, 2020, 42(2): 210-219.( ZHAO Zhong, et al. Design of general CFD software PHengLEI [J]. Computer Engineering & Science, 2020, 42(2): 210-219. (in Chinese) )
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[2] 赵钟,等.适用于任意网格的大规模并行CFD计算框架PHengLEI[J]. 计算机学报, 2019, 42(11):2368
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-2383. ( ZHAO Zhong, et al. PHengLEI: A Large Scale Parallel CFD Framework for Arbitrary Grids [J]. Chinese Journal of Computers, 2019, 42(11): 2368-2383. (in Chinese) )
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**声明：** 若用户将该软件用于学术研究或工程应用，须在相关的论文成果的显要位置处标注基于“风雷（PHengLEI）“软件，并引用“风雷（PHengLEI）”软件相关的参考文献（例如[1]和[2]）。
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**声明:** 若用户将该软件用于学术研究或工程应用,须在相关的论文成果的显要位置处标注基于“风雷(PHengLEI)“软件,并引用“风雷(PHengLEI)”软件相关的参考文献(例如[1]和[2])。
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## 2.软件功能
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    风雷软件是一款结构/非结构通用CFD软件，计算范围覆盖低速、亚跨声速和高超声速。软件采用有限体积法求解定常/非定常的雷诺平均NS方程（RANS方程），集成了典型湍流模型，如SA、SST模型等；无粘项采用Roe、Vanleer、AUSM、Steger-Warming等格式；粘性项采用中心格式，时间推进采用LU-SGS或Block LU-SGS隐式方法求解；非定常计算时，采用双时间步方法。针对大规模问题，软件支持分区并行计算，并且使用多重网格技术加速收敛。同时，风雷软件也提供常用前/后置接口，如Gridgen、ICEM-CFD、FieldView、Tecplot等。
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实现风雷软件使用矩方法求解稀薄非平衡问题
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## 3.代码获取
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1. 环境准备，安装git，官网地址：https://git-scm.com/;
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2. 点击右上角Fork按钮；
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3. Fork完成后，将生成并跳转到新的仓库，复制新仓库版本库地址，如https://git.osredm.com/PHengLEI/PHengLEI.git;
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4. 在本地选择一个目录，右键打开git bash，输入命令进行代码克隆，如git clone https://git.osredm.com/PHengLEI/PHengLEI.git;
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5. 输入用户名和密码，其中用户名是指上面命令中p开头的用户名，比如p68217053；
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6. 项目克隆完成后，进入项目目录，默认分支为master分支，可通过命令切换到ActiveBranch分支，如git checkout ActiveBranch;
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7. 切换到开发分支后，可输入git log查看日志，确认当前版本。
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1. 环境准备,安装git,官网地址:https://git-scm.com/;
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2. 点击右上角Fork按钮;
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3. Fork完成后,将生成并跳转到新的仓库,复制新仓库版本库地址,https://osredm.com/p86739025/PHengLEI-NCCR.git;
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4. 在本地选择一个目录,右键打开git bash,输入命令进行代码克隆,如git clone https://git.osredm.com/PHengLEI/PHengLEI.git;
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5. 输入用户名和密码,其中用户名是指上面命令中p开头的用户名,比如p68217053
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## 4.软件安装
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    风雷软件能够在Windows、Linux、Mac系统下运行，源代码采用C++语言编写，需要CMake软件构建项目，并行计算采用MPI库。因此，操作系统必须提供C++编译器、CMake2.8以上版本软件和MPI1.0或MPI2.0标准库。
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    风雷软件能够在Windows、Linux、Mac系统下运行,源代码采用C++语言编写,需要CMake软件构建项目,并行计算采用MPI库。因此,操作系统必须提供C++编译器、CMake2.8以上版本软件和MPI1.0或MPI2.0标准库。
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本程序同风雷主软件编译方法一致,无需特殊步骤。
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### 4.1 Windows环境配置
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    Windows环境下所有必备软件按照默认步骤安装即可。
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1. 安装Microsoft Visual Studio 2012以上版本；
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2. 安装MPI库，推荐采用MSMPI；
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1. 安装Microsoft Visual Studio 2012以上版本;
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2. 安装MPI库,推荐采用MSMPI;
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3. 安装Cmake。
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### 4.2 Linux环境配置
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    Linux环境配置的简要步骤如下：
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    Linux环境配置的简要步骤如下:
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1. 安装Cmake；
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2. 安装MPICH3库；
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3. 编译HDF5库；
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4. 编译CGNS库；
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1. 安装Cmake;
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2. 安装MPICH3库;
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3. 编译HDF5库;
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4. 编译CGNS库;
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5. 编译metis库和parmetis库。
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**备注：**Linux环境配置的具体步骤请阅读《风雷软件应用与开发指南》。
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**备注:**Linux环境配置的具体步骤请阅读《风雷软件应用与开发指南》。
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## 5.如何贡献
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    针对基于风雷软件进行二次开发的用户，后续添加如何测试、提交Pull Request的步骤。
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    软件贡献者信息参见项目根目录下的Contributing文件（待增加）。
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## 6.软件版权
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## 5.软件版权
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    风雷软件开源协议参见项目根目录下的LICENSE文件。
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## 7.鸣谢
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## 6.鸣谢
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    感谢所有参与风雷软件开发与推广的工作人员，也感谢所有支持风雷软件发展并提出宝贵意见和建议的广大用户。
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    感谢风雷研发团队的辛苦付出,感谢浙江大学陈伟芳教授和赵文文副教授的亲切指导。
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## 8.联系我们
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## 7.联系我们
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    电子邮箱：phenglei@126.com。
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    电子邮箱:yangjy2022@zju.edu.cn。
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# nBoundaryConditions: Number of global boundary conditions.
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# bcName : Boundary condition name.
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# bcType(in PHengLEI): Boundary condition type.
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# How to set boundary condition, for example:
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# string bcName = "Wall";
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# {
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# int bcType = 2;
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# int viscousType = 1;
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# double wallTemperature = -1.0;
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# double uWall = 0.0;
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# double vWall = 0.0;
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# double wWall = 0.0;
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# }
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# string bcName = "Inflow";
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# {
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# int bcType = 5;
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# int inflowParaType = 0;
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# double refMachNumber = 0.73;
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# double attackd = 2.79;
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# double angleSlide = 0.0;
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# double refReNumber = 6.5e6;
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# double refDimensionalTemperature = 288.15;
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# }
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# For more information, see examples/bin/boundary_condition.hypara file!!!
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int nBoundaryConditions = 4;
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string bcName = "SOLID_SURFACE";
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{
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string bodyName = "body";
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int bcType = 2;
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}
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string bcName = "SYMMETRY";
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{
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int bcType = 3;
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}
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string bcName = "INFLOW";
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{
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int bcType = 5;
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}
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string bcName = "OUTFLOW";
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{
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int bcType = 6;
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}
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# 'bcType' is defined as following:
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# -2: WAKE
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# -1: INTERFACE
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# 0 : NO_BOUNDARY_CONDITION
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# 1 : EXTRAPOLATION
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# 2 : SOLID_SURFACE
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# 3 : SYMMETRY
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# 4 : FARFIELD
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# 5 : INFLOW
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# 6 : OUTFLOW
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# 52: PRESSURE_INLET
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# 62: PRESSURE_OUTLET
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# 61: OUTFLOW_CONFINED
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# 7 : POLE
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File diff suppressed because it is too large
Load Diff
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#########################################################################
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# General Control Parameter #
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#########################################################################
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// maxSimuStep: The max simulation step, don't care simulation is restart or not.
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// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
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// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
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// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
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// intervalStepRes: The step intervals for residual 'res.dat' saved.
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int maxSimuStep = 200000;
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int intervalStepFlow = 100000;
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int intervalStepPlot = 100000;
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int intervalStepForce = 10000;
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int intervalStepRes = 10000;
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int isCalRarefied = 0;
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#########################################################################
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# Inflow Parameter #
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#########################################################################
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// refMachNumber: Mach number.
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// attackd: Angle of attack.
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// angleSlide: Angle of sideslip.
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// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
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// inflowParaType: The type of inflow parameters.
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// 0 -- the nondimensional conditions.
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// 1 -- the flight conditions.
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// 2 -- the experiment conditions.
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// 3 -- the subsonic boundary conditions.
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// 4 -- the condition that the velocity, temperature and density are given.
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// 5 -- the condition that the velocity, temperature and pressure are given.
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// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
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// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
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// freestream_vibration_temperature: Dimensional freestream vibration temperature.
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// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
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// height: Fly height, unit of km.
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// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
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// 1 dm = 0.1 m.
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// 1 cm = 0.01 m.
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// 1 mm = 0.001m.
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// 1 inch = 0.0254m.
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// 1 foot = 12 inches = 0.3048m.
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// 1 yard = 3 feet = 0.9144m.
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// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
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// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
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double refMachNumber = 5;
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double attackd = 0.00;
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double angleSlide = 0.00;
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double wallTemperature = 273;
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//The velocity, temperature and pressure are fixed.
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int inflowParaType = 5;
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double refDimensionalVelocity = 1683.7932;
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double refDimensionalTemperature = 273;
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double refDimensionalPressure = 4.8788;
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double gridScaleFactor = 1.0;
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double forceReferenceLengthSpanWise = 1.0; // unit of meter.
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double forceReferenceLength = 1.0; // unit of meter.
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double forceReferenceArea = 1.0; // unit of meter^2.
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double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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double TorqueRefZ = 0.0; // unit of meter.
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double knudsenLength = 1.0; // unit of meter.
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#########################################################################
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# Physical models #
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#########################################################################
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// viscousType: Viscous model.
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// 0 -- Euler.
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// 1 -- Laminar.
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// 3 -- 1eq turbulent.
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// 4 -- 2eq turbulent.
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// viscousName: Laminar or tubulent model.
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// -- "1eq-sa", when viscousType = 3.
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// -- "2eq-kw-menter-sst", when viscousType = 4.
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// DESType: Type of DES.
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// 0 -- RANS.(default)
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// 1 -- DES.
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// 2 -- DDES.
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// 3 -- IDDES.
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//int viscousType = 0;
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//string viscousName = "Euler";
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int viscousType = 1;
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string viscousName = "laminar";
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//int viscousType = 3;
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//string viscousName = "1eq-sa";
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//int viscousType = 4;
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//string viscousName = "2eq-kw-menter-sst";
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int DESType = 0;
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int roeEntropyFixMethod = 3;
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double roeEntropyScale = 1.0;
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#########################################################################
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# Spatial Discretisation #
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#########################################################################
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#*******************************************************************
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# Struct Solver *
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#*******************************************************************
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// inviscidSchemeName: Spatial discretisation scheme of struct grid.
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// Using this when solve structered grid or hybrid.
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// -- "vanleer", "steger", "ausmpw", "ausmpw+".
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// str_limiter_name: Limiter of struct grid.
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// -- "minmod", "3rd_minmod_smooth", "vanalbada".
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string inviscidSchemeName = "ausmpw+";
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string str_limiter_name = "vanalbada";
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#*******************************************************************
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# UnStruct Solver *
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#*******************************************************************
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// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
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// Using this when solve Unstructered grid or hybrid.
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// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
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// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
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// uns_limiter_name: Limiter of Unstruct grid.
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// -- "vencat", "barth".
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// -- "1st", meaning accuracy of first-order.
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// -- "nolim", no limiter.
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// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
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// The smaller the value, the more robust it is.
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string uns_scheme_name = "vanleer";
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string uns_limiter_name = "vencat";
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double venkatCoeff = 0.5;
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#########################################################################
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# Temporal Discretisation #
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#########################################################################
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// iunsteady: Steady or unsteady.
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// 0 -- steady.
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// 1 -- unsteay.
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// CFLEnd: The CFL number, [0.1, 100].
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// The bigger the value, the convergence faster but lower robustness.
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// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
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int iunsteady = 0;
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double CFLEnd = 10.0;
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double ktmax = 1.0e10;
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#########################################################################
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# File In or Out #
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#########################################################################
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// gridfile: The partitioned Grid file path, using relative path,
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// which is relative to the working directory.
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// IMPORTANT WARNING: The file index should be ignored,
|
||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/bluntcylinder_4.fts";
|
||||
int plotFieldType = 1;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
|
||||
// visualVariables: Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- viscosityLaminar(7), viscosityTurbulent(8),
|
||||
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
|
||||
// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
|
||||
// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
|
||||
// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
|
||||
// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40).
|
||||
// -- Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 12;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15, 38, 39, 40, 60];
|
||||
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23) , -Knudsen number(Kn_wall, 24)
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// limitVariables: Limit model (It is useful only if limitVector is 0).
|
||||
// 0 -- limit only for pressure and denstiny, then get the min value.
|
||||
// 1 -- limit for every variables, then get the min value.
|
||||
// limitVector:
|
||||
// 0 -- Each variable use the same limiter coefficient.
|
||||
// 1 -- Each variable use the respective limiter coefficients.
|
||||
// reconmeth:
|
||||
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
||||
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
|
||||
|
||||
int reconmeth = 0;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 1;
|
||||
|
||||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// isAdaptiveSolver: isAdaptiveSolver=0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
// nchemrad:
|
||||
// 0 -- compute the spectrum radius without considering chemical reaction flow.
|
||||
// 1 -- compute the spectrum radius that need to count the contribution from chemical reaction flow.
|
||||
// ntmodel: The thermodynamic temperature model.
|
||||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nContinueModel: The new continue model can switch different computation model.
|
||||
// 0 -- Not use the new continue model.
|
||||
// 1 -- use the new continue model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType: the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// For self-definition model, the gasfile is used to indicate the file path of the new gas model.
|
||||
// speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma.
|
||||
// initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName.
|
||||
// ifStartFromPerfectGasResults: The chemical reaction simulation is start from perfect gas flowfield or not, 0 is for no and else is for yes.
|
||||
// nIterFirstStep : the maximum number of iteration in the first step for the self-adaptive calculation.
|
||||
// nIterSecondStep : the maximum number of iteration in the second step for the self-adaptive calculation.
|
||||
// nIterThirdStep : the maximum number of iteration in the third step for the self-adaptive calculation.
|
||||
// nEnergyAssembly : the vibration energy is computed with combined method which includes the fitting method and the molecular kinetic theory.
|
||||
// 0 -- no,
|
||||
// 1 -- yes.
|
||||
// nControlVariable: the variable to computing the residual error that determines the convergence is meet or not in the one-temperature model.
|
||||
// 0 -- the density.
|
||||
// 1 -- the translation temperature.
|
||||
// 2 -- the vibration temperature.
|
||||
// 3 -- the electron temperature.
|
||||
// 4 -- the pressure.
|
||||
// 5 -- the mass fraction of oxygen.
|
||||
// 6 -- the mass fraction of nitrogen.
|
||||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// isMoleFractionType : 1 indicates the mass fractions, or else the mole fractions.
|
||||
|
||||
int isAdaptiveSolver = 0;
|
||||
int nIterFirstStep = 1000;
|
||||
int nIterSecondStep= 2000;
|
||||
int nIterThirdStep = 2000;
|
||||
int nEnergyAssembly = 0;
|
||||
int nControlVariable = 1;
|
||||
double firstStepError = 0.01;
|
||||
double secondStepError = 0.001;
|
||||
double thirdStepError = 0.001;
|
||||
|
||||
int nGasModel = 3;
|
||||
int nchem = 0;
|
||||
int ntmodel = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 1.0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
string gasfile = "DK5";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.07955, 0.134, 0.0509, 1.0e-9, 0.73555";
|
||||
int isMoleFractionType = 0;
|
||||
int nContinueModel = 1;
|
||||
int nRapidFlowfield = 0;
|
||||
int nSurfHeatMonitor = 1;
|
||||
double radiationCoef = 0.8;
|
||||
|
|
@ -0,0 +1,37 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating.
|
||||
// axisRotateOrder : axis rotating order.
|
||||
// 1 -- X-axis.
|
||||
// 2 -- Y-axis.
|
||||
// 3 -- Z-axis.
|
||||
// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE.
|
||||
// 1 -- PHengLEI, *.fts.
|
||||
// 2 -- CGNS, *.cgns.
|
||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||
// 5 -- Fluent, *.cas/*.msh.
|
||||
// 6 -- Ustar, mgrid.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
// 9 -- Gridgen type of structured grid, *.dat/*.grd.
|
||||
|
||||
int gridtype = 1;
|
||||
int nAxisRotateTimes = 0;
|
||||
int axisRotateOrder[] = [1, 2, 3];
|
||||
double axisRotateAngles[] = [0.0, 0.0, 0.0];
|
||||
int from_gtype = 9;
|
||||
|
||||
#########################################################################
|
||||
# File path #
|
||||
#########################################################################
|
||||
// from_gfile: path of original data file for unstructure grid convert from.
|
||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||
string from_gfile = "./grid/grid.dat";
|
||||
string out_gfile = "./grid/bluntcylinder.fts";
|
||||
|
|
@ -0,0 +1,52 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE: DON NOT MODIFY THE FOWLLOWING LINE.
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid, 2 or 3.
|
||||
// nparafile: the number of parameter files.
|
||||
// nsimutask: simulation task type.
|
||||
// 0 -- CFD Solver of NS or Turbulation.
|
||||
// 1 -- Grid generation: for special typical cases, such as cylinder, flat plate, etc.
|
||||
// Grid conversion: from other format to PHengLEI format (.fts).
|
||||
// Grid reconstruction: such as grid adaptation.
|
||||
// Grid merging: merge two blocks into one block.
|
||||
// Grid repairing: repair the original grid in order to remove the negative volume cells.
|
||||
// 2 -- Wall distance computation for turb-solver.
|
||||
// 3 -- Grid partition.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
//string parafilename = "./bin/cfd_para_subsonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
||||
string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
||||
//string parafilename = "./bin/cfd_para_incompressible.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_para.hypara";
|
||||
|
||||
//int nsimutask = 2;
|
||||
//string parafilename = "./bin/cfd_para.hypara";
|
||||
|
||||
//int nsimutask = 3;
|
||||
//string parafilename = "./bin/partition.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_deform_para.hypara";
|
||||
|
||||
//int nsimutask = 1;
|
||||
//string parafilename = "./bin/grid_refine_para.hypara";
|
||||
|
||||
//int nsimutask = 14;
|
||||
//string parafilename = "./bin/integrative_solver.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,24 @@
|
|||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// maxproc: The number of partition zones that want to be divided into,
|
||||
// which is equal to the number of CPU processors you want.
|
||||
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
|
||||
// 30~70 thousands unstructured cells per CPU-Core is suggested.
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/bluntcylinder.fts";
|
||||
string partition_grid_file = "./grid/bluntcylinder_4.fts";
|
||||
|
||||
int numberOfMultifile = 1;
|
||||
|
||||
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level.
|
||||
// 2 -- 2 level.
|
||||
// N -- N level,..., et al.
|
||||
int numberOfMultigrid = 1;
|
||||
Binary file not shown.
|
|
@ -0,0 +1,23 @@
|
|||
# Boundary Face Information of Grid ./grid/bluntcylinder.fts
|
||||
# nBoundaryConditions: number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
int nBoundaryConditions = 4;
|
||||
string bcName = "SOLID_SURFACE";
|
||||
{
|
||||
string bodyName = "body";
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "SYMMETRY";
|
||||
{
|
||||
int bcType = 3;
|
||||
}
|
||||
string bcName = "INFLOW";
|
||||
{
|
||||
int bcType = 5;
|
||||
}
|
||||
string bcName = "OUTFLOW";
|
||||
{
|
||||
int bcType = 6;
|
||||
}
|
||||
Binary file not shown.
Binary file not shown.
Binary file not shown.
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,18 @@
|
|||
FVBND 1 3
|
||||
No_Boundary_Condition
|
||||
Solid_Surface
|
||||
Symmetry
|
||||
Farfield
|
||||
Inflow
|
||||
Outflow
|
||||
Pole
|
||||
Generic_#1
|
||||
Generic_#2
|
||||
Generic_#3
|
||||
BOUNDARIES
|
||||
3 1 1 101 1 101 1 1
|
||||
3 1 1 101 1 101 4 4
|
||||
3 1 1 1 1 101 1 4
|
||||
6 1 101 101 1 101 1 4
|
||||
5 1 1 101 1 1 1 4
|
||||
2 1 1 101 101 101 1 4
|
||||
|
|
@ -0,0 +1,11 @@
|
|||
1
|
||||
1
|
||||
101 101 4
|
||||
blk-1
|
||||
6
|
||||
1 101 1 101 1 1 3
|
||||
1 101 1 101 4 4 3
|
||||
1 1 1 101 1 4 3
|
||||
101 101 1 101 1 4 6
|
||||
1 101 1 1 1 4 5
|
||||
1 101 101 101 1 4 2
|
||||
Loading…
Reference in New Issue