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README.md
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README.md
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#### 从命令行创建一个新的仓库
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# 国家数值风洞风雷软件算例库
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```bash
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touch README.md
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git init
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git add README.md
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git commit -m "first commit"
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git remote add origin https://git.osredm.com/p68217053/PHengLEI-TestCases.git
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git push -u origin master
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<img src="logo.png" alt="banner" style="zoom: 33%;" />
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[](https://img.shields.io/badge/build-passing-brightgreen) [](LICENSE) 
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国家数值风洞风雷软件算例库，包含Rae2822、Plate、Cylinder、30p30n、Sphere、NACA0012、M6、Electre、DoubleEllipse、CHNT等多种模型算例，正在持续更新中。
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## 导航
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- [使用说明](#使用说明)
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- [算例库中英文对照表](#算例库中英文对照表)
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- [License](#license)
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## 使用说明
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本算例库配套国家数值风洞风雷软件使用，使用时应切换到对应的版本。
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具体使用说明如下：
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```shell
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# 1、查看历史版本号，记住你需要的版本hash值
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# 如： f3ef592
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git log
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# 2、使用第一步得到的hash值，切换到对应版本
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git reset --hard f3ef592
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# 3、使用国家数值风洞风雷软件进行测试和计算
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```
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#### 从命令行推送已经创建的仓库
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```bash
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git remote add origin https://git.osredm.com/p68217053/PHengLEI-TestCases.git
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git push -u origin master
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```
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## 算例库中英文对照表
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二维结构
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| 中文 | 英文 |
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| -------------------------: | :--------------------------------- |
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| 二维结构高阶圆柱 | TwoD_Cylinder_Laminar_HighOrder_Struct |
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| 二维结构低速层流平板 | TwoD_Plate_Laminar_Struct_1CPU |
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| 二维结构高速层流平板 | TwoD_Plate_Laminar_Ma5_Struct_1CPU |
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| 二维结构低速湍流平板 | TwoD_LowMach_plate_SST_Struct |
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| 二维结构高速湍流平板 | TwoD_Plate_SST_Ma5_Struct_1CPU |
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| 二维结构圆柱高速绕流 | TwoD_Cylinder_Laminar_Ma8d03_Struct |
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| 二维结构圆柱化学非平衡 | TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct |
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| 二维结构30p30n翼型低速绕流 | TwoD_30p30n_SST_Struct |
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| 二维结构30p30n翼型低速绕流 | TwoD_30p30n_SST_Struct |
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| 二维结构Rae2822翼型跨声速绕流 | TwoD_Rae2822_SST_Struct |
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三维结构
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| 中文 | 英文 |
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| -------------------------: | :--------------------------------- |
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| 三维结构高阶双椭球 | ThreeD_DoubleEllipse_Laminar_HighOrder_Struct |
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| 三维结构球头高速绕流 | ThreeD_Sphere_Laminar_Ma10_Struct |
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| 三维结构圆柱LES模拟 | ThreeD_Cylinder_LES_Re3900_Struct |
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| 三维结构客机标模模拟 | ThreeD_CHNT_SST_Struct_16CPU |
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| 三维结构钝锥化学非平衡 | ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct |
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| 三维结构M6机翼跨声速绕流 | ThreeD_M6_SST_Struct_MG2_4CPU |
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| 三维结构NACA0012翼型低速绕流 | ThreeD_NACA0012_SA_Struct |
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其他算例正在持续更新中。
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## License
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[GPL](LICENSE)
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@ -0,0 +1,809 @@
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//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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// PPPPP H H EEEEE N N GGGGG L EEEEE III +
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// P P H H E NN N G L E I +
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// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
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// P H H E N N N G G L E I +
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// P H H EEEEE N N GGGGG LLLLL EEEEE III +
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//------------------------------------------------------------------------+
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// Platform for Hybrid Engineering Simulation of Flows +
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// China Aerodynamics Research and Development Center +
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// (C) Copyright, Since 2010 +
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//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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###########################################################################
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# Default parameters for Grid conversion #
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###########################################################################
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// gridtype: Grid type for generation, conversion, reconstruction, merging.
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// 0 -- Unstructured grid.
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// 1 -- Structured grid.
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// 2 -- Hybrid grid, include both of unstructured and structured grid.
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// gridobj: Task type of grid treatment.
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// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
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// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
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// 2 -- Grid refinement.
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// 3 -- Grid merging, merge two blocks into one block.
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// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
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// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
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// multiblock: Multi-block grid or not, only for structured grid conversion.
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// 0 -- Not.
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// 1 -- Yes.
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// grid_database_index: Case of typical case, only for gridobj=0.
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// 1 -- Laminar flat plate of subsonic flow.
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// 2 -- Laminar flat plate of supersonic flow.
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// 3 -- Turbulent flat plate of subsonic flow.
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// 4 -- Turbulent flat plate of supersonic flow.
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// iadapt: Adaptation number for unstructure grid.
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// iovrlap: Overlapping(overset) grid or not.
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// 0 -- NON-overlapping grid.
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// 1 -- Overlapping grid.
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// SymmetryFaceVector: The vector of symmetry face.
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// 0 -- X axis.
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// 1 -- Y axis.
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// 2 -- Z axis.
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int gridtype = 0;
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int gridobj = 1;
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int multiblock = 0;
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int grid_database_index = 3;
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int iadapt = 0;
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int iovrlap = 0;
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int SymmetryFaceVector = 1;
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// axisup: Type of Cartisien coordinates system, used in grid conversion.
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// 1 -- Y upward. (default)
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// 2 -- Z upward.
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int axisup = 1;
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// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
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// 0 -- Interface. (default)
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// 1 -- Physical boundary condition, used in Hybrid solver.
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int omit_no_bound_bc = 0;
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//-----------------------------------------------------------------------
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# Grid data type #
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//-----------------------------------------------------------------------
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// from_gtype/to_gtype: Type of grid data type in grid conversion process.
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// -1 -- MULTI_TYPE.
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// 1 -- PHengLEI, *.fts.
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// 2 -- CGNS, *.cgns.
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// 3 -- Plot3D type of structured grid, *.dat/*.grd.
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// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
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// 5 -- Fluent, *.cas/*.msh.
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// 6 -- Ustar, mgrid.in.
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// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
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// 8 -- GMSH, *.msh.
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// dumpOldGrid: If dump out the old grid file.
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// 0 -- Not. (default)
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// 1 -- Yes.
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int from_gtype = 2;
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int to_gtype = 1;
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int dumpOldGrid = 0;
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//-----------------------------------------------------------------------
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# File path #
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//-----------------------------------------------------------------------
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// from_gfile: path of original data file for unstructure grid convert from.
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// out_gfile: path of target file for grid convert to, *.fts type of file usually.
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string from_gfile = "./grid/rae2822_hybrid2d.cas";
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string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
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// ----------------- some advanced choices ------------------------------
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// iunsteady: The Grid is for unsteady simulation or not.
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int iunsteady = 0;
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int iale = 0;
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// fileformat: Ustar Grid file format.
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// 0 -- BINARY.
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// 1 -- ASCII.
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int fileformat = 0;
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// .skl meaning skeleton.
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string original_grid_info_file = "./grid/FLUENT_test.skl";
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// Parameters for hybrid solver.
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// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
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// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
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// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
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string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
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string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
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string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
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// Some parameters for structured overlapping grid.
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int codeOfDigHoles = 1;
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string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
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string holeFullFileName = "./oversetGridView/holeFullFile.dat";
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string linkFileName = "./oversetGridView/topology.dat";
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string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
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// ----------------- Adaptive Mesh Refine -------------------------------
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// In this file, the original_grid_file is used of the partition part.
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// If use it dependently, abstract it here.
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string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
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string geometryFileName = "./grid/jsm.igs";
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// geometryUnit: Geometry unit.
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// 1 -- meter.
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// 2 -- millimeter.
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// 3 -- inch.
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// exclusiveCase: Parallel projection exclusive case.
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// 0 -- NON case.
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// 1 -- JSM-C2-NPOFF case.
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// 2 -- CHNT.
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// projectOrgPoint: If the original wall points need to be projected or not.
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int geometryUnit = 1;
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int anisoRefine = 0;
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int isProject = 0;
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int readDist = 0;
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int isDeform = 0;
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int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
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int projectOrgPoint = 0; // if project original wall points.
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// ----------------- RBF Parameters -------------------------------------
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// symmetryPlane: Which symmetry plane is used in the mesh.
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// 0 -- without symmetry.
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// 1 -- plane of x=0.
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// 2 -- plane of y=0.
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// 3 -- plane of z=0.
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int numberOfReferenceCP = 10;
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double influenceRadius = 20;
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int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
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#########################################################################
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# Default parameters for Partition #
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#########################################################################
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// pgridtype: The grid type.
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// 0 -- unstruct grid.
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// 1 -- struct grid.
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// 2 -- refine structured grid.
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// maxproc: The number of partition zones that want to be divided into.
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int pgridtype = 0;
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int maxproc = 4;
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// traceMark: Trace mark or not, only for structured grid partition.
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// 0 -- Not.
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// 1 -- Yes.
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// blockIndexOfMark: the block index of mark, only for structured grid partition.
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// cellIndexOfMark: the cell index of mark, only for structured grid partition.
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int traceMark = 0;
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int blockIndexOfMark = 0;
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int cellIndexOfMark[] = [185,30,1];
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//-----------------------------------------------------------------------
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# File path #
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//-----------------------------------------------------------------------
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// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
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// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
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string original_grid_file = "./grid/sphere_mixed.fts";
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string partition_grid_file = "./grid/sphere_mixed__4.fts";
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// ------------------ Sompe advanced parameters -------------------------
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// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
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// 0 -- Interface. (default)
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// 1 -- Physical boundary condition, used in Hybrid solver.
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// npartmethod: Method of interface reconstruction, default is 1.
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// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
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// 1 -- Using ParMetis for homogeneous MPI.
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// 2 -- Using Metis for homogeneous MPI.
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// 3 -- using METIS partition for homogeneous OpenMP.
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// parmetisBalance: Used to specify the imbalance tolerance.
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// 1 -- perfect balance.
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// maxproc -- perfect imbalance.
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// 1.05 -- recommended.
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int omit_no_bound_bc = 0;
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int npartmethod = 1;
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int parallelPartitionMethod = 2;
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double parmetisBalance = 1.05;
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// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
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// 1 -- single level.
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// 2 -- 2 level.
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// N -- N level, ..., et al.
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int numberOfMultigrid = 1;
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#########################################################################
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# Default parameters for CFD simulation #
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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 file 'res.dat' saved.
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// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
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// 0 -- no precondition process. (default, mach > 0.3)
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// 1 -- carry out precondition process. (mach number <= 0.3)
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int maxSimuStep = 20000;
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int intervalStepFlow = 1000;
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int intervalStepPlot = 1000;
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int intervalStepForce = 100;
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int intervalStepRes = 10;
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int ifLowSpeedPrecon = 0;
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// compressible:
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// 0 -- incompressible flow.
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// 1 -- compressible flow. (default)
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int compressible = 1;
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//-----------------------------------------------------------------------
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# CFD Control 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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// 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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// 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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// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
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// dump_Q: Dump out thermal flux Q of solid wall.
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// 0 -- no dump out.
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// 1 -- dump out wall Q only.
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// 2 -- dump out wall Q & the typical position Q of ball.
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// 3 -- dump out wall Q & the typical position Q of cone.
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// 4 -- dump out wall Q & the typical position Q of double sphere.
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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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// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: 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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// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
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// condition is radiation equilibrium temperature, and 0.8 is the default value.
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double refMachNumber = 0.73;
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double attackd = 2.79;
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double angleSlide = 0.00;
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int inflowParaType = 0;
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double refReNumber = 6.5e6;
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double refDimensionalTemperature = 288.15;
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double freestream_vibration_temperature = 10000.00;
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//int inflowParaType = 1;
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//double height = 0.001;
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//int inflowParaType = 2;
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//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
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//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
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//int inflowParaType = 3;
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//int nsubsonicInlet = 1;
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//int nsubsonicOutlet = 1;
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//string inLetFileName = "./bin/subsonicInlet.hypara";
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//string outLetFileName = "./bin/subsonicOutlet.hypara";
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//double refDimensionalTemperature = 288.144;
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//double refDimensionalPressure = 1.01313E05;
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double wallTemperature = -1.0;
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int dump_Q = 0;
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double radiationCoef = 0.8;
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double gridScaleFactor = 1.0;
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double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceArea = 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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// directionMethod: The method of determining direction.
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// 1 -- using direciton.
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// 2 -- using face normal.
|
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// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
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// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
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// direction_inlet: The direction of inlet.
|
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// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
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// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
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// direction_outlet: The direction of outlet.
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int directionMethod = 2;
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double subsonicInletTotalPressure = 1.2e6;
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double subsonicInletTotalTemperature = 1300;
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double direction_inlet[] = 1, 0, 0;
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double subsonicOutletTotalPressure = 17.8571428;
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double subsonicOutletTotalTemperature = 1.0;
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double direction_outlet[] = 1, 0, 0;
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//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,205 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 15000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 10;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 0.785;
|
||||
double attackd = 2.61;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.703665e7;
|
||||
double refDimensionalTemperature = 298.15;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 0.1937; // unit of meter.
|
||||
double forceRefenenceArea = 0.12892; // unit of meter^2.
|
||||
double TorqueRefX = 0.66087; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
int viscousType = 4;
|
||||
string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "roe", "vanleer", "ausm+up", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "3rdsmooth", "smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "smooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 5.0;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 30.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/stm-dkbm-c-all__16.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
||||
double MUSCLCoefXk = 0.333333;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/stm-dkbm-c-all.grd";
|
||||
string out_gfile = "./grid/stm-dkbm-c-all.fts";
|
||||
|
|
@ -0,0 +1,51 @@
|
|||
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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,21 @@
|
|||
// 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).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 16;
|
||||
|
||||
string original_grid_file = "./grid/stm-dkbm-c-all.fts";
|
||||
string partition_grid_file = "./grid/stm-dkbm-c-all__16.fts";
|
||||
|
||||
// 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.
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,2 @@
|
|||
本网格由一个1400万的网格粗化8倍而来，仅供示意，对计算结果准确性不做保证。
|
||||
bin参数文件没有问题。
|
||||
|
|
@ -0,0 +1,838 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 3000;
|
||||
|
||||
int intervalStepFlow = 100;
|
||||
int intervalStepPlot = 100;
|
||||
int intervalStepForce = 1;
|
||||
int intervalStepRes = 1;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: the radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.20;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 3900;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The total pressure of subsonic inlet.
|
||||
// subsonicInletTotalTemperature: The total temperature of subsonic inlet.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The total pressure of subsonic outlet.
|
||||
// subsonicOutletTotalTemperature: The total temperature of subsonic outlet.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// limitVariables: Limit model.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int iviscous = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 1;
|
||||
double physicalTimeStep = 0.005;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 0;
|
||||
|
||||
int min_sub_iter = 20;
|
||||
int max_sub_iter = 20;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 1;
|
||||
|
||||
int RKStage = 2;
|
||||
double [] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/cylinder_Re3900_270w_split120.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 1;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 10;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 11, 12, 15];;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e5;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES : Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - not;
|
||||
// sgsmodel : subgrid scale model
|
||||
// = "smagorinsky" ;
|
||||
// = "dsm" ;
|
||||
// = "wale" ;
|
||||
// deltaFunctionType : = 1 - MAX(deltai, deltaj, deltak)
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3)
|
||||
// = 3 - Devloped by Scotti
|
||||
// wallDampingFunctionType : = 0 - no wall function
|
||||
// = 1 - van Driest
|
||||
// = 2 - developed by Dr. Deng Xiaobing
|
||||
// = 3 - developed by Piomelli
|
||||
// turbViscousCutType : turbulent viscosity cut type
|
||||
// = 0 - mu_total = mut + mul
|
||||
// = 1 - mu_total = max(mut-mul,0)+ mul
|
||||
// = 2 - mu_total = max(mut ,0)+ mul
|
||||
// smagConstant : constant of smagorinsky model.
|
||||
// waleConstant : constant of wale model
|
||||
// filterDirection[3] : filter variables in i, j, k direction or not;
|
||||
// averageDirection[3] : average variables in i, j, k direction or not;
|
||||
// isotropicConstant : constant of isotropic part of SGS stress
|
||||
|
||||
int iLES = 1;
|
||||
string sgsmodel = "smagorinsky";
|
||||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [1, 1, 0];
|
||||
double testFilterScale = 2.0;
|
||||
int averageWidth = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = 0.8;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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, nMGLevel.in.
|
||||
// 7 -- Hybrid, include both of unstructured and structured grid, *.fts.
|
||||
// 8 -- GMSH, *.msh.
|
||||
int gridtype = 1;
|
||||
int axisup = 2;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/cylinder_Re3900_270w_split120.grd";
|
||||
string out_gfile = "./grid/cylinder_Re3900_270w_split120.fts";
|
||||
|
|
@ -0,0 +1,41 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
//int nsimutask = 0;
|
||||
//string parafilename="./bin/cfd_para.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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = "./bin/cfd_para.hypara"
|
||||
string parafilename2 = "./bin/cfd_para.hypara";
|
||||
|
|
@ -0,0 +1,20 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 128;
|
||||
|
||||
string original_grid_file = "./grid/cylinder_Re3900_270w.fts";
|
||||
string partition_grid_file = "./grid/cylinder_Re3900_270w_128.fts";
|
||||
|
||||
|
||||
// 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 +1,119 @@
|
|||
1
|
||||
9
|
||||
81 5 93
|
||||
blk-4
|
||||
6
|
||||
-1 -81 1 5 1 1 -1
|
||||
-1 -81 1 5 85 85 3
|
||||
1 81 1 5 93 93 4
|
||||
1 1 1 5 -1 -93 -1
|
||||
35 35 1 5 -85 -177 9
|
||||
81 81 1 5 -1 -93 -1
|
||||
1 1 1 5 -85 -177 6
|
||||
1 81 1 1 1 93 99
|
||||
1 81 5 5 1 93 99
|
||||
81 5 89
|
||||
blk-3-split-1
|
||||
6
|
||||
81 1 1 5 1 1 2
|
||||
-1 -81 1 5 89 89 -1
|
||||
-1 -81 1 5 1 1 3
|
||||
1 1 1 5 -89 -1 -1
|
||||
69 69 1 5 -89 -1 5
|
||||
81 81 1 5 -89 -1 -1
|
||||
1 1 1 5 -89 -1 4
|
||||
81 1 1 1 1 89 99
|
||||
81 1 5 5 1 89 99
|
||||
81 5 85
|
||||
blk-3-split-2
|
||||
6
|
||||
-1 -81 1 5 1 1 -1
|
||||
-1 -81 1 5 89 89 2
|
||||
-1 -81 1 5 85 85 -1
|
||||
-1 -81 1 5 1 1 1
|
||||
1 1 1 5 -1 -85 -1
|
||||
35 35 1 5 -1 -85 9
|
||||
81 81 1 5 -1 -85 -1
|
||||
1 1 1 5 -1 -85 6
|
||||
81 1 1 1 1 85 99
|
||||
81 1 5 5 1 85 99
|
||||
69 5 89
|
||||
blk-2-split-1
|
||||
7
|
||||
1 69 1 5 1 1 2
|
||||
-1 -35 1 5 89 89 -1
|
||||
-1 -35 1 5 1 1 6
|
||||
-35 -69 1 5 89 89 -1
|
||||
-1 -35 1 5 1 1 7
|
||||
1 1 1 5 -89 -1 -1
|
||||
81 81 1 5 -89 -1 2
|
||||
69 69 -1 -5 1 89 -1
|
||||
1 1 -1 -5 1 89 5
|
||||
1 69 1 1 89 1 99
|
||||
1 69 5 5 89 1 99
|
||||
69 5 89
|
||||
blk-2-split-2
|
||||
7
|
||||
1 69 1 5 1 1 2
|
||||
-1 -35 1 5 89 89 -1
|
||||
-1 -35 1 5 1 1 8
|
||||
-35 -69 1 5 89 89 -1
|
||||
-1 -35 1 5 1 1 9
|
||||
1 1 -1 -5 1 89 -1
|
||||
69 69 -1 -5 1 89 4
|
||||
69 69 1 5 -89 -1 -1
|
||||
1 1 1 5 -89 -1 2
|
||||
1 69 1 1 89 1 99
|
||||
1 69 5 5 89 1 99
|
||||
35 5 177
|
||||
blk-1-split-1
|
||||
7
|
||||
-1 -35 1 5 1 1 -1
|
||||
-1 -35 1 5 89 89 4
|
||||
1 35 1 5 177 177 4
|
||||
1 1 1 5 -1 -85 -1
|
||||
81 81 1 5 -1 -85 3
|
||||
1 1 1 5 -85 -177 -1
|
||||
81 81 1 5 -1 -93 1
|
||||
35 35 -1 -5 1 177 -1
|
||||
1 1 -1 -5 1 177 7
|
||||
1 35 1 1 1 177 99
|
||||
1 35 5 5 1 177 99
|
||||
35 5 177
|
||||
blk-1-split-2
|
||||
6
|
||||
-1 -35 1 5 1 1 -1
|
||||
-35 -69 1 5 89 89 4
|
||||
1 35 1 5 177 177 4
|
||||
1 1 -1 -5 1 177 -1
|
||||
35 35 -1 -5 1 177 6
|
||||
35 35 -1 -5 1 177 -1
|
||||
1 1 -1 -5 1 177 8
|
||||
1 35 1 1 1 177 99
|
||||
1 35 5 5 1 177 99
|
||||
35 5 177
|
||||
blk-1-split-3
|
||||
6
|
||||
-1 -35 1 5 1 1 -1
|
||||
-1 -35 1 5 89 89 5
|
||||
1 35 1 5 177 177 4
|
||||
1 1 -1 -5 1 177 -1
|
||||
35 35 -1 -5 1 177 7
|
||||
35 35 -1 -5 1 177 -1
|
||||
1 1 -1 -5 1 177 9
|
||||
1 35 1 1 1 177 99
|
||||
1 35 5 5 1 177 99
|
||||
35 5 177
|
||||
blk-1-split-4
|
||||
7
|
||||
-1 -35 1 5 1 1 -1
|
||||
-35 -69 1 5 89 89 5
|
||||
1 35 1 5 177 177 4
|
||||
1 1 -1 -5 1 177 -1
|
||||
35 35 -1 -5 1 177 8
|
||||
35 35 1 5 -1 -85 -1
|
||||
1 1 1 5 -1 -85 3
|
||||
35 35 1 5 -85 -177 -1
|
||||
1 1 1 5 -1 -93 1
|
||||
1 35 1 1 1 177 99
|
||||
1 35 5 5 1 177 99
|
||||
Binary file not shown.
File diff suppressed because it is too large
Load Diff
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,267 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 50000;
|
||||
|
||||
int intervalStepFlow = 500;
|
||||
int intervalStepPlot = 500;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 8.15;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 288.0;
|
||||
int dump_Q = 1;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.67e7;
|
||||
double refDimensionalTemperature = 56.0;
|
||||
double freestream_vibration_temperature = 10000.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 0.01;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "steger";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 2.0;
|
||||
int CFLVaryStep = 100;
|
||||
|
||||
int nLUSGSSweeps = 4;
|
||||
double LUSGSTolerance = 1.0e-20;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/dbl_yzg__48.fts";
|
||||
int isPlotVolumeField = 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 1;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-4;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int nchem = 0;
|
||||
int ntmodel = 1;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
double catalyticCoef = 1.0;
|
||||
string gasfile = "DK5";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.07955, 0.134, 0.0509, 1.0e-9, 0.73555";
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# 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/dbl_yzg.cgns";
|
||||
string out_gfile = "./grid/dbl_yzg.fts";
|
||||
|
|
@ -0,0 +1,51 @@
|
|||
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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,21 @@
|
|||
// 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).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 48;
|
||||
|
||||
string original_grid_file = "./grid/dbl_yzg.fts";
|
||||
string partition_grid_file = "./grid/dbl_yzg__48.fts";
|
||||
|
||||
// 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 @@
|
|||
本套网格由燕振国提供。
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,240 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 30000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 100;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 12.935;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 343.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.628325e5;
|
||||
double refDimensionalTemperature = 265.0;
|
||||
double freestream_vibration_temperature = 265.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw","ausmdv".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "ausmdv";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLStart = 0.1;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 1000;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/3D_Electre_Half_Model_dy1D-5__6.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// 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 #
|
||||
#########################################################################
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int nchem = 1;
|
||||
int ntmodel = 1;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/3D_Electre_Half_Model_dy1D-5.grd";
|
||||
string out_gfile = "./grid/3D_Electre_Half_Model_dy1D-5.fts";
|
||||
|
|
@ -0,0 +1,51 @@
|
|||
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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,21 @@
|
|||
// 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).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 6;
|
||||
|
||||
string original_grid_file = "./grid/3D_Electre_Half_Model_dy1D-5.fts";
|
||||
string partition_grid_file = "./grid/3D_Electre_Half_Model_dy1D-5__6.fts";
|
||||
|
||||
// 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 +1,76 @@
|
|||
1
|
||||
6
|
||||
25 97 71
|
||||
A
|
||||
7
|
||||
1 25 1 31 1 1 2
|
||||
1 25 31 97 1 1 2
|
||||
1 25 1 97 71 71 4
|
||||
1 1 1 97 1 71 3
|
||||
25 25 -1 -97 1 71 -1
|
||||
1 1 -1 -97 1 71 2
|
||||
1 25 1 1 -1 -71 -1
|
||||
1 25 25 25 -1 -71 6
|
||||
1 25 97 97 1 71 6
|
||||
25 97 71
|
||||
B
|
||||
7
|
||||
1 25 1 31 1 1 2
|
||||
1 25 31 97 1 1 2
|
||||
1 25 1 97 71 71 4
|
||||
1 1 -1 -97 1 71 -1
|
||||
25 25 -1 -97 1 71 1
|
||||
25 25 -1 -97 1 71 -1
|
||||
1 1 -1 -97 1 71 3
|
||||
1 25 1 1 -1 -71 -1
|
||||
25 25 25 1 -1 -71 6
|
||||
1 25 97 97 1 71 6
|
||||
25 97 71
|
||||
C
|
||||
7
|
||||
1 25 1 31 1 1 2
|
||||
1 25 31 97 1 1 2
|
||||
1 25 1 97 71 71 4
|
||||
1 1 -1 -97 1 71 -1
|
||||
25 25 -1 -97 1 71 2
|
||||
25 25 -1 -97 1 71 -1
|
||||
1 1 -1 -97 1 71 4
|
||||
1 25 1 1 -1 -71 -1
|
||||
25 25 25 1 -1 -71 5
|
||||
1 25 97 97 1 71 6
|
||||
25 97 71
|
||||
D
|
||||
7
|
||||
1 25 1 31 1 1 2
|
||||
1 25 31 97 1 1 2
|
||||
1 25 1 97 71 71 4
|
||||
1 1 -1 -97 1 71 -1
|
||||
25 25 -1 -97 1 71 3
|
||||
25 25 1 97 1 71 3
|
||||
1 25 1 1 -1 -71 -1
|
||||
25 1 1 1 -1 -71 5
|
||||
1 25 97 97 1 71 6
|
||||
25 25 71
|
||||
S
|
||||
6
|
||||
1 25 1 25 1 1 2
|
||||
1 25 1 25 71 71 4
|
||||
1 1 1 25 1 71 3
|
||||
25 25 25 1 -1 -71 -1
|
||||
1 25 1 1 -1 -71 3
|
||||
25 1 1 1 -1 -71 -1
|
||||
1 25 1 1 -1 -71 4
|
||||
1 25 25 25 -1 -71 -1
|
||||
1 25 1 1 -1 -71 6
|
||||
25 25 71
|
||||
T
|
||||
6
|
||||
1 25 1 25 1 1 2
|
||||
1 25 1 25 71 71 4
|
||||
1 1 1 25 1 71 3
|
||||
25 25 25 1 -1 -71 -1
|
||||
1 25 1 1 -1 -71 2
|
||||
1 25 1 1 -1 -71 -1
|
||||
1 25 25 25 -1 -71 5
|
||||
1 25 25 25 -1 -71 -1
|
||||
1 25 1 1 -1 -71 1
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,205 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 10000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 0.8395;
|
||||
double attackd = 3.06;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.171e7;
|
||||
double refDimensionalTemperature = 288;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
int viscousType = 4;
|
||||
string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "roe", "vanleer", "ausm+up", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "3rdsmooth", "smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "smooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 5.0;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 0 -- is recommended for structured solver.
|
||||
// 1-3 -- is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 10.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level.
|
||||
// = 1 -- single-level.
|
||||
// > 1 -- multi-level.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 2;
|
||||
int flowInitStep = 100;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/m6_str__4.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
||||
double MUSCLCoefXk = 0.333333;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 2;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# 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/m6_str.cgns";
|
||||
string out_gfile = "./grid/m6_str.fts";
|
||||
|
|
@ -0,0 +1,45 @@
|
|||
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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_transonic.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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,21 @@
|
|||
// 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).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/m6_str.fts";
|
||||
string partition_grid_file = "./grid/m6_str__4.fts";
|
||||
|
||||
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
|
||||
// 1 -- single level.
|
||||
// 2 -- 2 level.
|
||||
// N -- N level,..., et al.
|
||||
int numberOfMultigrid = 2;
|
||||
Binary file not shown.
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,197 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 50000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// 2 - the experiment conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 0.799;
|
||||
double attackd = 2.26;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 9.0e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int iviscous = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int iviscous = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// - "roe", "vanleer", "ausm+up", "ausmpw"
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "3rdsmooth", "smooth"
|
||||
// - "nolim" - no limiter
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "smooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// - "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle"
|
||||
// - "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus"
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat", "barth"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 5.0;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 : is recommended for structured solver.
|
||||
// 1-3: is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 30.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level
|
||||
// = 1 : Single level.
|
||||
// > 1 : multi-level.
|
||||
// flowInitStep: Flow initialization step, 0~500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/NACA0012__4.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/NACA0012.grd";
|
||||
string out_gfile = "./grid/NACA0012.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,51 @@
|
|||
string title = "PHengLEI Main Parameter Control File";
|
||||
|
||||
// IMPORTANT NOTICE£ºDON NOT MODIFY THE FOWLLOWING LINE
|
||||
string defaultParaFile = "./bin/cfd_para.hypara";
|
||||
|
||||
// ndim: Dimensional of the grid: 2 or 3.
|
||||
// nparafile: the number of the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_transonic.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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/NACA0012.fts";
|
||||
string partition_grid_file = "./grid/NACA0012__4.fts";
|
||||
|
||||
|
||||
// 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 +1,15 @@
|
|||
1
|
||||
1
|
||||
353 166 3
|
||||
A
|
||||
8
|
||||
1 353 1 166 1 1 3
|
||||
1 353 1 166 3 3 3
|
||||
1 1 1 166 1 3 6
|
||||
353 353 1 166 1 3 6
|
||||
81 1 1 1 -1 -3 -1
|
||||
273 353 1 1 -1 -3 1
|
||||
81 273 1 1 1 3 2
|
||||
273 353 1 1 -1 -3 -1
|
||||
81 1 1 1 -1 -3 1
|
||||
1 353 166 166 1 3 5
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,191 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 25000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// 2 - the experiment conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 - no dump out.
|
||||
// 1 - dump out wall Q only.
|
||||
// 2 - dump out wall Q & the typical position Q of ball.
|
||||
// 3 - dump out wall Q & the typical position Q of cone.
|
||||
// 4 - dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 10.00;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 294.0 ;
|
||||
int dump_Q = 2;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.0e5;
|
||||
double refDimensionalTemperature = 79.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int iviscous = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 0.0001;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// - "vanleer", "steger", "ausmpw"
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "minmod", "3rd_minmod_smooth"
|
||||
|
||||
string inviscidSchemeName = "steger";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// - "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle"
|
||||
// - "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus"
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat", "barth"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 100;
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/3dball.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/3dball.grd";
|
||||
string out_gfile = "./grid/3dball.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,42 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 3;
|
||||
int nparafile = 1;
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_hypersonic.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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = ""
|
||||
string parafilename2 = "";
|
||||
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 1;
|
||||
|
||||
string original_grid_file = "./grid/3dball.fts";
|
||||
string partition_grid_file = "./grid/3dball.fts";
|
||||
|
||||
|
||||
// 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 +1,11 @@
|
|||
1
|
||||
1
|
||||
61 81 19
|
||||
A
|
||||
6
|
||||
1 61 1 81 1 1 3
|
||||
1 61 1 81 19 19 3
|
||||
1 1 1 81 19 1 73
|
||||
61 61 1 81 19 1 6
|
||||
1 61 1 1 19 1 2
|
||||
1 61 81 81 19 1 5
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,189 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 50000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
|
||||
// ifLowSpeedPrecon: precondition to accelerate convergence for low speed flow.
|
||||
// ONLY available for unstructured solver!
|
||||
// 0 -- no precondition process (default, mach > 0.2).
|
||||
// 1 -- carry out precondition process ( mach number < 0.2 ).
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 0.2;
|
||||
double attackd = 19.0;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 9.0e6;
|
||||
double refDimensionalTemperature = 288.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int iviscous = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
int viscousType = 4;
|
||||
string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "3rdsmooth", "smooth"
|
||||
// - "nolim" - no limiter
|
||||
|
||||
string str_limiter_name = "smooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 50.0;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 : is recommended for structured solver.
|
||||
// 1-3: is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 10.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level
|
||||
// = 1 : Single level.
|
||||
// > 1 : multi-level.
|
||||
// flowInitStep: Flow initialization step, 0~500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/30p30n_str__4.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/30p30n_str.grd";
|
||||
string out_gfile = "./grid/30p30n_str.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,41 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = "./bin/cfd_para.hypara"
|
||||
string parafilename2 = "./bin/cfd_para.hypara";
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/30p30n_str.fts";
|
||||
string partition_grid_file = "./grid/30p30n_str__4.fts";
|
||||
|
||||
|
||||
// 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 +1,161 @@
|
|||
1
|
||||
8
|
||||
81 617
|
||||
A
|
||||
21
|
||||
1 41 1 1 4
|
||||
1 1 65 1 -1
|
||||
353 353 -65 -1 7
|
||||
1 1 65 129 -1
|
||||
281 281 -1 -65 6
|
||||
1 1 189 129 -1
|
||||
121 121 -61 -1 8
|
||||
1 1 221 189 -1
|
||||
121 121 -93 -61 8
|
||||
1 1 221 245 -1
|
||||
121 121 -93 -117 8
|
||||
1 1 309 245 -1
|
||||
41 41 65 1 2
|
||||
1 1 309 341 -1
|
||||
41 41 -65 -97 2
|
||||
1 1 -481 -553 -1
|
||||
41 41 -65 -137 5
|
||||
1 1 -481 -449 -1
|
||||
41 41 -65 -33 5
|
||||
1 1 -373 -449 -1
|
||||
121 121 -33 -109 4
|
||||
1 1 -341 -373 -1
|
||||
121 121 -1 -33 4
|
||||
41 1 617 617 4
|
||||
1 1 -553 -617 -1
|
||||
1 1 -65 -1 7
|
||||
81 81 553 617 4
|
||||
81 41 617 617 4
|
||||
81 81 341 553 4
|
||||
81 81 245 341 4
|
||||
81 81 65 245 4
|
||||
81 81 65 1 4
|
||||
41 81 1 1 4
|
||||
41 97
|
||||
B
|
||||
6
|
||||
41 41 65 1 -1
|
||||
1 1 309 245 1
|
||||
-1 -41 1 1 -1
|
||||
81 121 117 117 8
|
||||
1 1 65 1 2
|
||||
41 41 -65 -97 -1
|
||||
1 1 309 341 1
|
||||
1 1 97 65 2
|
||||
1 41 97 97 -1
|
||||
81 121 1 1 4
|
||||
81 49
|
||||
C
|
||||
6
|
||||
81 49 49 49 -1
|
||||
81 49 1 1 4
|
||||
81 81 1 49 2
|
||||
81 49 1 1 -1
|
||||
81 49 117 117 8
|
||||
-1 -49 49 49 -1
|
||||
1 49 1 1 4
|
||||
1 1 49 1 2
|
||||
-49 -1 1 1 -1
|
||||
49 1 117 117 8
|
||||
121 141
|
||||
D
|
||||
14
|
||||
121 121 -1 -33 -1
|
||||
1 1 -341 -373 1
|
||||
81 121 1 1 -1
|
||||
1 41 97 97 2
|
||||
81 49 1 1 -1
|
||||
81 49 49 49 3
|
||||
1 1 33 1 2
|
||||
1 49 1 1 -1
|
||||
-1 -49 49 49 3
|
||||
121 121 -33 -109 -1
|
||||
1 1 -373 -449 1
|
||||
1 1 77 33 2
|
||||
1 1 93 77 2
|
||||
1 1 109 93 2
|
||||
1 1 125 109 2
|
||||
1 1 -125 -141 -1
|
||||
1 1 -17 -1 8
|
||||
49 1 141 141 -1
|
||||
113 161 65 65 6
|
||||
-121 -49 141 141 -1
|
||||
41 113 65 65 6
|
||||
121 121 141 109 -1
|
||||
41 41 -1 -33 5
|
||||
41 137
|
||||
E
|
||||
8
|
||||
41 41 -1 -33 -1
|
||||
121 121 141 109 4
|
||||
1 1 33 1 2
|
||||
1 41 1 1 -1
|
||||
1 41 65 65 6
|
||||
41 41 -65 -33 -1
|
||||
1 1 -481 -449 1
|
||||
1 1 65 33 2
|
||||
41 41 -65 -137 -1
|
||||
1 1 -481 -553 1
|
||||
1 1 137 65 2
|
||||
41 1 137 137 -1
|
||||
1 41 65 65 7
|
||||
281 65
|
||||
F
|
||||
8
|
||||
1 1 65 1 2
|
||||
1 161 1 1 -1
|
||||
73 233 65 65 7
|
||||
113 161 65 65 -1
|
||||
49 1 141 141 4
|
||||
41 113 65 65 -1
|
||||
-121 -49 141 141 4
|
||||
1 41 65 65 -1
|
||||
1 41 1 1 5
|
||||
161 281 65 65 -1
|
||||
1 121 1 1 8
|
||||
281 281 -1 -65 -1
|
||||
1 1 65 129 1
|
||||
161 281 1 1 -1
|
||||
233 353 65 65 7
|
||||
353 65
|
||||
G
|
||||
7
|
||||
1 1 -65 -1 -1
|
||||
1 1 -553 -617 1
|
||||
1 41 65 65 -1
|
||||
41 1 137 137 5
|
||||
73 41 65 65 2
|
||||
73 233 65 65 -1
|
||||
1 161 1 1 6
|
||||
233 353 65 65 -1
|
||||
161 281 1 1 6
|
||||
353 353 -65 -1 -1
|
||||
1 1 65 1 1
|
||||
1 353 1 1 4
|
||||
121 117
|
||||
H
|
||||
11
|
||||
1 1 61 17 2
|
||||
1 1 -17 -1 -1
|
||||
1 1 -125 -141 4
|
||||
1 121 1 1 -1
|
||||
161 281 65 65 6
|
||||
121 121 -61 -1 -1
|
||||
1 1 189 129 1
|
||||
1 1 93 61 2
|
||||
121 121 -93 -61 -1
|
||||
1 1 221 189 1
|
||||
1 1 117 93 2
|
||||
81 49 117 117 -1
|
||||
81 49 1 1 3
|
||||
49 1 117 117 -1
|
||||
-49 -1 1 1 3
|
||||
81 121 117 117 -1
|
||||
-1 -41 1 1 2
|
||||
121 121 -93 -117 -1
|
||||
1 1 221 245 1
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,267 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 500;
|
||||
int intervalStepPlot = 200;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 8.03;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 294.44;
|
||||
int dump_Q = 1;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.835e5;
|
||||
double refDimensionalTemperature = 124.94;
|
||||
double freestream_vibration_temperature = 10000.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "steger";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 100;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int nLUSGSSweeps = 4;
|
||||
double LUSGSTolerance = 1.0e-20;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/cylinder_str.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 1;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-4;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
#########################################################################
|
||||
# Non-equilibrium gas #
|
||||
#########################################################################
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int nchem = 0;
|
||||
int ntmodel = 1;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
double catalyticCoef = 1.0;
|
||||
string gasfile = "DK5";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.07955, 0.134, 0.0509, 1.0e-9, 0.73555";
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 2;
|
||||
|
||||
#########################################################################
|
||||
# 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/cylinder_str.cgns";
|
||||
string out_gfile = "./grid/cylinder_str.fts";
|
||||
|
|
@ -0,0 +1,51 @@
|
|||
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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,21 @@
|
|||
// 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).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/cylinder_str.fts";
|
||||
string partition_grid_file = "./grid/cylinder_str__4.fts";
|
||||
|
||||
// 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 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,193 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 30000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumbe: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// 2 - the experiment conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 - no dump out.
|
||||
// 1 - dump out wall Q only.
|
||||
// 2 - dump out wall Q & the typical position Q of ball.
|
||||
// 3 - dump out wall Q & the typical position Q of cone.
|
||||
// 4 - dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 8.03;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 294.0 ;
|
||||
int dump_Q = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 3.67e5;
|
||||
double refDimensionalTemperature = 125.0;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int iviscous = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 0.0001;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// - "vanleer", "steger", "ausmpw"
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "minmod", "3rd_minmod_smooth"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanleer";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// - "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle"
|
||||
// - "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus"
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat", "barth"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 3.0;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/input.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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;
|
||||
|
||||
double MUSCLCoefXk = 0.333333;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/input.grd";
|
||||
string out_gfile = "./grid/input.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,42 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_hypersonic.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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = ""
|
||||
string parafilename2 = "";
|
||||
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 1;
|
||||
|
||||
string original_grid_file = "./grid/input.fts";
|
||||
string partition_grid_file = "./grid/input.fts";
|
||||
|
||||
|
||||
// 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 +1,9 @@
|
|||
1
|
||||
1
|
||||
101 81
|
||||
A
|
||||
4
|
||||
1 1 1 81 6
|
||||
1 101 81 81 5
|
||||
101 101 1 81 6
|
||||
1 101 1 1 2
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,238 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 10000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 100;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
|
||||
double refMachNumber = 8.7569;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 300.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 4.7001e5;
|
||||
double refDimensionalTemperature = 694.00;
|
||||
double freestream_vibration_temperature = 694.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#########################################################################
|
||||
# Physical models #
|
||||
#########################################################################
|
||||
// viscousType : Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "1eq-sa", when viscousType = 3.
|
||||
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS.(default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int viscousType = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "minmod", "3rd_minmod_smooth".
|
||||
|
||||
string inviscidSchemeName = "ausmdv";
|
||||
string str_limiter_name = "minmod";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "vencat", "barth".
|
||||
// -- "1st", meaning accuracy of first-order.
|
||||
// -- "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// CFLEnd: The CFL number, [0.1, 100].
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 1000;
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "./grid/2D_HEG_CYLINDER_65X88_DY2D-7__4.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// ----------------- 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).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// 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 #
|
||||
#########################################################################
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int nchem = 1;
|
||||
int ntmodel = 1;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
double catalyticCoef = 1.0;
|
||||
string gasfile = "DK11";
|
||||
string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
string initMassFraction = "0.07955,0.134,0.0509,1.0e-9,0.0,0.0,0.0,0.0,0.0,0.73555,0.0";
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
|
@ -0,0 +1,30 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/2D_HEG_CYLINDER_65X88_DY2D-7.grd";
|
||||
string out_gfile = "./grid/2D_HEG_CYLINDER_65X88_DY2D-7.fts";
|
||||
|
|
@ -0,0 +1,51 @@
|
|||
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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
|
||||
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
//@string parafilename1 = ""
|
||||
//@string parafilename2 = "";
|
||||
|
|
@ -0,0 +1,21 @@
|
|||
// 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).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 4;
|
||||
|
||||
string original_grid_file = "./grid/2D_HEG_CYLINDER_65X88_DY2D-7.fts";
|
||||
string partition_grid_file = "./grid/2D_HEG_CYLINDER_65X88_DY2D-7__4.fts";
|
||||
|
||||
// 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 +1,9 @@
|
|||
1
|
||||
1
|
||||
65 88
|
||||
A
|
||||
4
|
||||
65 1 1 1 2
|
||||
65 65 1 88 6
|
||||
1 65 88 88 4
|
||||
1 1 1 88 3
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,191 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 100000;
|
||||
|
||||
int intervalStepFlow = 5000;
|
||||
int intervalStepPlot = 5000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 100;
|
||||
|
||||
|
||||
// ifLowSpeedPrecon: precondition to accelerate convergence for low speed flow.
|
||||
// ONLY available for unstructured solver!
|
||||
// 0 -- no precondition process (default, mach > 0.2).
|
||||
// 1 -- carry out precondition process ( mach number < 0.2 ).
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 0.2;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 5.0e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
double gridScaleFactor = 0.001;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 2.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int iviscous = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
int viscousType = 4;
|
||||
string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "3rdsmooth", "smooth"
|
||||
// - "nolim" - no limiter
|
||||
|
||||
string str_limiter_name = "nolim";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 50.0;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 : is recommended for structured solver.
|
||||
// 1-3: is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 500.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level
|
||||
// = 1 : Single level.
|
||||
// > 1 : multi-level.
|
||||
// flowInitStep: Flow initialization step, 0~500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/Mesh4_137_97.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
||||
double MUSCLCoefXk =0.333333;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/Mesh4_137_97.grd";
|
||||
string out_gfile = "./grid/Mesh4_137_97.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,42 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = ""
|
||||
string parafilename2 = "";
|
||||
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 1;
|
||||
|
||||
string original_grid_file = "./grid/Mesh4_137_97.fts";
|
||||
string partition_grid_file = "./grid/Mesh4_137_97.fts";
|
||||
|
||||
|
||||
// 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 +1,10 @@
|
|||
1
|
||||
1
|
||||
137 97
|
||||
A
|
||||
5
|
||||
1 25 1 1 3
|
||||
25 137 1 1 2
|
||||
137 137 1 97 6
|
||||
1 137 97 97 4
|
||||
1 1 1 97 4
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,193 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 50000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// 2 - the experiment conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 - no dump out.
|
||||
// 1 - dump out wall Q only.
|
||||
// 2 - dump out wall Q & the typical position Q of ball.
|
||||
// 3 - dump out wall Q & the typical position Q of cone.
|
||||
// 4 - dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 5.00;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
double wallTemperature = 327.36;
|
||||
int dump_Q = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 1.5e7;
|
||||
double refDimensionalTemperature = 300.33;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
|
||||
|
||||
double gridScaleFactor = 0.001;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 2.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int iviscous = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 0.0002;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// - "vanleer", "steger", "ausmpw"
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "minmod", "3rd_minmod_smooth"
|
||||
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "smooth";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// - "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle"
|
||||
// - "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus"
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat", "barth"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_scheme_name = "vanleer";
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 0.5;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 100;
|
||||
int CFLVaryStep = 500;
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/plate_137_97.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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;
|
||||
|
||||
double MUSCLCoefXk = 0.333333;
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/plate_137_97.grd";
|
||||
string out_gfile = "./grid/plate_137_97.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,42 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
int nparafile = 1;
|
||||
int nsimutask = 0;
|
||||
string parafilename = "./bin/cfd_para_hypersonic.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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = ""
|
||||
string parafilename2 = "";
|
||||
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 1;
|
||||
|
||||
string original_grid_file = "./grid/plate_137_97.fts";
|
||||
string partition_grid_file = "./grid/plate_137_97.fts";
|
||||
|
||||
|
||||
// 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 +1,10 @@
|
|||
1
|
||||
1
|
||||
137 97
|
||||
A
|
||||
5
|
||||
1 25 1 1 3
|
||||
25 137 1 1 2
|
||||
137 137 1 97 6
|
||||
1 137 97 97 4
|
||||
1 1 1 97 4
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
|
|
@ -0,0 +1,193 @@
|
|||
#########################################################################
|
||||
# General Control Parameter #
|
||||
#########################################################################
|
||||
// maxsimustep: the max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: the step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: the step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: the step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: the step intervals for residual 'res.dat' saved.
|
||||
|
||||
int maxSimuStep = 150000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
|
||||
|
||||
// ifLowSpeedPrecon: precondition to accelerate convergence for low speed flow.
|
||||
// ONLY available for unstructured solver!
|
||||
// 0 -- no precondition process (default, mach > 0.2).
|
||||
// 1 -- carry out precondition process ( mach number < 0.2 ).
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
#########################################################################
|
||||
# Inflow Parameter #
|
||||
#########################################################################
|
||||
// refMachNumber: Mach number per meter.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
||||
// inflowParaType: the type of inflow parameters.
|
||||
// 0 - the nondimensional conditions.
|
||||
// 1 - the flight conditions.
|
||||
// height: Fly height, unit of km.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
||||
|
||||
double refMachNumber = 0.1;
|
||||
double attackd = 0.00;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 2.0e5;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
#*******************************************************************
|
||||
# Physical models *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model
|
||||
// 0 - Euler
|
||||
// 1 - Lamilar
|
||||
// 3 - 1eq turbulent
|
||||
// 4 - 2eq turbulent
|
||||
// viscousName : Laminar or tubulent model
|
||||
// - "1eq-sa", when iviscous = 3
|
||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
||||
// DESType : Type of DES
|
||||
// 0 - RANS (default);
|
||||
// 1 - DES;
|
||||
// 2 - DDES;
|
||||
// 3 - IDDES;
|
||||
|
||||
//int iviscous = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
int viscousType = 1;
|
||||
string viscousName = "laminar";
|
||||
|
||||
//int iviscous = 3;
|
||||
//string viscousName = "1eq-sa";
|
||||
|
||||
//int iviscous = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
int roeEntropyFixMethod = 2;
|
||||
double roeEntropyScale = 1.0;
|
||||
#########################################################################
|
||||
# Spatial Discretisation #
|
||||
#########################################################################
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// str_limiter_name: Limiter of struct grid
|
||||
// - "3rdsmooth", "smooth"
|
||||
// - "nolim" - no limiter
|
||||
|
||||
string str_limiter_name = "nolim";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver *
|
||||
#*******************************************************************
|
||||
// uns_limiter_name: Limiter of Unstruct grid
|
||||
// - "vencat"
|
||||
// - "1st", meaning accuracy of first-order.
|
||||
// - "nolim", no limiter.
|
||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
||||
// The smaller the value, the more robust it is.
|
||||
|
||||
string uns_limiter_name = "vencat";
|
||||
double venkatCoeff = 50.0;
|
||||
|
||||
#########################################################################
|
||||
# Temporal Discretisation #
|
||||
#########################################################################
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 - steady
|
||||
// 1 - unsteay
|
||||
// CFLEnd: The CFL number, [0.1, 100]
|
||||
// The bigger the value, the convergence faster but lower robustness.
|
||||
// nLUSGSSweeps: Number of Sub-iteration of LU-SGS.
|
||||
// 1 : is recommended for structured solver.
|
||||
// 1-3: is recommended for unstructured solver.
|
||||
|
||||
int iunsteady = 0;
|
||||
|
||||
double CFLEnd = 100.0;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
|
||||
#########################################################################
|
||||
# Multi-Grid parameters #
|
||||
#########################################################################
|
||||
// nMGLevel: The number of Multi-Grid level
|
||||
// = 1 : Single level.
|
||||
// > 1 : multi-level.
|
||||
// flowInitStep: Flow initialization step, 0~500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int flowInitStep = 100;
|
||||
|
||||
|
||||
#########################################################################
|
||||
# File In or Out #
|
||||
#########################################################################
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// IMPORTANT WARNNING: 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!
|
||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
||||
|
||||
string gridfile = "./grid/flat_laminar_73_81.fts";
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
|
||||
// ---------------- 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)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
||||
// Arriables order must from small to larger.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// limitVariables: limit model.
|
||||
// 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 = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
|
||||
double MUSCLCoefXk = 0.333333;
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,34 @@
|
|||
#########################################################################
|
||||
# Grid data type #
|
||||
#########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
// from_gtype: Type of grid data type in grid conversion process.
|
||||
// -1 -- MULTI_TYPE
|
||||
// 1 -- HyperFLOW( 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.
|
||||
int gridtype = 1;
|
||||
int axisup = 1;
|
||||
int from_gtype = 3;
|
||||
|
||||
#########################################################################
|
||||
# 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/flat_laminar_73_81.grd";
|
||||
string out_gfile = "./grid/flat_laminar_73_81.fts";
|
||||
|
||||
|
||||
|
||||
|
||||
|
|
@ -0,0 +1,41 @@
|
|||
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 the parameter file.
|
||||
// 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 HyperFLOW 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.
|
||||
// 4 -- Knowledge repository / examples of PHengLEI-API.
|
||||
int ndim = 2;
|
||||
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/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 = 4;
|
||||
//string parafilename = "./bin/repository.hypara";
|
||||
//int nsimutask = 5;
|
||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
||||
//int nsimutask = 99;
|
||||
//string parafilename = "./bin/post_processing.hypara";
|
||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
||||
int iovrlap = 0;
|
||||
int numberOfGridProcessor = 0;
|
||||
// ATP read
|
||||
string parafilename1 = "./bin/cfd_para.hypara"
|
||||
string parafilename2 = "./bin/cfd_para.hypara";
|
||||
|
|
@ -0,0 +1,23 @@
|
|||
// 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(HyperFLOW/PHengLEI type, *.fts).
|
||||
// partition_grid_file : target partition grid file(HyperFLOW/PHengLEI type, *.fts).
|
||||
|
||||
int pgridtype = 1;
|
||||
int maxproc = 1;
|
||||
|
||||
string original_grid_file = "./grid/flat_laminar_73_81.fts";
|
||||
string partition_grid_file = "./grid/flat_laminar_73_81.fts";
|
||||
|
||||
|
||||
// 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 +1,11 @@
|
|||
1
|
||||
1
|
||||
73 81
|
||||
A
|
||||
6
|
||||
1 33 1 1 3
|
||||
33 73 1 1 2
|
||||
73 73 1 81 6
|
||||
33 73 81 81 4
|
||||
1 33 81 81 4
|
||||
1 1 81 1 5
|
||||
|
|
@ -0,0 +1,809 @@
|
|||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
|
||||
// P P H H E NN N G L E I +
|
||||
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
|
||||
// P H H E N N N G G L E I +
|
||||
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
|
||||
//------------------------------------------------------------------------+
|
||||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
###########################################################################
|
||||
// gridtype: Grid type for generation, conversion, reconstruction, merging.
|
||||
// 0 -- Unstructured grid.
|
||||
// 1 -- Structured grid.
|
||||
// 2 -- Hybrid grid, include both of unstructured and structured grid.
|
||||
// gridobj: Task type of grid treatment.
|
||||
// 0 -- Grid generation of typical case, such as cylinder, flat plate, etc.
|
||||
// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
|
||||
// 2 -- Grid refinement.
|
||||
// 3 -- Grid merging, merge two blocks into one block.
|
||||
// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
|
||||
// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
|
||||
// multiblock: Multi-block grid or not, only for structured grid conversion.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// grid_database_index: Case of typical case, only for gridobj=0.
|
||||
// 1 -- Laminar flat plate of subsonic flow.
|
||||
// 2 -- Laminar flat plate of supersonic flow.
|
||||
// 3 -- Turbulent flat plate of subsonic flow.
|
||||
// 4 -- Turbulent flat plate of supersonic flow.
|
||||
// iadapt: Adaptation number for unstructure grid.
|
||||
// iovrlap: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// SymmetryFaceVector: The vector of symmetry face.
|
||||
// 0 -- X axis.
|
||||
// 1 -- Y axis.
|
||||
// 2 -- Z axis.
|
||||
int gridtype = 0;
|
||||
int gridobj = 1;
|
||||
int multiblock = 0;
|
||||
int grid_database_index = 3;
|
||||
int iadapt = 0;
|
||||
int iovrlap = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
//-----------------------------------------------------------------------
|
||||
// from_gtype/to_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.
|
||||
// dumpOldGrid: If dump out the old grid file.
|
||||
// 0 -- Not. (default)
|
||||
// 1 -- Yes.
|
||||
int from_gtype = 2;
|
||||
int to_gtype = 1;
|
||||
int dumpOldGrid = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# 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/rae2822_hybrid2d.cas";
|
||||
string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
|
||||
|
||||
// ----------------- some advanced choices ------------------------------
|
||||
// iunsteady: The Grid is for unsteady simulation or not.
|
||||
int iunsteady = 0;
|
||||
int iale = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
// 0 -- BINARY.
|
||||
// 1 -- ASCII.
|
||||
int fileformat = 0;
|
||||
|
||||
// .skl meaning skeleton.
|
||||
string original_grid_info_file = "./grid/FLUENT_test.skl";
|
||||
|
||||
// Parameters for hybrid solver.
|
||||
// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
|
||||
// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
|
||||
string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
|
||||
string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
|
||||
string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
|
||||
|
||||
// Some parameters for structured overlapping grid.
|
||||
int codeOfDigHoles = 1;
|
||||
string holeBasicFileName = "./oversetGridView/holeBasicFile.inp";
|
||||
string holeFullFileName = "./oversetGridView/holeFullFile.dat";
|
||||
string linkFileName = "./oversetGridView/topology.dat";
|
||||
string zoneInverseFileName = "./oversetGridView/zoneInverseMapping.inp";
|
||||
|
||||
// ----------------- Adaptive Mesh Refine -------------------------------
|
||||
// In this file, the original_grid_file is used of the partition part.
|
||||
// If use it dependently, abstract it here.
|
||||
string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts";
|
||||
string geometryFileName = "./grid/jsm.igs";
|
||||
|
||||
// geometryUnit: Geometry unit.
|
||||
// 1 -- meter.
|
||||
// 2 -- millimeter.
|
||||
// 3 -- inch.
|
||||
// exclusiveCase: Parallel projection exclusive case.
|
||||
// 0 -- NON case.
|
||||
// 1 -- JSM-C2-NPOFF case.
|
||||
// 2 -- CHNT.
|
||||
// projectOrgPoint: If the original wall points need to be projected or not.
|
||||
int geometryUnit = 1;
|
||||
int anisoRefine = 0;
|
||||
int isProject = 0;
|
||||
int readDist = 0;
|
||||
int isDeform = 0;
|
||||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
// ----------------- RBF Parameters -------------------------------------
|
||||
// symmetryPlane: Which symmetry plane is used in the mesh.
|
||||
// 0 -- without symmetry.
|
||||
// 1 -- plane of x=0.
|
||||
// 2 -- plane of y=0.
|
||||
// 3 -- plane of z=0.
|
||||
int numberOfReferenceCP = 10;
|
||||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
// pgridtype: The grid type.
|
||||
// 0 -- unstruct grid.
|
||||
// 1 -- struct grid.
|
||||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
|
||||
// traceMark: Trace mark or not, only for structured grid partition.
|
||||
// 0 -- Not.
|
||||
// 1 -- Yes.
|
||||
// blockIndexOfMark: the block index of mark, only for structured grid partition.
|
||||
// cellIndexOfMark: the cell index of mark, only for structured grid partition.
|
||||
int traceMark = 0;
|
||||
int blockIndexOfMark = 0;
|
||||
int cellIndexOfMark[] = [185,30,1];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File path #
|
||||
//-----------------------------------------------------------------------
|
||||
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||
string original_grid_file = "./grid/sphere_mixed.fts";
|
||||
string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
||||
|
||||
// ------------------ Sompe advanced parameters -------------------------
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
// npartmethod: Method of interface reconstruction, default is 1.
|
||||
// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
|
||||
// 1 -- Using ParMetis for homogeneous MPI.
|
||||
// 2 -- Using Metis for homogeneous MPI.
|
||||
// 3 -- using METIS partition for homogeneous OpenMP.
|
||||
// parmetisBalance: Used to specify the imbalance tolerance.
|
||||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
double parmetisBalance = 1.05;
|
||||
|
||||
// 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;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for CFD simulation #
|
||||
#########################################################################
|
||||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// refMachNumber: Mach number.
|
||||
// attackd: Angle of attack.
|
||||
// angleSlide: Angle of sideslip.
|
||||
// inflowParaType: The type of inflow parameters.
|
||||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||
// height: Fly height, unit of km.
|
||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
||||
// 0 -- no dump out.
|
||||
// 1 -- dump out wall Q only.
|
||||
// 2 -- dump out wall Q & the typical position Q of ball.
|
||||
// 3 -- dump out wall Q & the typical position Q of cone.
|
||||
// 4 -- dump out wall Q & the typical position Q of double sphere.
|
||||
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||
// 1 dm = 0.1 m.
|
||||
// 1 cm = 0.01 m.
|
||||
// 1 mm = 0.001m.
|
||||
// 1 inch = 0.0254m.
|
||||
// 1 foot = 12 inches = 0.3048m.
|
||||
// 1 yard = 3 feet = 0.9144m.
|
||||
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||
// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
|
||||
// condition is radiation equilibrium temperature, and 0.8 is the default value.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
||||
//int inflowParaType = 2;
|
||||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
int dump_Q = 0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double TorqueRefX = 0.0; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
string inviscidSchemeName = "roe";
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
// 3 -- 1eq turbulent.
|
||||
// 4 -- 2eq turbulent.
|
||||
// viscousName: Laminar or tubulent model.
|
||||
// -- "0eq-bl".
|
||||
// -- "1eq-sa".
|
||||
// -- "2eq-kw-menter-sst".
|
||||
// -- "2eq-kw-menter-bsl".
|
||||
// -- "2eq-kw-wilcox-1988".
|
||||
// -- "2eq-kw-wilcox-1998".
|
||||
// -- "2eq-kw-kok-tnt".
|
||||
// -- "2eq-kw-wilcox-2006".
|
||||
// -- "easm-kw-2003".
|
||||
// -- "easm-kw-2005".
|
||||
// DESType: Type of DES.
|
||||
// 0 -- RANS. (default)
|
||||
// 1 -- DES.
|
||||
// 2 -- DDES.
|
||||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "nolim", no limiter.
|
||||
// uns_vis_name: Discretisation method of viscous term.
|
||||
// -- "std", "test", "aver", "new1", "new2".
|
||||
// uns_gradient: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
// 1 -- new method, it is dependent of grid scale.
|
||||
// 4 -- Ustar limiter model, without grid size unitary.
|
||||
// 7 -- default used.
|
||||
// venkatCoeff: Cofficient of vencat, when using vencat limter.
|
||||
// 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.
|
||||
// skewnessAngle: The skewness angle of grid cells.
|
||||
// roeEntropyFixMethod: Entropy fix (correction) method.
|
||||
// 1 -- direct fix, which limits the minimum eigenvalue directly.
|
||||
// 2 -- multi-dimensional fix, which is derived from structured solver and now is only valid for struct solver.
|
||||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
||||
//int viscousType = 1;
|
||||
//string viscousName = "laminar";
|
||||
|
||||
int viscousType = 3;
|
||||
string viscousName = "1eq-sa";
|
||||
|
||||
//int viscousType = 4;
|
||||
//string viscousName = "2eq-kw-menter-sst";
|
||||
|
||||
int DESType = 0;
|
||||
|
||||
string uns_scheme_name = "roe";
|
||||
string uns_limiter_name = "vencat";
|
||||
string uns_vis_name = "test";
|
||||
string gradientName = "ggnode";
|
||||
|
||||
int ivencat = 7;
|
||||
double venkatCoeff = 5.0;
|
||||
int reconmeth = 1;
|
||||
int limitVariables = 0;
|
||||
int limitVector = 0;
|
||||
double limit_angle = 0;
|
||||
double skewnessAngle = 60.0;
|
||||
|
||||
int roeEntropyFixMethod = 3;
|
||||
double roeEntropyScale = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
// physicalTimeStep: The nondimensional physical time step.
|
||||
// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
|
||||
// ifStaticsFlowField: Statistical variables for DES simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// min_sub_iter: The min sub iteration of unsteady simulation.
|
||||
// max_sub_iter: The max sub iteration of unsteady simulation.
|
||||
// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
|
||||
// tscheme: Temporal Discretisation method.
|
||||
// 1 -- Runge-Kutta Multi-State.
|
||||
// 2 -- Point implicit.
|
||||
// 3 -- Full implicit.
|
||||
// 4 -- LU-SGS.
|
||||
// 5 -- Block LU-SGS.
|
||||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Lower G-S iteration.
|
||||
// 8 -- Upper G-S iteration.
|
||||
// 9 -- Lower/Upper G-S iteration.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
// LUSGSTolerance: Sub iter tolerance of LU-SGS or Block LU-SGS.
|
||||
// ifLocalTimeStep: Time step method.
|
||||
// 0 --Local.
|
||||
// 1 --Global.
|
||||
// visl_min: Minimum value of laminar viscosity coefficient.
|
||||
// turbCFLScale: Turbulence model cfl number factor.
|
||||
// iale: Arbitrary Lagrangian-Eulerian method.
|
||||
// 0 -- no ALE method.
|
||||
// 1 -- ALE method for non-moving grids.
|
||||
// 2 -- ALE method for moving grids.
|
||||
// 3 -- ALE method for deforming grids.
|
||||
// wallFunctionType: The type of wall function to implement.
|
||||
// 0 -- no wall function. (default)
|
||||
// 1 -- standard wall function.
|
||||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int startStatisticStep = 800000;
|
||||
|
||||
int min_sub_iter = 50;
|
||||
int max_sub_iter = 50;
|
||||
double tol_sub_iter = 0.01;
|
||||
|
||||
int tscheme = 4;
|
||||
int iSimplifyViscousTerm = 1;
|
||||
int ifLocalTimeStep = 0;
|
||||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double ktmax = 1.0e10;
|
||||
|
||||
int swapDq = 1;
|
||||
|
||||
int nLUSGSSweeps = 1;
|
||||
double LUSGSTolerance = 0.01;
|
||||
int order = 2;
|
||||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int iale = 0;
|
||||
int ialetype = 2;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
double dtau_max = 1E-01;
|
||||
|
||||
int wallFunctionType = 0;
|
||||
|
||||
int RKStage = 2;
|
||||
double lamda[] = 0.5, 1.0;
|
||||
|
||||
//int RKStage = 1;
|
||||
//double lamda[] = 1.0;
|
||||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
// 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!
|
||||
// isPlotVolumeField: If dump out the field results to visulization.
|
||||
// walldistMethod: The method to compute wall distance.
|
||||
// 0 -- accurate but not fast enough.
|
||||
// 1 -- fast but not accurate enough.
|
||||
// 2 -- super fast but more non-accurate!
|
||||
// resSaveFile: The file path to save the residual convergence process, write data for every default (intervalStepRes) steps.
|
||||
// turbresfile: The file path to save the residual convergence process of turbulence, write data for every default (intervalStepRes) steps.
|
||||
// aircoeffile: The file path to save the aerodynamic force coefficients convergence process, write data for every default (intervalStepForce) steps.
|
||||
// restartNSFile: The file path to write restart flowfield variables, write data for every default (intervalStepFlow) steps.
|
||||
// turbfile: The file path to write restart flowfield variables of turbulence , write data for every default(intervalStepFlow) steps.
|
||||
// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
|
||||
// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
||||
string componentDefineFile = "bin/component.hypara";
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string componentforcefile = "results/component_aircoef.dat";
|
||||
|
||||
string overset_gridfile = "iblank.ovs";
|
||||
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
int visualfileType = 1;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
// sliceAxis: Normal vector of slice.
|
||||
// 1 -- X_DIR.
|
||||
// 2 -- Y_DIR.
|
||||
// 3 -- Z_DIR.
|
||||
// slicePostion: Coordinate of slice.
|
||||
|
||||
int visualSlice = 0;
|
||||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
// 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(33), electron temperature(34),
|
||||
// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
// 1 -- Edwards.
|
||||
// 2 -- new.
|
||||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turb_vis_kind = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double turb_min_coef = 1.0e-1;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 1.0e-1;
|
||||
double kwoo = 1.0;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
double sdilim = 1.0e20;
|
||||
double coef_kvist = 1.0;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
// iapplication:
|
||||
// 0 -- NS.
|
||||
// 1 -- MHD.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
// 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.
|
||||
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int nm = 5;
|
||||
|
||||
// MHD
|
||||
double bxoo = 0.0;
|
||||
double byoo = 0.0;
|
||||
double bzoo = 0.0;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
double prt = 0.90;
|
||||
double sc_l = 0.5;
|
||||
double sc_t = 0.5;
|
||||
|
||||
int nchem = 0;
|
||||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
double catalyticCoef = 0.0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, NO+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
//string speciesName = "O, O2, NO, N, O+, O2+, NO+, N+, N2+, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.77, 0.0";
|
||||
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
// nMGLevel: The number of level of Multi-Grid.
|
||||
// <= 1 -- Single-level.
|
||||
// > 1 -- multi-level.
|
||||
// MGPreIteration: For each grid, the number of pre-smoothing steps.
|
||||
// n_post: For each grid, the number of post-smoothing steps.
|
||||
// MGCoarsestIteration: For the coarest grid the number of smoothing steps.
|
||||
// MGFasType: V-multi cycle or W-multi cycle.
|
||||
// 1 -- V-multi cycle.
|
||||
// 2 -- W-multi cycle.
|
||||
// flowInitStep: Flow initialization step, 0 - 500 is suggested.
|
||||
// Multi-Grid : Number of steps computing on coarse grid, during flow initialization.
|
||||
// Single-Grid: Number of steps computing using first-order with vanleer, during flow initialization.
|
||||
// mgCFLScale: CFL number enlarge times for coarse grid.
|
||||
// mprol: Multi-grid interpolation method, interpolation from coarse cell to fine grid.
|
||||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
int MGFasType = 1;
|
||||
int n_post = 0;
|
||||
int flowInitStep = 100;
|
||||
int mprol = 2;
|
||||
double mgCFLScale = 1.0;
|
||||
double mgCorrectionLimit = 0.01;
|
||||
|
||||
//--------------- Some parameter for turbulent model --------------------
|
||||
// neasm: The variation of kw turbulent model.
|
||||
// ismooth_turb: Residual smooth for turb or not.
|
||||
// SSTProductType: The type of product term based on vorticity for SST.
|
||||
// SAProductType: The type of product term based on vorticity for SA.
|
||||
int neasm = -3;
|
||||
int SSTProductType = 0;
|
||||
int ismooth_turb = 0;
|
||||
int SAProductType = 2;
|
||||
|
||||
// ----------------- Overset Grid parameter -----------------------------
|
||||
int codeOfDigHoles = 1;
|
||||
int codeOfTurbulentModel = 0;
|
||||
string masterFileName = "./grid/searchFile.inp";
|
||||
string holeBasicFileName = "./grid/holeBasicFile.inp";
|
||||
string holeFullFileName = "./grid/holeFullFile.dat";
|
||||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
// <= 2 -- finite volume method.
|
||||
// >= 3 -- finite difference order. (to be completed)
|
||||
// 0 -- default.
|
||||
// str_highorder_interpolation_epsilon: Epsilon in weighted interpolation, bigger epsilon, better convergence,
|
||||
// smaller epsilon, robuster for shock-detecting.
|
||||
// str_highorder_interpolation_type:
|
||||
// -- "classical", "test".
|
||||
// str_highorder_flux_name:
|
||||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
// MUSCLCoefXk: The parameter of MUSCL interpolations, belongs to [-1, 1].
|
||||
// -1 -- seconde-order fully-upwind differencing.
|
||||
// 0 -- seconde-order upwind-biased differencing.
|
||||
// 0.333333 -- third-order upwind-biased differencing.
|
||||
// 1 -- seconde-order central differencing.
|
||||
// MUSCLCoefXb: The limiter parameter.
|
||||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
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Reference in New Issue