diff --git a/ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara b/ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara +++ b/ThreeD_CHNT_SST_Struct_16CPU/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/bin/key.hypara b/ThreeD_Cylinder_LES_Re3900_Struct/bin/key.hypara deleted file mode 100644 index 7e91c8f..0000000 --- a/ThreeD_Cylinder_LES_Re3900_Struct/bin/key.hypara +++ /dev/null @@ -1,41 +0,0 @@ -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"; diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/bin/partition.hypara b/ThreeD_Cylinder_LES_Re3900_Struct/bin/partition.hypara deleted file mode 100644 index f194d47..0000000 --- a/ThreeD_Cylinder_LES_Re3900_Struct/bin/partition.hypara +++ /dev/null @@ -1,20 +0,0 @@ -// 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; \ No newline at end of file diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_23w_split9.grd b/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_23w_split9.grd deleted file mode 100644 index 7fed4cc..0000000 Binary files a/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_23w_split9.grd and /dev/null differ diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_23w_split9.inp b/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_23w_split9.inp deleted file mode 100644 index 3c7169f..0000000 --- a/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_23w_split9.inp +++ /dev/null @@ -1,119 +0,0 @@ - 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 - 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- 25 25 -1 -49 1 25 -1 - 1 1 -1 -49 1 25 80 - 1 25 1 1 1 25 99 - 1 25 49 49 1 25 99 diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/bin/cfd_para.hypara b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara similarity index 67% rename from ThreeD_Cylinder_LES_Re3900_Struct/bin/cfd_para.hypara rename to ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara index 5fb2cf9..b1551cc 100644 --- a/ThreeD_Cylinder_LES_Re3900_Struct/bin/cfd_para.hypara +++ b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/cfd_para.hypara @@ -10,22 +10,22 @@ // (C) Copyright, Since 2010 + //+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ########################################################################### -# Default parameters for Grid conversion # +# 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. +// 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. +// 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. +// 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. @@ -33,28 +33,28 @@ // 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. +// 0 -- NON-overlapping grid. +// 1 -- Overlapping grid. // SymmetryFaceVector: The vector of symmetry face. -// 0 -- X axis. -// 1 -- Y axis. -// 2 -- Z axis. +// 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; +int SymmetryFaceVector = 1; // axisup: Type of Cartisien coordinates system, used in grid conversion. -// 1 -- Y upward. (default) -// 2 -- Z upward. -int axisup = 1; +// 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. +// 0 -- Interface. (default) +// 1 -- Physical boundary condition, used in Hybrid solver. int omit_no_bound_bc = 0; //----------------------------------------------------------------------- @@ -63,19 +63,19 @@ int omit_no_bound_bc = 0; // 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. +// 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. +// 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; +// 0 -- Not. (default) +// 1 -- Yes. +int from_gtype = 2; +int to_gtype = 1; +int dumpOldGrid = 0; //----------------------------------------------------------------------- # File path # @@ -87,13 +87,13 @@ 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; +int iunsteady = 0; +int iale = 0; // fileformat: Ustar Grid file format. // 0 -- BINARY. // 1 -- ASCII. -int fileformat = 0; +int fileformat = 0; // .skl meaning skeleton. string original_grid_info_file = "./grid/FLUENT_test.skl"; @@ -102,22 +102,22 @@ string original_grid_info_file = "./grid/FLUENT_test.skl"; // 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"; +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"; +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"; +string adapt_grid_file = "./grid/sphere_mixed_adapt1.fts"; +string geometryFileName = "./grid/jsm.igs"; // geometryUnit: Geometry unit. // 1 -- meter. @@ -130,11 +130,11 @@ string geometryFileName = "./grid/jsm.igs"; // projectOrgPoint: If the original wall points need to be projected or not. int geometryUnit = 1; int anisoRefine = 0; -int isProject = 0; +int isProject = 0; int readDist = 0; -int isDeform = 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. +int projectOrgPoint = 0; // if project original wall points. // ----------------- RBF Parameters ------------------------------------- // symmetryPlane: Which symmetry plane is used in the mesh. @@ -147,33 +147,33 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! -// periodicType: Which periodic boundary is used. +// Notice:Periodic boundary only support translation or rotation along the X axis! +// periodicType: Which symmetry plane is used in the mesh. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. // 2 -- Rotational periodicity. -int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; -double rotationAngle = 0.0; +int periodicType = 1; +double translationLength[] = [0,3.14,0]; +double rotationAngle = 0; ######################################################################### -# Default parameters for Partition # +# 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. +// 2 -- refine structured grid. +// maxproc: The number of partition zones that want to be divided into. int pgridtype = 0; -int maxproc = 4; +int maxproc = 4; // traceMark: Trace mark or not, only for structured grid partition. -// 0 -- Not. -// 1 -- Yes. +// 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 traceMark = 0; +int blockIndexOfMark = 0; int cellIndexOfMark[] = [185,30,1]; //----------------------------------------------------------------------- @@ -181,22 +181,22 @@ int cellIndexOfMark[] = [185,30,1]; //----------------------------------------------------------------------- // 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"; +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. +// 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. +// 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. +// 1.05 -- recommended. int omit_no_bound_bc = 0; int npartmethod = 1; @@ -207,7 +207,7 @@ double parmetisBalance = 1.05; // 1 -- single level. // 2 -- 2 level. // N -- N level, ..., et al. -int numberOfMultigrid = 1; +int numberOfMultigrid = 1; ######################################################################### # Default parameters for CFD simulation # @@ -215,88 +215,80 @@ int numberOfMultigrid = 1; // 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. -// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved. // intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved. -// intervalStepRes: The step intervals for residual file 'res.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 = 20000; - -int intervalStepFlow = 1000; -int intervalStepPlot = 1000; +int maxSimuStep = 3000; +int intervalStepFlow = 1000; +int intervalStepPlot = 1000; int intervalStepSample = 1000; -int intervalStepForce = 100; -int intervalStepRes = 10; -int ifLowSpeedPrecon = 0; +int intervalStepForce = 100; +int intervalStepRes = 10; +int ifLowSpeedPrecon = 0; // compressible: // 0 -- incompressible flow. // 1 -- compressible flow. (default) -int compressible = 1; +int compressible = 1; //----------------------------------------------------------------------- -# CFD Control Parameter # +# CFD Control Parameter # //----------------------------------------------------------------------- // refMachNumber: Mach number. -// attackd: Angle of attack. +// 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. +// 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. +// 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. +// 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 +// 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; +double refMachNumber = 0.20; +double attackd = 0.00; +double angleSlide = 0.00; -int inflowParaType = 0; -double refReNumber = 6.5e6; -double refDimensionalTemperature = 288.15; -double freestream_vibration_temperature = 10000.00; +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 = 1; +//double height = 0.001; -//int inflowParaType = 2; +//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; +//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; +int dump_Q = 0; double radiationCoef = 0.8; double gridScaleFactor = 1.0; @@ -308,11 +300,12 @@ double TorqueRefX = 0.0; // unit of meter. double TorqueRefY = 0.0; // unit of meter. double TorqueRefZ = 0.0; // unit of meter. + //----------------------------------------------------------------------- -# Spatial Discretisation # +# Spatial Discretisation # //----------------------------------------------------------------------- #******************************************************************* -# Struct Solver * +# Struct Solver * #******************************************************************* // inviscidSchemeName: Spatial discretisation scheme of struct grid. // Using this when solve structered grid or hybrid. @@ -323,13 +316,13 @@ double TorqueRefZ = 0.0; // unit of meter. // -- "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"; +string inviscidSchemeName = "roe"; +string str_limiter_name = "vanalbada"; #******************************************************************* -# UnStruct Solver or Common * +# UnStruct Solver or Common * #******************************************************************* -// viscousType: Viscous model. +// iviscous: Viscous model. // 0 -- Euler. // 1 -- Lamilar. // 2 -- Algebraic. @@ -352,14 +345,14 @@ string str_limiter_name = "vanalbada"; // 2 -- DDES. // 3 -- IDDES. // uns_scheme_name: Spatial discretisation scheme of Unstruct grid. -// Using this when solve Unstructered grid or hybrid. +// 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. +// uns_vis_name: Discretisation method of viscous term. // -- "std", "test", "aver", "new1", "new2". // uns_gradient: Gradient reconstruction method. // -- "default", "ggcell", "ggnode", "lsq". @@ -369,7 +362,7 @@ string str_limiter_name = "vanalbada"; // 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). +// 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: @@ -389,43 +382,43 @@ string str_limiter_name = "vanalbada"; //int viscousType = 0; //string viscousName = "Euler"; -//int viscousType = 1; -//string viscousName = "laminar"; +int viscousType = 1; +string viscousName = "laminar"; -int viscousType = 3; -string viscousName = "1eq-sa"; +//int viscousType = 3; +//string viscousName = "1eq-sa"; //int viscousType = 4; //string viscousName = "2eq-kw-menter-sst"; -int DESType = 0; +int DESType = 0; -string uns_scheme_name = "roe"; -string uns_limiter_name = "vencat"; -string uns_vis_name = "test"; -string gradientName = "ggnode"; +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 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; +int roeEntropyFixMethod = 3; +double roeEntropyScale = 1.0; //----------------------------------------------------------------------- # Temporal Discretisation # //----------------------------------------------------------------------- -// iunsteady: Steady or unsteady. +// 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. +// 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. @@ -441,14 +434,14 @@ double roeEntropyScale = 1.0; // 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. +// 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. +// 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. @@ -466,64 +459,64 @@ double roeEntropyScale = 1.0; // 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 iunsteady = 1; +double physicalTimeStep = 0.005; +int ifStartFromSteadyResults = 0; +int ifStaticsFlowField = 0; +int startStatisticStep = 0; -int min_sub_iter = 50; -int max_sub_iter = 50; +int min_sub_iter = 20; +int max_sub_iter = 20; double tol_sub_iter = 0.01; -int tscheme = 4; -int iSimplifyViscousTerm = 1; +int tscheme = 4; +int iSimplifyViscousTerm = 1; int ifLocalTimeStep = 0; double CFLStart = 0.01; double CFLEnd = 10.0; -int CFLVaryStep = 500; +int CFLVaryStep = 500; -double ktmax = 1.0e10; +double ktmax = 1.0e10; -int swapDq = 1; +int swapDq = 1; -int nLUSGSSweeps = 1; -double LUSGSTolerance = 0.01; -int order = 2; +int nLUSGSSweeps = 1; +double LUSGSTolerance = 0.01; +int order = 2; -double visl_min = 0.01; +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; +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 wallFunctionType = 0; -int RKStage = 2; +int RKStage = 2; double lamda[] = 0.5, 1.0; -//int RKStage = 1; -//double lamda[] = 1.0; +//int RKStage = 1; +//double lamda[] = 1.0; -//int RKStage = 4; +//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. +// 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, +// 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. +// 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! @@ -535,15 +528,15 @@ double lamda[] = 0.5, 1.0; // 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"; +string gridfile = "./grid/cylinder_270w_split120.fts"; int walldistMethod = 1; -string resSaveFile = "results/res.dat"; +string resSaveFile = "results/res.dat"; string turbresfile = "results/turbres.dat"; string aircoeffile = "results/aircoef.dat"; -string restartNSFile = "results/flow.dat"; +string restartNSFile = "results/flow.dat"; string turbfile = "results/turb.dat"; string visualfile = "results/tecflow.plt"; @@ -554,14 +547,14 @@ string surfacefile = ""; string wall_varfile = ""; -string componentDefineFile = "bin/component.hypara"; -string jetDefineFile = "bin/jet.hypara"; +string componentDefineFile = "bin/component.hypara"; +string jetDefineFile = "bin/jet.hypara"; string componentforcefile = "results/component_aircoef.dat"; -string overset_gridfile = "iblank.ovs"; +string overset_gridfile = "iblank.ovs"; -int isPlotVolumeField = 0; +int isPlotVolumeField = 1; // visualfileType: The file type of visualfile. // 0 -- Tecplot binary. @@ -578,27 +571,26 @@ int visualfileType = 1; // 3 -- Z_DIR. // slicePostion: Coordinate of slice. -int visualSlice = 0; -int sliceAxis = 1; -double slicePostion = -0.5; -string sliceFile = "results/Slice.plt"; +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]; +// 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];; // dumpStandardModel: Dump many standard model data. // 1 -- Turbulent flat plate. @@ -617,6 +609,7 @@ int ifSetProbesToMonitor = 0; string probesDefineFile = "bin/probes_location.hypara"; int nProbeVariables = 6; int probeVariables[] = [0, 1, 2, 3, 4, 5]; + //----------------------------------------------------------------------- # Turbulence Parameter # //----------------------------------------------------------------------- @@ -633,16 +626,57 @@ 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; +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 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; +int monitorNegativeConstant = 0; + //----------------------------------------------------------------------- # Other Parameter # //----------------------------------------------------------------------- @@ -676,41 +710,42 @@ int monitor_vistmax = 0; // "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. +// 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; +int iapplication = 0; +int iCodeBranch = 0; +int nm = 5; // MHD double bxoo = 0.0; double byoo = 0.0; double bzoo = 0.0; -double refGama = 1.4; +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 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 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 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 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; @@ -727,22 +762,22 @@ int ifStartFromPerfectGasResults = 0; // 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. +// 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; +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 -------------------- @@ -756,16 +791,16 @@ 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"; +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 # +# High Order Struct Solver # ######################################################################### // ifvfd: // 0 -- NSSolverStruct using Finite Volume Method. @@ -785,9 +820,9 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp"; int ifvfd = 0; string str_highorder_solver = "WCNS"; int SolverStructOrder = 0; -double str_highorder_interpolation_epsilon = 1.0e-6; +double str_highorder_interpolation_epsilon = 1.0e-4; string str_highorder_interpolation_type = "test"; -string str_highorder_flux_name = "steger"; +string str_highorder_flux_name = "roe"; string structhighordergradient = "conservation"; double coefofstrflux = 0.5; double limitcoefofinterface = 0.0; @@ -803,17 +838,17 @@ double limitcoefofinterface = 0.0; // 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; +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"; +//@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"; diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/bin/grid_para.hypara b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/grid_para.hypara similarity index 90% rename from ThreeD_Cylinder_LES_Re3900_Struct/bin/grid_para.hypara rename to ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/grid_para.hypara index 65429d4..1cd1b92 100644 --- a/ThreeD_Cylinder_LES_Re3900_Struct/bin/grid_para.hypara +++ b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/grid_para.hypara @@ -19,12 +19,12 @@ // 8 -- GMSH, *.msh. int gridtype = 1; int axisup = 2; -int from_gtype = 3; +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_Re3900_270w_split120.grd"; -string out_gfile = "./grid/cylinder_Re3900_270w_split120.fts"; +string from_gfile = "./grid/cylinder_270w_split120.cgns"; +string out_gfile = "./grid/cylinder_270w_split120.fts"; diff --git a/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/key.hypara b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/key.hypara new file mode 100644 index 0000000..97f35f2 --- /dev/null +++ b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/bin/key.hypara @@ -0,0 +1,54 @@ +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 = 21; +//string parafilename = "./bin/integrative_solver.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 = ""; diff --git a/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_270w_split120.grd b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/grid/cylinder_270w_split120.cgns similarity index 81% rename from ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_270w_split120.grd rename to ThreeD_Cylinder_LES_Re3900_Struct_120CPU/grid/cylinder_270w_split120.cgns index c91aa6f..241f880 100644 Binary files a/ThreeD_Cylinder_LES_Re3900_Struct/grid/cylinder_Re3900_270w_split120.grd and b/ThreeD_Cylinder_LES_Re3900_Struct_120CPU/grid/cylinder_270w_split120.cgns differ diff --git a/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/bin/cfd_para.hypara b/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/bin/cfd_para.hypara +++ b/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/ThreeD_DoubleEllipse_Laminar_HighOrder_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara b/ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara +++ b/ThreeD_Electre_Laminar_OneTemperMode_NCW_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara b/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara +++ b/ThreeD_M6_SST_Struct_MG2_4CPU/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/ThreeD_NACA0012_SA_Struct/bin/cfd_para.hypara b/ThreeD_NACA0012_SA_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/ThreeD_NACA0012_SA_Struct/bin/cfd_para.hypara +++ b/ThreeD_NACA0012_SA_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara b/ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara index 9fdb623..92a8e59 100644 --- a/ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara +++ b/ThreeD_ShockWave_PeriodicBoundary_SA_Struct_4CPU/bin/cfd_para.hypara @@ -4,8 +4,7 @@ // 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 + @@ -147,15 +146,15 @@ int numberOfReferenceCP = 10; double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; -// ----------------- Periodic Parameters ------------------------------------- -//Notice:Periodic boundary only support translation or rotation along the X axis! -// periodicType: Which symmetry plane is used in the mesh. -// 0 -- without Periodic Boundary. -// 1 -- Translational periodicity. -// 2 -- Rotational periodicity. -int periodicType = 2; -double translationLength = 0; -double rotationAngle = 1; +// ----------------- Periodic Parameters -------------------------------- +// Notice: Rotational periodicity only support rotation along the X axis! +// periodicType: Which periodic boundary is used. +// 0 -- without Periodic Boundary. +// 1 -- Translational periodicity. +// 2 -- Rotational periodicity. +int periodicType = 2; +double translationLength[] = [0.0,0.0,0.0]; +double rotationAngle = 1.0; ######################################################################### # Default parameters for Partition # @@ -330,7 +329,7 @@ string str_limiter_name = "vanalbada"; #******************************************************************* # UnStruct Solver or Common * #******************************************************************* -// iviscous: Viscous model. +// viscousType: Viscous model. // 0 -- Euler. // 1 -- Lamilar. // 2 -- Algebraic. @@ -535,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -553,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -594,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -645,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -677,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -684,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -697,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -714,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### @@ -790,8 +860,8 @@ double str_highorder_interpolation_epsilon = 1.0e-6; string str_highorder_interpolation_type = "test"; string str_highorder_flux_name = "steger"; string structhighordergradient = "conservation"; -double coefofstrflux = 0.5; -double limitcoefofinterface= 0.0; +double coefofstrflux = 0.5; +double limitcoefofinterface = 0.0; // ----------------- Advanced choices ----------------------------------- // outtimesc: Time stepping scheme for the outer loop. diff --git a/ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara b/ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara +++ b/ThreeD_Sphere_Laminar_Ma10_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_30p30n_SST_Struct/bin/cfd_para.hypara b/TwoD_30p30n_SST_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_30p30n_SST_Struct/bin/cfd_para.hypara +++ b/TwoD_30p30n_SST_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/cfd_para.hypara b/TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/cfd_para.hypara index 61698c0..f52cf86 100644 --- a/TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/cfd_para.hypara +++ b/TwoD_BackwardStep_PressureOutlet_SA_Struct_4CPU/bin/cfd_para.hypara @@ -146,15 +146,15 @@ int numberOfReferenceCP = 10; double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; -// ----------------- Periodic Parameters ------------------------------------- -//Notice:Periodic boundary only support translation or rotation along the X axis! -// periodicType: Which symmetry plane is used in the mesh. -// 0 -- without Periodic Boundary. -// 1 -- Translational periodicity. -// 2 -- Rotational periodicity. -int periodicType = 0; -double translationLength = 0; -double rotationAngle = 0; +// ----------------- Periodic Parameters -------------------------------- +// Notice: Rotational periodicity only support rotation along the X axis! +// periodicType: Which periodic boundary is used. +// 0 -- without Periodic Boundary. +// 1 -- Translational periodicity. +// 2 -- Rotational periodicity. +int periodicType = 0; +double translationLength[] = [0.0,0.0,0.0]; +double rotationAngle = 0.0; ######################################################################### # Default parameters for Partition # @@ -329,7 +329,7 @@ string str_limiter_name = "vanalbada"; #******************************************************************* # UnStruct Solver or Common * #******************************************************************* -// iviscous: Viscous model. +// viscousType: Viscous model. // 0 -- Euler. // 1 -- Lamilar. // 2 -- Algebraic. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### @@ -789,8 +860,8 @@ double str_highorder_interpolation_epsilon = 1.0e-6; string str_highorder_interpolation_type = "test"; string str_highorder_flux_name = "steger"; string structhighordergradient = "conservation"; -double coefofstrflux = 0.5; -double limitcoefofinterface= 0.0; +double coefofstrflux = 0.5; +double limitcoefofinterface = 0.0; // ----------------- Advanced choices ----------------------------------- // outtimesc: Time stepping scheme for the outer loop. diff --git a/TwoD_Cylinder_Laminar_HighOrder_Struct/TwoD_Cylinder_Laminar_HighOrder_Struct/bin/cfd_para.hypara b/TwoD_Cylinder_Laminar_HighOrder_Struct/TwoD_Cylinder_Laminar_HighOrder_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Cylinder_Laminar_HighOrder_Struct/TwoD_Cylinder_Laminar_HighOrder_Struct/bin/cfd_para.hypara +++ b/TwoD_Cylinder_Laminar_HighOrder_Struct/TwoD_Cylinder_Laminar_HighOrder_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara b/TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara +++ b/TwoD_Cylinder_Laminar_Ma8d03_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara b/TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara +++ b/TwoD_Cylinder_Laminar_OneTemperMode_FCW_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_LowMach_plate_SST_Struct/bin/cfd_para.hypara b/TwoD_LowMach_plate_SST_Struct/bin/cfd_para.hypara deleted file mode 100644 index 5fb2cf9..0000000 --- a/TwoD_LowMach_plate_SST_Struct/bin/cfd_para.hypara +++ /dev/null @@ -1,819 +0,0 @@ -//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ -// 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; - -// ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! -// periodicType: Which periodic boundary is used. -// 0 -- without Periodic Boundary. -// 1 -- Translational periodicity. -// 2 -- Rotational periodicity. -int periodicType = 0; -double translationLength[] = [0.0,0.0,0.0]; -double rotationAngle = 0.0; - -######################################################################### -# 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. -// intervalStepSample: The step intervals for monitored probes variables file 'sample.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 intervalStepSample = 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. - -//----------------------------------------------------------------------- -# 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 probesflowfile = "results/sample.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; - -// ifSetProbesToMonitor: Set probes location to Monitor. -// 0 -- Do not monitor. -// 1 -- To monitor and save data to files. -// probesDefineFile: probes location information file. -// nProbeVariables: Number of variables want to be dumped for probes monitered. -// probeVariables : Variable types dumped, listed as following: -// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5). -// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!! -// probeVariables order must from small to big. -int ifSetProbesToMonitor = 0; -string probesDefineFile = "bin/probes_location.hypara"; -int nProbeVariables = 6; -int probeVariables[] = [0, 1, 2, 3, 4, 5]; -//----------------------------------------------------------------------- -# 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; -string str_highorder_solver = "WCNS"; -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"; -double coefofstrflux = 0.5; -double limitcoefofinterface = 0.0; - -// ----------------- 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"; diff --git a/TwoD_LowMach_plate_SST_Struct/bin/cfd_para_subsonic.hypara b/TwoD_LowMach_plate_SST_Struct/bin/cfd_para_subsonic.hypara deleted file mode 100644 index a541eaf..0000000 --- a/TwoD_LowMach_plate_SST_Struct/bin/cfd_para_subsonic.hypara +++ /dev/null @@ -1,191 +0,0 @@ -######################################################################### -# 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; diff --git a/TwoD_LowMach_plate_SST_Struct/bin/grid_para.hypara b/TwoD_LowMach_plate_SST_Struct/bin/grid_para.hypara deleted file mode 100644 index 2510da2..0000000 --- a/TwoD_LowMach_plate_SST_Struct/bin/grid_para.hypara +++ /dev/null @@ -1,34 +0,0 @@ -######################################################################### -# 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"; - - - - diff --git a/TwoD_LowMach_plate_SST_Struct/bin/key.hypara b/TwoD_LowMach_plate_SST_Struct/bin/key.hypara deleted file mode 100644 index 094591e..0000000 --- a/TwoD_LowMach_plate_SST_Struct/bin/key.hypara +++ /dev/null @@ -1,42 +0,0 @@ -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 = ""; - diff --git a/TwoD_LowMach_plate_SST_Struct/bin/partition.hypara b/TwoD_LowMach_plate_SST_Struct/bin/partition.hypara deleted file mode 100644 index e46087c..0000000 --- a/TwoD_LowMach_plate_SST_Struct/bin/partition.hypara +++ /dev/null @@ -1,23 +0,0 @@ -// 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; - - - diff --git a/TwoD_LowMach_plate_SST_Struct/grid/Mesh4_137_97.grd b/TwoD_LowMach_plate_SST_Struct/grid/Mesh4_137_97.grd deleted file mode 100644 index c69890c..0000000 Binary files a/TwoD_LowMach_plate_SST_Struct/grid/Mesh4_137_97.grd and /dev/null differ diff --git a/TwoD_LowMach_plate_SST_Struct/grid/Mesh4_137_97.inp b/TwoD_LowMach_plate_SST_Struct/grid/Mesh4_137_97.inp deleted file mode 100644 index a4eee46..0000000 --- a/TwoD_LowMach_plate_SST_Struct/grid/Mesh4_137_97.inp +++ /dev/null @@ -1,10 +0,0 @@ - 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 diff --git a/TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara b/TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara +++ b/TwoD_Plate_Laminar_Ma5_Struct_1CPU/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara b/TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara +++ b/TwoD_Plate_Laminar_Struct_1CPU/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara b/TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara +++ b/TwoD_Plate_SST_Ma5_Struct_1CPU/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### diff --git a/TwoD_Plate_Subsonic_TotalPressTempBC_Structure_SA_4CPU/bin/cfd_para.hypara b/TwoD_Plate_Subsonic_TotalPressTempBC_Structure_SA_4CPU/bin/cfd_para.hypara index 61698c0..f52cf86 100644 --- a/TwoD_Plate_Subsonic_TotalPressTempBC_Structure_SA_4CPU/bin/cfd_para.hypara +++ b/TwoD_Plate_Subsonic_TotalPressTempBC_Structure_SA_4CPU/bin/cfd_para.hypara @@ -146,15 +146,15 @@ int numberOfReferenceCP = 10; double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; -// ----------------- Periodic Parameters ------------------------------------- -//Notice:Periodic boundary only support translation or rotation along the X axis! -// periodicType: Which symmetry plane is used in the mesh. -// 0 -- without Periodic Boundary. -// 1 -- Translational periodicity. -// 2 -- Rotational periodicity. -int periodicType = 0; -double translationLength = 0; -double rotationAngle = 0; +// ----------------- Periodic Parameters -------------------------------- +// Notice: Rotational periodicity only support rotation along the X axis! +// periodicType: Which periodic boundary is used. +// 0 -- without Periodic Boundary. +// 1 -- Translational periodicity. +// 2 -- Rotational periodicity. +int periodicType = 0; +double translationLength[] = [0.0,0.0,0.0]; +double rotationAngle = 0.0; ######################################################################### # Default parameters for Partition # @@ -329,7 +329,7 @@ string str_limiter_name = "vanalbada"; #******************************************************************* # UnStruct Solver or Common * #******************************************************************* -// iviscous: Viscous model. +// viscousType: Viscous model. // 0 -- Euler. // 1 -- Lamilar. // 2 -- Algebraic. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; ######################################################################### @@ -789,8 +860,8 @@ double str_highorder_interpolation_epsilon = 1.0e-6; string str_highorder_interpolation_type = "test"; string str_highorder_flux_name = "steger"; string structhighordergradient = "conservation"; -double coefofstrflux = 0.5; -double limitcoefofinterface= 0.0; +double coefofstrflux = 0.5; +double limitcoefofinterface = 0.0; // ----------------- Advanced choices ----------------------------------- // outtimesc: Time stepping scheme for the outer loop. diff --git a/TwoD_Rae2822_SST_Struct/bin/cfd_para.hypara b/TwoD_Rae2822_SST_Struct/bin/cfd_para.hypara index 5fb2cf9..f52cf86 100644 --- a/TwoD_Rae2822_SST_Struct/bin/cfd_para.hypara +++ b/TwoD_Rae2822_SST_Struct/bin/cfd_para.hypara @@ -147,7 +147,7 @@ double influenceRadius = 20; int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0; // ----------------- Periodic Parameters -------------------------------- -// Notice:Rotational periodicity only support rotation along the X axis! +// Notice: Rotational periodicity only support rotation along the X axis! // periodicType: Which periodic boundary is used. // 0 -- without Periodic Boundary. // 1 -- Translational periodicity. @@ -534,6 +534,9 @@ double lamda[] = 0.5, 1.0; // 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. +// nDumpSurfaceInfo = 0 the "wall_varfile" write the informations including heat flux. +// nDumpSurfaceInfo = 1 the "wall_varfile" write the informations without heat flux. + int numberOfGridGroups = 1; string gridfile = "./grid/rae2822_hybrid2d__4.fts"; @@ -552,6 +555,7 @@ string wall_aircoefile = "results/wall_aircoef.dat"; string probesflowfile = "results/sample.dat"; string surfacefile = ""; +int nDumpSurfaceInfo = 0; string wall_varfile = ""; string componentDefineFile = "bin/component.hypara"; @@ -593,7 +597,9 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0]; // -- 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), +// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), +// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36), +// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40), // -- 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. @@ -644,17 +650,75 @@ double coef_kvist = 1.0; int monitor_vistmax = 0; //----------------------------------------------------------------------- -# Other Parameter # +# LES Parameter # +//----------------------------------------------------------------------- +// iLES: Create LESSolver or not. +// >= 1 - Create LESSolver; +// < 1 - not. +// amplitudeofDisturb: Amplitude of adding disturb. +// disturbstep: Unsteady time step or steady iteration of adding random disturb. +// iterdisturb: Add random disturb in every sub-iter or only first sub-iter. +// = 0 - in only first sub-iter; +// != 0 - in every sub-iter. +// ipraddisturb: Add density and pressure disturb or not. +// ibodyforce: Add body force in source flux of NS equations or not. +// = 0 - not; +// != 0 - Add body force. +// bodyforce: Body force in source flux of NS equations or not. +// utau: friction velocity, using in DNSDisturb. +// 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 = 0; +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[] = [0, 0, 0]; +double testFilterScale = 2.0; +int averageWidth = 1; +int monitorNegativeConstant = 0; + +//----------------------------------------------------------------------- +# Other Parameters for Hypersonic Non-equilibrium Gas # //----------------------------------------------------------------------- // dg_high_order: // 0 -- generic order accuracy. // 1 -- high order accuracy. // iapplication: -// 0 -- NS. -// 1 -- MHD. +// 0 -- gas model is fixed in the codes. +// 1 -- gas model is imported from library files. +// iCodeBranch: +// 0 -- The old code version is used for Navier-Stokes. +// 1 -- A new code version is active for Navier-Stokes solver. // nm: Equation number of the physics, but is out of commision now. // 4 -- for 2D. // 5 -- for 3D. +// nGasModel: The type of gas. +// 0 -- Earth gas. +// 1 -- Mars gas. // nchem: // 0 -- without chemical reaction flow. // 1 -- the chemical reaction flow is considered. @@ -676,6 +740,7 @@ int monitor_vistmax = 0; // "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions. // "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions. // "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions. +// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas. // For self-definition model, the gasfile is used to indicate the file path of the new gas model. // speciesName: Used to list the names of each species, while each species name is separated by the symbol of comma. // initMassFraction: Used to list the initial mass fractions of species in accordance with the sequence of names in the parameter speciesName. @@ -683,6 +748,7 @@ int monitor_vistmax = 0; int dg_high_order = 0; int iapplication = 0; +int iCodeBranch = 0; int nm = 5; // MHD @@ -696,6 +762,7 @@ double prt = 0.90; double sc_l = 0.5; double sc_t = 0.5; +int nGasModel = 0; int nchem = 0; int nchemsrc = 1; int nchemrad = 1; @@ -713,6 +780,10 @@ string initMassFraction = "0.0, 0.23, 0.0, 0.0, 0.77"; //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"; +//string gasfile = "Mars-Pa8"; +//string speciesName = "O, O2, NO, N, N2, C, CO, CO2"; +//string initMassFraction = "0.0015, 0.0429, 0.0, 0.0, 0.0, 0.0, 0.0777, 0.8779"; + int ifStartFromPerfectGasResults = 0; #########################################################################