forked from PHengLEI/PHengLEI-TestCases
V2171 A11
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@ -26,15 +26,7 @@
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// multiblock: Multi-block grid or not, only for structured grid conversion.
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// multiblock: Multi-block grid or not, only for structured grid conversion.
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// 0 -- Not.
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// 0 -- Not.
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// 1 -- Yes.
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// 1 -- Yes.
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// grid_database_index: Case of typical case, only for gridobj=0.
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// 1 -- Laminar flat plate of subsonic flow.
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// 2 -- Laminar flat plate of supersonic flow.
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// 3 -- Turbulent flat plate of subsonic flow.
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// 4 -- Turbulent flat plate of supersonic flow.
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// iadapt: Adaptation number for unstructure grid.
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// iadapt: Adaptation number for unstructure grid.
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// iovrlap: Overlapping(overset) grid or not.
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// 0 -- NON-overlapping grid.
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// 1 -- Overlapping grid.
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// SymmetryFaceVector: The vector of symmetry face.
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// SymmetryFaceVector: The vector of symmetry face.
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// 0 -- X axis.
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// 0 -- X axis.
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// 1 -- Y axis.
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// 1 -- Y axis.
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@ -42,9 +34,7 @@
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int gridtype = 0;
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int gridtype = 0;
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int gridobj = 1;
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int gridobj = 1;
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int multiblock = 0;
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int multiblock = 0;
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int grid_database_index = 3;
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int iadapt = 0;
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int iadapt = 0;
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int iovrlap = 0;
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int SymmetryFaceVector = 1;
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int SymmetryFaceVector = 1;
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// axisup: Type of Cartisien coordinates system, used in grid conversion.
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// axisup: Type of Cartisien coordinates system, used in grid conversion.
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@ -89,22 +79,18 @@ string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
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// iunsteady: The Grid is for unsteady simulation or not.
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// iunsteady: The Grid is for unsteady simulation or not.
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int iunsteady = 0;
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int iunsteady = 0;
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int iale = 0;
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int iale = 0;
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int codeOfAleModel = 0;
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// fileformat: Ustar Grid file format.
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// fileformat: Ustar Grid file format.
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// 0 -- BINARY.
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// 0 -- BINARY.
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// 1 -- ASCII.
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// 1 -- ASCII.
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int fileformat = 0;
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int fileformat = 0;
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// .skl meaning skeleton.
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string original_grid_info_file = "./grid/FLUENT_test.skl";
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// Parameters for hybrid solver.
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// Parameters for hybrid solver.
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// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
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// mixgrid_uns: path of unstructure grid file for hybrid solver, *.fts type.
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// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
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// mixgrid_str: path of structure grid file for hybrid solver, *.fts type.
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// mixgrid_str_bc: path of structure grid boundary condition file for hybrid solver.
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string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
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string mixgrid_uns = "./grid/rae2822_uns2d_4.fts";
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string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
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string mixgrid_str = "./grid/flat_laminr_133_85_2d.fts";
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string mixgrid_str_bc = "./grid/flat_laminr_133_85_2d.inp";
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// Some parameters for structured overlapping grid.
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// Some parameters for structured overlapping grid.
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int codeOfDigHoles = 1;
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int codeOfDigHoles = 1;
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@ -176,6 +162,11 @@ int traceMark = 0;
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int blockIndexOfMark = 0;
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int blockIndexOfMark = 0;
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int cellIndexOfMark[] = [185,30,1];
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int cellIndexOfMark[] = [185,30,1];
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// parallel Strategy:
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//! -# 0 : each zone is assigned to the one that defined in grid partition procedure.
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//! -# 1 : random assigned for each zone or by some else ways.
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int parallelStrategy = 1;
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//-----------------------------------------------------------------------
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//-----------------------------------------------------------------------
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# File path #
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# File path #
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//-----------------------------------------------------------------------
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//-----------------------------------------------------------------------
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@ -253,12 +244,6 @@ int compressible = 1;
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// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
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// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
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// height: Fly height, unit of km.
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// height: Fly height, unit of km.
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// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
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// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
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// dump_Q: Dump out thermal flux Q of solid wall.
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// 0 -- no dump out.
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// 1 -- dump out wall Q only.
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// 2 -- dump out wall Q & the typical position Q of ball.
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// 3 -- dump out wall Q & the typical position Q of cone.
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// 4 -- dump out wall Q & the typical position Q of double sphere.
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// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
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// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
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// 1 dm = 0.1 m.
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// 1 dm = 0.1 m.
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// 1 cm = 0.01 m.
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// 1 cm = 0.01 m.
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@ -296,11 +281,11 @@ double freestream_vibration_temperature = 10000.00;
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//double refDimensionalPressure = 1.01313E05;
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//double refDimensionalPressure = 1.01313E05;
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double wallTemperature = -1.0;
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double wallTemperature = -1.0;
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int dump_Q = 0;
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double radiationCoef = 0.8;
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double radiationCoef = 0.8;
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double gridScaleFactor = 1.0;
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double gridScaleFactor = 1.0;
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int numberOfAerodynamicForceComponents = 1;
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double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
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double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceArea = 1.0; // unit of meter^2.
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double forceRefenenceArea = 1.0; // unit of meter^2.
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@ -410,7 +395,6 @@ double venkatCoeff = 5.0;
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int reconmeth = 1;
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int reconmeth = 1;
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int limitVariables = 0;
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int limitVariables = 0;
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int limitVector = 0;
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int limitVector = 0;
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double limit_angle = 0;
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double skewnessAngle = 60.0;
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double skewnessAngle = 60.0;
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int roeEntropyFixMethod = 3;
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int roeEntropyFixMethod = 3;
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@ -454,7 +438,7 @@ double roeEntropyScale = 1.0;
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// 1 --Global.
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// 1 --Global.
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// visl_min: Minimum value of laminar viscosity coefficient.
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// visl_min: Minimum value of laminar viscosity coefficient.
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// turbCFLScale: Turbulence model cfl number factor.
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// turbCFLScale: Turbulence model cfl number factor.
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// iale: Arbitrary Lagrangian-Eulerian method.
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// codeOfAleModel: Arbitrary Lagrangian-Eulerian method.
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// 0 -- no ALE method.
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// 0 -- no ALE method.
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// 1 -- ALE method for non-moving grids.
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// 1 -- ALE method for non-moving grids.
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// 2 -- ALE method for moving grids.
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// 2 -- ALE method for moving grids.
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@ -471,7 +455,9 @@ double physicalTimeStep = 0.01;
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int ifStartFromSteadyResults = 0;
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int ifStartFromSteadyResults = 0;
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int ifStaticsFlowField = 0;
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int ifStaticsFlowField = 0;
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int startStatisticStep = 800000;
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int startStatisticStep = 800000;
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int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
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int methodOfDualTime = 3;
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int min_sub_iter = 50;
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int min_sub_iter = 50;
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int max_sub_iter = 50;
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int max_sub_iter = 50;
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double tol_sub_iter = 0.01;
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double tol_sub_iter = 0.01;
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@ -493,14 +479,13 @@ int order = 2;
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double visl_min = 0.01;
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double visl_min = 0.01;
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double turbCFLScale = 1.0;
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double turbCFLScale = 1.0;
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double csrv = 2.0;
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double timemax = 1.0e10;
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double timemax = 1.0e10;
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double dtsave = -1.0;
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double dtsave = -1.0;
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int iale = 0;
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int codeOfAleModel = 0;
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int ialetype = 2;
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int aleStartStrategy = -1;
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int maxale = 10;
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int maxale = 10;
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double dtau = 0.001;
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double dtau = 0.001;
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double dtau_max = 1E-01;
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int wallFunctionType = 0;
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int wallFunctionType = 0;
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@ -522,7 +507,7 @@ double lamda[] = 0.5, 1.0;
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// IMPORTANT WARNING: The file index should be ignored,
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// IMPORTANT WARNING: The file index should be ignored,
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// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
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// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
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// please use 'rae2822_hybrid2d__4.fts' here!
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// please use 'rae2822_hybrid2d__4.fts' here!
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// isPlotVolumeField: If dump out the field results to visulization.
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// plotFieldType: If dump out the field results to visulization.
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// walldistMethod: The method to compute wall distance.
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// walldistMethod: The method to compute wall distance.
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// 0 -- accurate but not fast enough.
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// 0 -- accurate but not fast enough.
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// 1 -- fast but not accurate enough.
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// 1 -- fast but not accurate enough.
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@ -550,22 +535,18 @@ string restartNSFile = "results/flow.dat";
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string turbfile = "results/turb.dat";
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string turbfile = "results/turb.dat";
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string visualfile = "results/tecflow.plt";
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string visualfile = "results/tecflow.plt";
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string Qwall_file = "results/Qwall.dat";
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string wall_aircoefile = "results/wall_aircoef.dat";
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string wall_aircoefile = "results/wall_aircoef.dat";
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string probesflowfile = "results/sample.dat";
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string probesflowfile = "results/sample.dat";
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string surfacefile = "";
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int nDumpSurfaceInfo = 0;
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int nDumpSurfaceInfo = 0;
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string wall_varfile = "";
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string wall_varfile = "";
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string componentDefineFile = "bin/component.hypara";
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string jetDefineFile = "bin/jet.hypara";
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string jetDefineFile = "bin/jet.hypara";
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string componentforcefile = "results/component_aircoef.dat";
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string overset_gridfile = "results/iblank.ovs";
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string sixDofFileName = "results/sixDofInfo.dat";
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string overset_gridfile = "iblank.ovs";
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int plotFieldType = 0;
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int isPlotVolumeField = 0;
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// visualfileType: The file type of visualfile.
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// visualfileType: The file type of visualfile.
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// 0 -- Tecplot binary.
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// 0 -- Tecplot binary.
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@ -600,7 +581,7 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
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// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
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// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21),
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// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
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// -- vibration temperature(Tv, 33), electron temperature(Te, 34), vibrational energy(Ev, 35), electric energy(Ee, 36),
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// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
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// -- number density of electron(Ne, 37), dimensioanl density(rho, 38), dimensioanl pressure(p, 39), dimensioanl temperature(T, 40),
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
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// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
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// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
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// Variables order must from small to big.
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// Variables order must from small to big.
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int nVisualVariables = 8;
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int nVisualVariables = 8;
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@ -610,19 +591,48 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
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// 1 -- Turbulent flat plate.
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// 1 -- Turbulent flat plate.
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int dumpStandardModel = 0;
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int dumpStandardModel = 0;
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// ifSetProbesToMonitor: Set probes location to Monitor.
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// ifSetDataMonitor: Whether to set the data monitor.
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// 0 -- Do not monitor.
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// 0 -- No.
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// 1 -- To monitor and save data to files.
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// 1 -- Yes.
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// probesDefineFile: probes location information file.
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// dataMonitorType: The type of data Monitor.
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// 0 -- Probes data monitor.
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// 1 -- Lines data monitor.
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// 2 -- Surfaces data monitor.
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// probesDefineFile: Probes location information file.
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// nLines: The number of lines need to be monitored.
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// linesDefineFile: Lines location information file.
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// nSurfaces: The number of surfaces need to be monitored.
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// surfacesDefineFile: Surfaces location information file.
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// searchCellsMethod: method to search the cell of each probe.
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// 0 -- Nearest cell to the probe.
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// 1 -- Real cell where the probe is located.
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// nProbeVariables: Number of variables want to be dumped for probes monitered.
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// nProbeVariables: Number of variables want to be dumped for probes monitered.
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// probeVariables : Variable types dumped, listed as following:
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// probeVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
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// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
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// probeVariables order must from small to big.
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// probeVariables order must from small to big.
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int ifSetProbesToMonitor = 0;
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// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
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string probesDefineFile = "bin/probes_location.hypara";
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// 0 -- Take the value of probe's cell as probe real value.
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// 1 -- Interpolation from probe's and neighbouring cell to probe.
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// 2 -- Interpolation from probe's cell nodes to probe.
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int ifSetDataMonitor = 0;
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int dataMonitorType = 0;
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string probesDefineFile = "bin/probes_XYZ.dat";
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//int dataMonitorType = 1;
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//int nLines = 1;
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//string linesDefineFile = "bin/lines_XYZ.dat";
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//int dataMonitorType = 2;
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//int nSurfaces = 4;
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//string surfacesDefineFile = "bin/surfaces_XYZ.dat";
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int searchCellsMethod = 0;
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int nProbeVariables = 6;
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int nProbeVariables = 6;
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int probeVariables[] = [0, 1, 2, 3, 4, 5];
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int probeVariables[] = [0, 1, 2, 3, 4, 5];
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int probeVariablesInterpolationMethod = 0;
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//-----------------------------------------------------------------------
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//-----------------------------------------------------------------------
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# Turbulence Parameter #
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# Turbulence Parameter #
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//-----------------------------------------------------------------------
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//-----------------------------------------------------------------------
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@ -634,19 +644,17 @@ int probeVariables[] = [0, 1, 2, 3, 4, 5];
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// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
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// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
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int turbInterval = 1;
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int turbInterval = 1;
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int turb_vis_kind = 2;
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int kindOfTurbSource = 0;
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int kindOfTurbSource = 0;
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int mod_turb_res = 0;
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int mod_turb_res = 0;
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double turb_relax = 1.0;
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double turb_relax = 1.0;
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double turb_min_coef = 1.0e-1;
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double freeStreamViscosity = 1.0e-3;
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double freeStreamViscosity = 1.0e-3;
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double muoo = 1.0e-1;
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double muoo = 3.0;
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double kwoo = 1.0;
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double kwoo = 5.0;
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int transitionType = 0;
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double turbIntensity = -1.0;
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# maximum eddy viscosity (myt/my) max.
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# maximum eddy viscosity (myt/my) max.
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double eddyViscosityLimit = 1.0e10;
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double eddyViscosityLimit = 1.0e10;
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double sdilim = 1.0e20;
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double coef_kvist = 1.0;
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int monitor_vistmax = 0;
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int monitor_vistmax = 0;
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//-----------------------------------------------------------------------
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//-----------------------------------------------------------------------
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@ -751,11 +759,6 @@ int iapplication = 0;
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int iCodeBranch = 0;
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int iCodeBranch = 0;
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int nm = 5;
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int nm = 5;
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// MHD
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double bxoo = 0.0;
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double byoo = 0.0;
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double bzoo = 0.0;
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double refGama = 1.4;
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double refGama = 1.4;
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double prl = 0.72;
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double prl = 0.72;
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double prt = 0.90;
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double prt = 0.90;
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@ -878,6 +881,30 @@ double MUSCLCoefXk = -1;
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double MUSCLCoefXb = 1.0;
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double MUSCLCoefXb = 1.0;
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int allReduceStep = 1;
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int allReduceStep = 1;
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// ----------------- overlap configuration ------------------------------
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// codeOfOversetGrid: Overlapping(overset) grid or not.
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// 0 -- NON-overlapping grid.
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// 1 -- Overlapping grid.
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int codeOfOversetGrid = 0;
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int codeOfOversetSlipGrid = 0;
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int readOversetFileOrNot = 0;
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int symetryOrNot = 0;
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int readInAuxiliaryInnerGrid = 1;
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int readInAuxiliaryOuterGrid = 0;
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int readInSklFileOrNot = 0;
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string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||||
|
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||||
|
string auxiliaryInnerGrid2 = "";
|
||||||
|
string oversetGridFileName = "./grid/overlap.ovs";
|
||||||
|
double walldistMainZone = 1.0
|
||||||
|
double toleranceForOversetSearch = 1.0e-3;
|
||||||
|
double toleranceForOversetBox = 1.0e-3;
|
||||||
|
int twoOrderInterpolationOrNot = 0;
|
||||||
|
int keyEnlargeOfActiveNodes = 0;
|
||||||
|
int outTecplotOverset = 0;
|
||||||
|
|
||||||
|
int numberOfMovingBodies = 2;
|
||||||
|
|
||||||
// ---------------- ATP read --------------------------------------------
|
// ---------------- ATP read --------------------------------------------
|
||||||
//@int inflowParaType = 0;
|
//@int inflowParaType = 0;
|
||||||
//@double refReNumber = 2.329418E08;
|
//@double refReNumber = 2.329418E08;
|
||||||
|
|
@ -888,3 +915,9 @@ int allReduceStep = 1;
|
||||||
//@int nsubsonicOutlet = 0;
|
//@int nsubsonicOutlet = 0;
|
||||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||||
|
|
||||||
|
#########################################################################
|
||||||
|
# Old Parameter #
|
||||||
|
#########################################################################
|
||||||
|
int isPlotVolumeField = 0;
|
||||||
|
|
||||||
|
|
@ -0,0 +1,193 @@
|
||||||
|
#########################################################################
|
||||||
|
# General Control Parameter #
|
||||||
|
#########################################################################
|
||||||
|
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||||
|
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||||
|
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||||
|
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||||
|
// intervalStepRes: The step intervals for residual 'res.dat' saved.
|
||||||
|
|
||||||
|
int maxSimuStep = 25000;
|
||||||
|
|
||||||
|
int intervalStepFlow = 1000;
|
||||||
|
int intervalStepPlot = 1000;
|
||||||
|
int intervalStepForce = 100;
|
||||||
|
int intervalStepRes = 10;
|
||||||
|
|
||||||
|
#########################################################################
|
||||||
|
# Inflow Parameter #
|
||||||
|
#########################################################################
|
||||||
|
// refMachNumber: Mach number.
|
||||||
|
// attackd: Angle of attack.
|
||||||
|
// angleSlide: Angle of sideslip.
|
||||||
|
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
||||||
|
// inflowParaType: The type of inflow parameters.
|
||||||
|
// 0 -- the nondimensional conditions.
|
||||||
|
// 1 -- the flight conditions.
|
||||||
|
// 2 -- the experiment conditions.
|
||||||
|
// 3 -- the subsonic boundary conditions.
|
||||||
|
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
||||||
|
// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
|
||||||
|
// freestream_vibration_temperature: Dimensional freestream vibration temperature.
|
||||||
|
// refDimensionalPressure: Dimensional reference pressure, or the total pressure only for the experiment condition.
|
||||||
|
// height: Fly height, unit of km.
|
||||||
|
// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
|
||||||
|
// 1 dm = 0.1 m.
|
||||||
|
// 1 cm = 0.01 m.
|
||||||
|
// 1 mm = 0.001m.
|
||||||
|
// 1 inch = 0.0254m.
|
||||||
|
// 1 foot = 12 inches = 0.3048m.
|
||||||
|
// 1 yard = 3 feet = 0.9144m.
|
||||||
|
// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
|
||||||
|
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
|
||||||
|
|
||||||
|
double refMachNumber = 10.00;
|
||||||
|
double attackd = 0.00;
|
||||||
|
double angleSlide = 0.00;
|
||||||
|
|
||||||
|
double wallTemperature = 294.0;
|
||||||
|
|
||||||
|
int inflowParaType = 0;
|
||||||
|
double refReNumber = 1.0e5;
|
||||||
|
double refDimensionalTemperature = 79.0;
|
||||||
|
|
||||||
|
//int inflowParaType = 1;
|
||||||
|
//double height = 0.001;
|
||||||
|
|
||||||
|
//int inflowParaType = 2;
|
||||||
|
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||||
|
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||||
|
|
||||||
|
double gridScaleFactor = 1.0;
|
||||||
|
|
||||||
|
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||||
|
double forceRefenenceLength = 1.0; // unit of meter.
|
||||||
|
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||||
|
double TorqueRefX = 0.0; // unit of meter.
|
||||||
|
double TorqueRefY = 0.0; // unit of meter.
|
||||||
|
double TorqueRefZ = 0.0; // unit of meter.
|
||||||
|
|
||||||
|
#########################################################################
|
||||||
|
# Physical models #
|
||||||
|
#########################################################################
|
||||||
|
// viscousType: Viscous model.
|
||||||
|
// 0 -- Euler.
|
||||||
|
// 1 -- Lamilar.
|
||||||
|
// 3 -- 1eq turbulent.
|
||||||
|
// 4 -- 2eq turbulent.
|
||||||
|
// viscousName: Laminar or tubulent model.
|
||||||
|
// -- "1eq-sa", when viscousType = 3.
|
||||||
|
// -- "2eq-kw-menter-sst", when viscousType = 4.
|
||||||
|
// DESType: Type of DES.
|
||||||
|
// 0 -- RANS.(default)
|
||||||
|
// 1 -- DES.
|
||||||
|
// 2 -- DDES.
|
||||||
|
// 3 -- IDDES.
|
||||||
|
|
||||||
|
//int viscousType = 0;
|
||||||
|
//string viscousName = "Euler";
|
||||||
|
|
||||||
|
int viscousType = 1;
|
||||||
|
string viscousName = "laminar";
|
||||||
|
|
||||||
|
//int viscousType = 3;
|
||||||
|
//string viscousName = "1eq-sa";
|
||||||
|
|
||||||
|
//int viscousType = 4;
|
||||||
|
//string viscousName = "2eq-kw-menter-sst";
|
||||||
|
|
||||||
|
int DESType = 0;
|
||||||
|
|
||||||
|
int roeEntropyFixMethod = 2;
|
||||||
|
double roeEntropyScale = 0.0001;
|
||||||
|
#########################################################################
|
||||||
|
# Spatial Discretisation #
|
||||||
|
#########################################################################
|
||||||
|
#*******************************************************************
|
||||||
|
# Struct Solver *
|
||||||
|
#*******************************************************************
|
||||||
|
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||||
|
// Using this when solve structered grid or hybrid.
|
||||||
|
// -- "vanleer", "steger", "ausmpw".
|
||||||
|
// str_limiter_name: Limiter of struct grid.
|
||||||
|
// -- "minmod", "3rd_minmod_smooth".
|
||||||
|
|
||||||
|
string inviscidSchemeName = "steger";
|
||||||
|
string str_limiter_name = "minmod";
|
||||||
|
|
||||||
|
#*******************************************************************
|
||||||
|
# UnStruct Solver *
|
||||||
|
#*******************************************************************
|
||||||
|
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||||
|
// Using this when solve Unstructered grid or hybrid.
|
||||||
|
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||||
|
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
|
||||||
|
// uns_limiter_name: Limiter of Unstruct grid.
|
||||||
|
// -- "vencat", "barth".
|
||||||
|
// -- "1st", meaning accuracy of first-order.
|
||||||
|
// -- "nolim", no limiter.
|
||||||
|
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'.
|
||||||
|
// The smaller the value, the more robust it is.
|
||||||
|
|
||||||
|
string uns_scheme_name = "vanleer";
|
||||||
|
string uns_limiter_name = "vencat";
|
||||||
|
double venkatCoeff = 0.5;
|
||||||
|
|
||||||
|
#########################################################################
|
||||||
|
# Temporal Discretisation #
|
||||||
|
#########################################################################
|
||||||
|
// iunsteady: Steady or unsteady.
|
||||||
|
// 0 -- steady.
|
||||||
|
// 1 -- unsteay.
|
||||||
|
// CFLEnd: The CFL number, [0.1, 100].
|
||||||
|
// The bigger the value, the convergence faster but lower robustness.
|
||||||
|
// ktmax: The lower the value, the more robustness, 1.0e5 - 1.0e10.
|
||||||
|
|
||||||
|
int iunsteady = 0;
|
||||||
|
|
||||||
|
double CFLEnd = 10.0;
|
||||||
|
int CFLVaryStep = 100;
|
||||||
|
double ktmax = 1.0e10;
|
||||||
|
|
||||||
|
#########################################################################
|
||||||
|
# File In or Out #
|
||||||
|
#########################################################################
|
||||||
|
// gridfile: The partitioned Grid file path, using relative path,
|
||||||
|
// which is relative to the working directory.
|
||||||
|
// IMPORTANT WARNING: The file index should be ignored,
|
||||||
|
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
||||||
|
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||||
|
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||||
|
|
||||||
|
string gridfile = "./grid/3dball.fts";
|
||||||
|
int plotFieldType = 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),
|
||||||
|
// -- 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).
|
||||||
|
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||||
|
// Variables order must from small to big.
|
||||||
|
|
||||||
|
int nVisualVariables = 8;
|
||||||
|
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||||
|
|
||||||
|
// limitVariables: Limit model (It is useful only if limitVector is 0).
|
||||||
|
// 0 -- limit only for pressure and denstiny, then get the min value.
|
||||||
|
// 1 -- limit for every variables, then get the min value.
|
||||||
|
// limitVector:
|
||||||
|
// 0 -- Each variable use the same limiter coefficient.
|
||||||
|
// 1 -- Each variable use the respective limiter coefficients.
|
||||||
|
// reconmeth:
|
||||||
|
// 0 -- When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
||||||
|
// 1 -- Q+, Q- use the min limiter coefficients of left and right cell.
|
||||||
|
|
||||||
|
int reconmeth = 0;
|
||||||
|
int limitVariables = 0;
|
||||||
|
int limitVector = 1;
|
||||||
|
|
@ -8,8 +8,8 @@
|
||||||
// 1 -- Y upward. (default)
|
// 1 -- Y upward. (default)
|
||||||
// 2 -- Z upward.
|
// 2 -- Z upward.
|
||||||
// from_gtype: Type of grid data type in grid conversion process.
|
// from_gtype: Type of grid data type in grid conversion process.
|
||||||
// -1 -- MULTI_TYPE
|
// -1 -- MULTI_TYPE.
|
||||||
// 1 -- HyperFLOW( PHengLEI ), *.fts.
|
// 1 -- PHengLEI, *.fts.
|
||||||
// 2 -- CGNS, *.cgns.
|
// 2 -- CGNS, *.cgns.
|
||||||
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
// 3 -- Plot3D type of structured grid, *.dat/*.grd.
|
||||||
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
// 4 -- Fieldview type of unstructured grid, *.dat/*.inp.
|
||||||
|
|
@ -28,7 +28,3 @@ int from_gtype = 3;
|
||||||
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
// out_gfile: path of target file for grid convert to, *.fts type of file usually.
|
||||||
string from_gfile = "./grid/3dball.grd";
|
string from_gfile = "./grid/3dball.grd";
|
||||||
string out_gfile = "./grid/3dball.fts";
|
string out_gfile = "./grid/3dball.fts";
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
|
|
@ -0,0 +1,53 @@
|
||||||
|
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 = 14;
|
||||||
|
//string parafilename = "./bin/integrative_solver.hypara";
|
||||||
|
|
||||||
|
//int nsimutask = 99;
|
||||||
|
//string parafilename = "./bin/post_processing.hypara";
|
||||||
|
|
||||||
|
// ---------------- Advanced Parameters, DO NOT care it ----------------
|
||||||
|
int numberOfGridProcessor = 0;
|
||||||
|
// ATP read
|
||||||
|
//@string parafilename1 = ""
|
||||||
|
//@string parafilename2 = "";
|
||||||
|
|
@ -0,0 +1,21 @@
|
||||||
|
// pgridtype: The grid type.
|
||||||
|
// 0 -- unstruct grid.
|
||||||
|
// 1 -- struct grid.
|
||||||
|
// maxproc: The number of partition zones that want to be divided into,
|
||||||
|
// which is equal to the number of CPU processors you want.
|
||||||
|
// Usually, 50~100 thousands structured cells per CPU-Core is suggested.
|
||||||
|
// 30~70 thousands unstructured cells per CPU-Core is suggested.
|
||||||
|
// original_grid_file: Original grid file that want to be divided(PHengLEI type, *.fts).
|
||||||
|
// partition_grid_file: Target partition grid file(PHengLEI type, *.fts).
|
||||||
|
|
||||||
|
int pgridtype = 1;
|
||||||
|
int maxproc = 1;
|
||||||
|
|
||||||
|
string original_grid_file = "./grid/3dball.fts";
|
||||||
|
string partition_grid_file = "./grid/3dball.fts";
|
||||||
|
|
||||||
|
// numberOfMultigrid: Number of multi-grid levels, ONLY used for structured grid.
|
||||||
|
// 1 -- single level.
|
||||||
|
// 2 -- 2 level.
|
||||||
|
// N -- N level,..., et al.
|
||||||
|
int numberOfMultigrid = 1;
|
||||||
|
|
@ -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 = 25000;
|
|
||||||
|
|
||||||
int intervalStepFlow = 1000;
|
|
||||||
int intervalStepPlot = 1000;
|
|
||||||
int intervalStepForce = 100;
|
|
||||||
int intervalStepRes = 10;
|
|
||||||
|
|
||||||
#########################################################################
|
|
||||||
# Inflow Parameter #
|
|
||||||
#########################################################################
|
|
||||||
// refMachNumber: Mach number per meter.
|
|
||||||
// attackd: Angle of attack.
|
|
||||||
// angleSlide: Angle of sideslip.
|
|
||||||
// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
|
|
||||||
// refDimensionalTemperature: dimensional reference temperature, or the total temperature only for the experiment condition.
|
|
||||||
// refDimensionalPressure: dimensional reference pressure , or the total pressure only for the experiment condition.
|
|
||||||
// inflowParaType: the type of inflow parameters.
|
|
||||||
// 0 - the nondimensional conditions.
|
|
||||||
// 1 - the flight conditions.
|
|
||||||
// 2 - the experiment conditions.
|
|
||||||
// height: Fly height, unit of km.
|
|
||||||
// wallTemperature: Temprature of the solid wall, minus value is for adiabatic boundary condition.
|
|
||||||
// dump_Q: Dump out thermal flux Q of solid wall.
|
|
||||||
// 0 - no dump out.
|
|
||||||
// 1 - dump out wall Q only.
|
|
||||||
// 2 - dump out wall Q & the typical position Q of ball.
|
|
||||||
// 3 - dump out wall Q & the typical position Q of cone.
|
|
||||||
// 4 - dump out wall Q & the typical position Q of double sphere.
|
|
||||||
// gridScaleFactor: The customizable unit of the grid, default value 1.0 metre.
|
|
||||||
// forceRefenenceLength, forceRefenenceArea: Reference length and area, independent to grid scale.
|
|
||||||
// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent to grid scale.
|
|
||||||
|
|
||||||
double refMachNumber = 10.00;
|
|
||||||
double attackd = 0.00;
|
|
||||||
double angleSlide = 0.00;
|
|
||||||
|
|
||||||
double wallTemperature = 294.0 ;
|
|
||||||
int dump_Q = 2;
|
|
||||||
|
|
||||||
int inflowParaType = 0;
|
|
||||||
double refReNumber = 1.0e5;
|
|
||||||
double refDimensionalTemperature = 79.0;
|
|
||||||
|
|
||||||
//int inflowParaType = 1;
|
|
||||||
//double height = 0.001;
|
|
||||||
|
|
||||||
//int inflowParaType = 2;
|
|
||||||
//double refDimensionalTemperature = 6051.024; //the total temperature, T*(1+(gama0-1)*M*M/2).
|
|
||||||
//double refDimensionalPressure = 4.299696E09; //the total pressure, p*(T0/T)^(gama0/(gama0-1)).
|
|
||||||
|
|
||||||
double gridScaleFactor = 1.0;
|
|
||||||
|
|
||||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
|
||||||
double forceRefenenceLength = 1.0; // unit of meter.
|
|
||||||
double forceRefenenceArea = 1.0; // unit of meter^2
|
|
||||||
double TorqueRefX = 0.0; // unit of meter.
|
|
||||||
double TorqueRefY = 0.0; // unit of meter.
|
|
||||||
double TorqueRefZ = 0.0; // unit of meter.
|
|
||||||
|
|
||||||
#*******************************************************************
|
|
||||||
# Physical models *
|
|
||||||
#*******************************************************************
|
|
||||||
// iviscous: Viscous model
|
|
||||||
// 0 - Euler
|
|
||||||
// 1 - Lamilar
|
|
||||||
// 3 - 1eq turbulent
|
|
||||||
// 4 - 2eq turbulent
|
|
||||||
// viscousName : Laminar or tubulent model
|
|
||||||
// - "1eq-sa", when iviscous = 3
|
|
||||||
// - "2eq-kw-menter-sst", when iviscous = 4
|
|
||||||
// DESType : Type of DES
|
|
||||||
// 0 - RANS (default);
|
|
||||||
// 1 - DES;
|
|
||||||
// 2 - DDES;
|
|
||||||
// 3 - IDDES;
|
|
||||||
|
|
||||||
//int iviscous = 0;
|
|
||||||
//string viscousName = "Euler";
|
|
||||||
|
|
||||||
int viscousType = 1;
|
|
||||||
string viscousName = "laminar";
|
|
||||||
|
|
||||||
//int iviscous = 3;
|
|
||||||
//string viscousName = "1eq-sa";
|
|
||||||
|
|
||||||
//int iviscous = 4;
|
|
||||||
//string viscousName = "2eq-kw-menter-sst";
|
|
||||||
|
|
||||||
int DESType = 0;
|
|
||||||
|
|
||||||
int roeEntropyFixMethod = 2;
|
|
||||||
double roeEntropyScale = 0.0001;
|
|
||||||
#########################################################################
|
|
||||||
# Spatial Discretisation #
|
|
||||||
#########################################################################
|
|
||||||
#*******************************************************************
|
|
||||||
# Struct Solver *
|
|
||||||
#*******************************************************************
|
|
||||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid
|
|
||||||
// Using this when solve structered grid or hybrid.
|
|
||||||
// - "vanleer", "steger", "ausmpw"
|
|
||||||
// str_limiter_name: Limiter of struct grid
|
|
||||||
// - "minmod", "3rd_minmod_smooth"
|
|
||||||
|
|
||||||
string inviscidSchemeName = "steger";
|
|
||||||
string str_limiter_name = "minmod";
|
|
||||||
|
|
||||||
#*******************************************************************
|
|
||||||
# UnStruct Solver *
|
|
||||||
#*******************************************************************
|
|
||||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid
|
|
||||||
// Using this when solve Unstructered grid or hybrid.
|
|
||||||
// - "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle"
|
|
||||||
// - "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus"
|
|
||||||
// uns_limiter_name: Limiter of Unstruct grid
|
|
||||||
// - "vencat", "barth"
|
|
||||||
// - "1st", meaning accuracy of first-order.
|
|
||||||
// - "nolim", no limiter.
|
|
||||||
// venkatCoeff: Coefficient of vencat limiter, when uns_limiter_name = 'vencat'
|
|
||||||
// The smaller the value, the more robust it is.
|
|
||||||
|
|
||||||
string uns_scheme_name = "vanleer";
|
|
||||||
string uns_limiter_name = "vencat";
|
|
||||||
double venkatCoeff = 0.5;
|
|
||||||
|
|
||||||
#########################################################################
|
|
||||||
# Temporal Discretisation #
|
|
||||||
#########################################################################
|
|
||||||
// iunsteady: Steady or unsteady.
|
|
||||||
// 0 - steady
|
|
||||||
// 1 - unsteay
|
|
||||||
// CFLEnd: The CFL number, [0.1, 100]
|
|
||||||
// The bigger the value, the convergence faster but lower robustness.
|
|
||||||
// ktmax: The lower the value, the more robustness, 1.0e5 ~ 1.0e10.
|
|
||||||
|
|
||||||
int iunsteady = 0;
|
|
||||||
|
|
||||||
double CFLEnd = 10.0;
|
|
||||||
int CFLVaryStep = 100;
|
|
||||||
double ktmax = 1.0e10;
|
|
||||||
|
|
||||||
|
|
||||||
#########################################################################
|
|
||||||
# File In or Out #
|
|
||||||
#########################################################################
|
|
||||||
// gridfile: The partitioned Grid file path, using relative path,
|
|
||||||
// which is relative to the working directory.
|
|
||||||
// IMPORTANT WARNNING: the file index should be ignored,
|
|
||||||
// e.g. if the partitioned grid is rae2822_hybrid2d__4_0.fts,
|
|
||||||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
|
||||||
// isPlotVolumeField: If dump out the whole field results to tecplot or not, 0/1.
|
|
||||||
|
|
||||||
string gridfile = "./grid/3dball.fts";
|
|
||||||
int isPlotVolumeField = 0;
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
|
||||||
// nVisualVariables: number of variables want to be dumped for tecplot visualization.
|
|
||||||
// visualVariables : variable types dumped, listed as following:
|
|
||||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6)
|
|
||||||
// -- viscosityLaminar(7), viscosityTurbulent(8)
|
|
||||||
// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), strain_rate(13), Q_criteria(14)
|
|
||||||
// -- Cp(15), timeStep(16), volume(17)
|
|
||||||
// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21)
|
|
||||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
|
|
||||||
// Arriables order must from small to larger.
|
|
||||||
int nVisualVariables = 8;
|
|
||||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|
||||||
|
|
||||||
// limitVariables: limit model.
|
|
||||||
// 0 - limit only for pressure and denstiny, then get the min value
|
|
||||||
// 1 - limit for every variables, then get the min value
|
|
||||||
// limitVector:
|
|
||||||
// 0 - Each variable use the same limiter coefficient.
|
|
||||||
// 1 - Each variable use the respective limiter coefficients.
|
|
||||||
// reconmeth:
|
|
||||||
// 0 - When reconstruct face value, Q+, Q- use respective limiter coefficients.
|
|
||||||
// 1 - Q+, Q- use the min limiter coefficients of left and right cell.
|
|
||||||
int reconmeth = 0;
|
|
||||||
int limitVariables = 0;
|
|
||||||
int limitVector = 1;
|
|
||||||
|
|
@ -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 = 3;
|
|
||||||
int nparafile = 1;
|
|
||||||
int nsimutask = 0;
|
|
||||||
string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
|
||||||
//string parafilename = "./bin/cfd_para_transonic.hypara";
|
|
||||||
//string parafilename = "./bin/cfd_para_supersonic.hypara";
|
|
||||||
//string parafilename = "./bin/cfd_para_hypersonic.hypara";
|
|
||||||
//string parafilename = "./bin/incompressible.hypara";
|
|
||||||
//int nsimutask = 1;
|
|
||||||
//string parafilename = "./bin/grid_para.hypara";
|
|
||||||
//int nsimutask = 2;
|
|
||||||
//string parafilename = "./bin/cfd_para.hypara";
|
|
||||||
//int nsimutask = 3;
|
|
||||||
//string parafilename = "./bin/partition.hypara";
|
|
||||||
//int nsimutask = 4;
|
|
||||||
//string parafilename = "./bin/repository.hypara";
|
|
||||||
//int nsimutask = 5;
|
|
||||||
//string parafilename = "./bin/overset_grid_view.hypara";
|
|
||||||
//int nsimutask = 99;
|
|
||||||
//string parafilename = "./bin/post_processing.hypara";
|
|
||||||
// ---------------- advanced Parameters, DO NOT care it -----------
|
|
||||||
int iovrlap = 0;
|
|
||||||
int numberOfGridProcessor = 0;
|
|
||||||
// ATP read
|
|
||||||
string parafilename1 = ""
|
|
||||||
string parafilename2 = "";
|
|
||||||
|
|
||||||
|
|
@ -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/3dball.fts";
|
|
||||||
string partition_grid_file = "./grid/3dball.fts";
|
|
||||||
|
|
||||||
|
|
||||||
// Number of multi-grid levels, ONLY used for structured grid.
|
|
||||||
// 1 -- single level, 2 -- 2 level, N -- N level, ..., et al.
|
|
||||||
int numberOfMultigrid = 1;
|
|
||||||
|
|
||||||
|
|
||||||
|
|
||||||
Loading…
Reference in New Issue