forked from PHengLEI/PHengLEI-TestCases
PHengLEI2112版本已有算例参数及文档更新
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hechao
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@ -21,6 +21,7 @@
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// 1 -- Grid conversion, from other grid data to PHenglEI, such as Fluent, CGNS.
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// 2 -- Grid refinement.
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// 3 -- Grid merging, merge two blocks into one block.
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// 4 -- Grid deformation, achieve unstructured grid deformation.
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// 5 -- Grid repairing, repair the original grid in order to remove the negative volume cells.
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// 6 -- Grid mirroring, mirror a symmetry grid to whole grid.
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// multiblock: Multi-block grid or not, only for structured grid conversion.
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@ -72,13 +73,15 @@ int dumpOldGrid = 0;
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//-----------------------------------------------------------------------
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// from_gfile: path of original data file for unstructure grid convert from.
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// out_gfile: path of target file for grid convert to, *.fts type of file usually.
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int numberOfGridFile = 1;
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string from_gfile = "./grid/rae2822_hybrid2d.cas";
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string from_gfile1= "";
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string out_gfile = "./grid/flat_laminr_133_85_2d.fts";
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// ----------------- some advanced choices ------------------------------
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// iunsteady: The Grid is for unsteady simulation or not.
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int iunsteady = 0;
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int iale = 0;
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int codeOfAleModel = 0;
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// fileformat: Ustar Grid file format.
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@ -122,15 +125,38 @@ int isDeform = 0;
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int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
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int projectOrgPoint = 0; // if project original wall points.
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// ----------------- Grid Deform Parameters -----------------------------
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// deformationMethod: Grid Deform.
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// 1 -- SPRING.
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// 2 -- RBF.
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// stationalGridFile: Original grid file.
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// visualFileName : The visualization file path of deform grid.
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// nDeformStep : The max deform step.
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// flapAngle : The max flap angle.
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// rotatePostionZ : Rotate postion.
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// rotatePostionY : Rotate postion.
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// gridSlice : If dump slice grid.
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// sliceAxis : Grid slice axis.
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// slicePosition : Grid slice position.
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int nDeformStep = 40;
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double flapAngle = 10.0;
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double rotatePostionZ = 4.00003;
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double rotatePostionY = 3.05;
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int deformationMethod = 2;
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string stationalGridFile = "./grid/Segment2Brid.fts";
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string visualFileName = "./results/deformedGrid.dat"
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int gridSlice = 1;
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int sliceAxis = 1;
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double slicePosition = 13;
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// ----------------- RBF Parameters -------------------------------------
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// symmetryPlane: Which symmetry plane is used in the mesh.
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// 0 -- without symmetry.
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// 1 -- plane of x=0.
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// 2 -- plane of y=0.
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// 3 -- plane of z=0.
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int numberOfReferenceCP = 10;
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double influenceRadius = 20;
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int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
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// numberOfReferenceCP : Number of reference Control Points.
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// influencePara : The RBF influence radius parameter.
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int numberOfReferenceCP = 40;
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double influencePara = 25.0;
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// ----------------- Periodic Parameters --------------------------------
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// Notice: Rotational periodicity only support rotation along the X axis!
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@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
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// 0 -- without Periodic Boundary.
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// 1 -- Translational periodicity.
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// 2 -- Rotational periodicity.
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// translationLength[]: The relative distance between two periodic face
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which only support one direction.
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// rotationAngle: The relative angle between two periodic face.
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which is recorded in degrees.
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int periodicType = 0;
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double translationLength[] = [0.0,0.0,0.0];
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double rotationAngle = 0.0;
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@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
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// 0 -- Interface. (default)
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// 1 -- Physical boundary condition, used in Hybrid solver.
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// npartmethod: Method of interface reconstruction, default is 1.
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// parallelPartMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
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// parallelPartitionMethod: Method of parallel partition, this is set only when execute parallel partition. It would be skipped when serial partition.
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// 1 -- Using ParMetis for homogeneous MPI.
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// 2 -- Using Metis for homogeneous MPI.
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// 3 -- using METIS partition for homogeneous OpenMP.
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@ -238,6 +269,8 @@ int compressible = 1;
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// 1 -- the flight conditions.
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// 2 -- the experiment conditions.
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// 3 -- the subsonic boundary conditions.
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// 4 -- the condition that the velocity, temperature and density are given.
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// 5 -- the condition that the velocity, temperature and pressure are given.
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// refReNumber: Reynolds number, which is based unit length, unit of 1/m.
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// refDimensionalTemperature: Dimensional reference temperature, or the total temperature only for the experiment condition.
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// freestream_vibration_temperature: Dimensional freestream vibration temperature.
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@ -251,10 +284,12 @@ int compressible = 1;
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// 1 inch = 0.0254m.
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// 1 foot = 12 inches = 0.3048m.
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// 1 yard = 3 feet = 0.9144m.
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// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
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// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: Reference length, SpanWise length and area, independent of grid unit.
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// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
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// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
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// condition is radiation equilibrium temperature, and 0.8 is the default value.
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// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
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// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
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double refMachNumber = 0.73;
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double attackd = 2.79;
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@ -263,7 +298,7 @@ double angleSlide = 0.00;
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int inflowParaType = 0;
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double refReNumber = 6.5e6;
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double refDimensionalTemperature = 288.15;
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double freestream_vibration_temperature = 10000.00;
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double freestream_vibration_temperature = 300.00;
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//int inflowParaType = 1;
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//double height = 0.001;
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@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
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//double refDimensionalTemperature = 288.144;
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//double refDimensionalPressure = 1.01313E05;
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//The velocity, temperature and density are fixed.
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//int inflowParaType = 4;
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//double refDimensionalVelocity = 1000.0;
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//double refDimensionalDensity = 1.0e3;
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//The velocity, temperature and pressure are fixed.
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//int inflowParaType = 5;
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//double refDimensionalVelocity = 1000.0;
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//double refDimensionalPressure = 1.0e5;
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//The MachNumber, temperature and pressure are fixed.
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//int inflowParaType = 6;
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//double refDimensionalTemperature = 293;
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//double refDimensionalPressure = 8886.06;
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double wallTemperature = -1.0;
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double radiationCoef = 0.8;
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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 forceRefenenceLength = 1.0; // unit of meter.
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double forceRefenenceArea = 1.0; // unit of meter^2.
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double forceReferenceLengthSpanWise = 1.0; // unit of meter.
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double forceReferenceLength = 1.0; // unit of meter.
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double forceReferenceArea = 1.0; // unit of meter^2.
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double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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double TorqueRefZ = 0.0; // unit of meter.
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double refMolecularWeight = 28.9644; // unit of g/mol.
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//-----------------------------------------------------------------------
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# Spatial Discretisation #
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@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
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// Using this when solve structered grid or hybrid.
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// -- "vanleer", "steger", "hlle", "lax_f".
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// -- "roe", "modified_roe".
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// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
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// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
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// str_limiter_name: Limiter of struct grid.
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// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
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// -- "nolim", no limiter.
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@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
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// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
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// Using this when solve Unstructered grid or hybrid.
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// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
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// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpwplus".
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// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
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// uns_limiter_name: Limiter of Unstruct grid.
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// -- "barth", "vencat", "vanleer", "minmod".
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// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
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// -- "nolim", no limiter.
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// uns_vis_name: Discretisation method of viscous term.
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// -- "std", "test", "aver", "new1", "new2".
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// uns_gradient: Gradient reconstruction method.
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// gradientName: Gradient reconstruction method.
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// -- "default", "ggcell", "ggnode", "lsq".
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// ivencat: Variation of vencat limiter.
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// 0 -- org method, it is independent of grid scale.
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@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
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// 1 -- unsteay.
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// physicalTimeStep: The nondimensional physical time step.
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// ifStartFromSteadyResults: The unsteady simulation is start from steady flowfield or not, 0 is for no and else is for yes.
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// ifStaticsFlowField: Statistical variables for DES simulation.
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// ifStaticsFlowField: Statistical variables for unsteady simulation.
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// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
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// startStatisticStep: Outer step when start statistics.
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// when the value is larger than "maxSimuStep", it is useless.
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// statisticalTimePeriod: Used as time period of statistic analysis.
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// when the value is negative, time period is treated as infinite.
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// statisticMethod: Statistic reynolds stress method.
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0 --tau = <q^2> - <q>^2
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1 --tau = <u'u'>
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// min_sub_iter: The min sub iteration of unsteady simulation.
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// max_sub_iter: The max sub iteration of unsteady simulation.
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// tol_sub_iter: The tolerance of sub iteration of unsteady simulation.
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@ -454,7 +511,10 @@ int iunsteady = 0;
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double physicalTimeStep = 0.01;
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int ifStartFromSteadyResults = 0;
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int ifStaticsFlowField = 0;
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int ifStaticsReynoldsStress = 0;
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int startStatisticStep = 800000;
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double statisticalTimePeriod = -1.0;
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int statisticMethod = 0;
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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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@ -482,8 +542,6 @@ 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 dtsave = -1.0;
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int codeOfAleModel = 0;
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int aleStartStrategy = -1;
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int maxale = 10;
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double dtau = 0.001;
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@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
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int numberOfGridGroups = 1;
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string gridfile = "./grid/rae2822_hybrid2d__4.fts";
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string wallTemperaturefile= "";
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int walldistMethod = 1;
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@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
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string visualfile = "results/tecflow.plt";
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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 samplefile = "results/sample.dat";
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int nDumpSurfaceInfo = 0;
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string wall_varfile = "";
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string jetDefineFile = "bin/jet.hypara";
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string overset_gridfile = "results/iblank.ovs";
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string sixDofFileName = "results/sixDofInfo.dat";
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string derivativeFileName = "results/identify.dat";
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string hysteresisFileName = "results/force_beta.plt";
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int plotFieldType = 0;
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@ -554,6 +614,11 @@ int plotFieldType = 0;
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int visualfileType = 1;
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// samplefileMode: The dump mode of sample file.
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// 0 -- dump out every probe/line/surface data for all step intervals.
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// 1 -- dump out all probe/line/surface data for every step intervals.
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int samplefileMode = 0;
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// visualSlice: The slice of tecflow.
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// 0 -- Do not save slice data.
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// 1 -- comput and save it to sliceFile.
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@ -567,11 +632,13 @@ int visualSlice = 0;
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int sliceAxis = 1;
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double slicePostion = -0.5;
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string sliceFile = "results/Slice.plt";
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int dumpWallFaceCenter = 0;
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// min-max box of the visual block.
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double lowerPlotFieldBox[] = [0.0 0.0 0.0];
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double upperPlotFieldBox[] = [1.0 1.0 1.0];
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//-----------the optional parameters list for the flow field output----------------
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// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
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// visualVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
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@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
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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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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44), iblank(81).
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// -- specific heat ratio(gama, 56)
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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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//-----------the optional parameters list for the wall boundary condition----------------
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// nVisualWallVariables: The number of visual variables on wall.
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// visualWallVariables : dumped variable types, listed as following:
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// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
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// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
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// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
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// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
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// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
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// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
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// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
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// -overlap iblank(iblank, 81)
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int nVisualVariables = 8;
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int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
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int nVisualWallVariables = 9;
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int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
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// dumpStandardModel: Dump many standard model data.
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// 1 -- Turbulent flat plate.
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int dumpStandardModel = 0;
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@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 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 turbOrderStruct = 2;
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int kindOfTurbSource = 0;
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int mod_turb_res = 0;
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double turb_relax = 1.0;
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@ -652,6 +736,10 @@ double muoo = 3.0;
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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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int freeturbIntensitySRModify = 0;
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double freeDecayXLocation = 0.0;
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int compressibleCorrection = 0;
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int transitionMaFix = 1;
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# maximum eddy viscosity (myt/my) max.
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double eddyViscosityLimit = 1.0e10;
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@ -661,8 +749,8 @@ int monitor_vistmax = 0;
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# LES Parameter #
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//-----------------------------------------------------------------------
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// iLES: Create LESSolver or not.
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// >= 1 - Create LESSolver;
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// < 1 - not.
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// == 1 - Create LESSolver;
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// != 1 - not.
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// amplitudeofDisturb: Amplitude of adding disturb.
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// disturbstep: Unsteady time step or steady iteration of adding random disturb.
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// iterdisturb: Add random disturb in every sub-iter or only first sub-iter.
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@ -676,8 +764,9 @@ int monitor_vistmax = 0;
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// utau: friction velocity, using in DNSDisturb.
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// sgsmodel: subgrid scale model.
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// = "smagorinsky";
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// = "dsm";
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// = "wale".
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// = "dsmCom";
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// = "wale";
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// = "sigma".
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// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
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// = 2 - pow(deltai * deltaj *deltak, 1/3);
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// = 3 - Devloped by Scotti.
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@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
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int deltaFunctionType = 2;
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int wallDampingFunctionType = 1;
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int turbViscousCutType = 2;
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double smagConstant = 0.135;
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double smagConstant = 0.1;
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double isotropicConstant = 0.0;
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double waleConstant = 0.6;
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double sigmaConstant = 1.35;
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int filterDirection[] = [1, 1, 0];
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int averageDirection[] = [0, 0, 0];
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double testFilterScale = 2.0;
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@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
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// nm: Equation number of the physics, but is out of commision now.
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// 4 -- for 2D.
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// 5 -- for 3D.
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// nGasModel: The type of gas.
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// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
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// Otherwise, the pure gas with one component is used for perfect gas.
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// 0 -- Earth gas.
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// 1 -- Mars gas.
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// 2 -- Argon.
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// 3 -- Nitrogen.
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// nEnergyRecycle: The type of EnergyModel Recycle.
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// 0 -- not used .
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||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -57,9 +57,9 @@ double refDimensionalTemperature = 288.15;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -61,9 +61,9 @@ double freestream_vibration_temperature = 10000.0;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -57,9 +57,9 @@ double refDimensionalTemperature = 288.15;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -59,9 +59,9 @@ double refDimensionalTemperature = 300.33;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -60,9 +60,9 @@ double refDimensionalTemperature = 125.0;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -56,9 +56,9 @@ double refDimensionalTemperature = 288.15;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -56,9 +56,9 @@ double refDimensionalTemperature = 288.15;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -57,9 +57,9 @@ double refDimensionalTemperature = 288.0;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -56,9 +56,9 @@ double refDimensionalTemperature = 288;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -56,9 +56,9 @@ double refDimensionalTemperature = 298.15;
|
|||
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 0.1937; // unit of meter.
|
||||
double forceRefenenceArea = 0.12892; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 0.1937; // unit of meter.
|
||||
double forceReferenceArea = 0.12892; // unit of meter^2.
|
||||
double TorqueRefX = 0.66087; // unit of meter.
|
||||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -60,9 +60,9 @@ double refDimensionalTemperature = 79.0;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -61,9 +61,9 @@ double freestream_vibration_temperature = 10000.0;
|
|||
|
||||
double gridScaleFactor = 0.01;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -57,9 +57,9 @@ double refDimensionalTemperature = 298.33;
|
|||
|
||||
double gridScaleFactor = 0.0127;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
|
|
@ -26,14 +26,14 @@ string bcName = "FARFIELD";
|
|||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Inflow";
|
||||
string bcName = "INFLOW";
|
||||
{
|
||||
int bcType = 52;
|
||||
double totalPressure = 118309.784;
|
||||
double totalTemperature = 302.4;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
}
|
||||
string bcName = "Outflow";
|
||||
string bcName = "OUTFLOW";
|
||||
{
|
||||
int bcType = 62;
|
||||
double staticPressure = 115056.0;
|
||||
|
|
|
|||
|
|
@ -1,56 +0,0 @@
|
|||
# nBoundaryConditons : number of global boundary conditions.
|
||||
# bcName : Boundary Condition Name.
|
||||
# bcType(in PHengLEI): Boundary Condition Type.
|
||||
|
||||
# Account of how to set boundaryconditon.
|
||||
# string bcName = "Farfield";
|
||||
# {
|
||||
# int bcType = 4;
|
||||
# int inflowParaType = 1;
|
||||
# double attackd = 0;
|
||||
# double refReNumber = 6.5e6;
|
||||
# double refMachNumber = 3.5;
|
||||
# double angleSlide = 0;
|
||||
# }
|
||||
|
||||
int nBoundaryConditons = 5;
|
||||
string bcName = "SOLID_SURFACE";
|
||||
{
|
||||
int bcType = 2;
|
||||
}
|
||||
string bcName = "SYMMETRY";
|
||||
{
|
||||
int bcType = 3;
|
||||
}
|
||||
string bcName = "FARFIELD";
|
||||
{
|
||||
int bcType = 4;
|
||||
}
|
||||
string bcName = "Inflow";
|
||||
{
|
||||
int bcType = 52;
|
||||
double totalPressure = 118309.784;
|
||||
double totalTemperature = 302.4;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
}
|
||||
string bcName = "Outflow";
|
||||
{
|
||||
int bcType = 62;
|
||||
double staticPressure = 115056.0;
|
||||
}
|
||||
|
||||
# 'bcType' is defined as following:
|
||||
# 99: PERIODIC
|
||||
# -2: WAKE
|
||||
# -1: INTERFACE
|
||||
# 0 : NO_BOUNDARY_CONDITION
|
||||
# 1 : EXTRAPOLATION
|
||||
# 2 : SOLID_SURFACE
|
||||
# 3 : SYMMETRY
|
||||
# 4 : FARFIELD
|
||||
# 5 : INFLOW
|
||||
# 6 : OUTFLOW
|
||||
# 52: PRESSURE_INLET
|
||||
# 62: PRESSURE_OUTLET
|
||||
# 61: OUTFLOW_CONFINED
|
||||
# 7 : POLE
|
||||
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -60,9 +60,9 @@ double refDimensionalTemperature = 300.00;
|
|||
|
||||
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 forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
Binary file not shown.
|
|
@ -21,6 +21,7 @@
|
|||
// 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.
|
||||
// 4 -- Grid deformation, achieve unstructured grid deformation.
|
||||
// 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.
|
||||
|
|
@ -72,13 +73,15 @@ int dumpOldGrid = 0;
|
|||
//-----------------------------------------------------------------------
|
||||
// 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.
|
||||
int numberOfGridFile = 1;
|
||||
string from_gfile = "./grid/rae2822_hybrid2d.cas";
|
||||
string from_gfile1= "";
|
||||
|
||||
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 codeOfAleModel = 0;
|
||||
|
||||
// fileformat: Ustar Grid file format.
|
||||
|
|
@ -122,15 +125,38 @@ int isDeform = 0;
|
|||
int exclusiveCase = 0; // 0: NON case; 1: JSM-C2-NPOFF case; 2: CHNT.
|
||||
int projectOrgPoint = 0; // if project original wall points.
|
||||
|
||||
|
||||
// ----------------- Grid Deform Parameters -----------------------------
|
||||
// deformationMethod: Grid Deform.
|
||||
// 1 -- SPRING.
|
||||
// 2 -- RBF.
|
||||
// stationalGridFile: Original grid file.
|
||||
// visualFileName : The visualization file path of deform grid.
|
||||
// nDeformStep : The max deform step.
|
||||
// flapAngle : The max flap angle.
|
||||
// rotatePostionZ : Rotate postion.
|
||||
// rotatePostionY : Rotate postion.
|
||||
// gridSlice : If dump slice grid.
|
||||
// sliceAxis : Grid slice axis.
|
||||
// slicePosition : Grid slice position.
|
||||
int nDeformStep = 40;
|
||||
double flapAngle = 10.0;
|
||||
double rotatePostionZ = 4.00003;
|
||||
double rotatePostionY = 3.05;
|
||||
|
||||
int deformationMethod = 2;
|
||||
string stationalGridFile = "./grid/Segment2Brid.fts";
|
||||
string visualFileName = "./results/deformedGrid.dat"
|
||||
|
||||
int gridSlice = 1;
|
||||
int sliceAxis = 1;
|
||||
double slicePosition = 13;
|
||||
|
||||
// ----------------- 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;
|
||||
// numberOfReferenceCP : Number of reference Control Points.
|
||||
// influencePara : The RBF influence radius parameter.
|
||||
int numberOfReferenceCP = 40;
|
||||
double influencePara = 25.0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice: Rotational periodicity only support rotation along the X axis!
|
||||
|
|
@ -138,6 +164,11 @@ int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of
|
|||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
// translationLength[]: The relative distance between two periodic face
|
||||
which only support one direction.
|
||||
// rotationAngle: The relative angle between two periodic face.
|
||||
which is recorded in degrees.
|
||||
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
|
@ -180,7 +211,7 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 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.
|
||||
// parallelPartitionMethod: 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.
|
||||
|
|
@ -238,6 +269,8 @@ int compressible = 1;
|
|||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
// 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.
|
||||
|
|
@ -251,10 +284,12 @@ int compressible = 1;
|
|||
// 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.
|
||||
// forceReferenceLength, forceReferenceLengthSpanWise, forceReferenceArea: 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.
|
||||
// refMolecularWeight : the reference molecular weight of gas used for perfect gas. The unit is g/mol.
|
||||
// Generally, the gas is air. Sometimes, it is experiment gas, such as Nitrogen, Argon, and so on.
|
||||
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
|
|
@ -263,7 +298,7 @@ double angleSlide = 0.00;
|
|||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
double refDimensionalTemperature = 288.15;
|
||||
double freestream_vibration_temperature = 10000.00;
|
||||
double freestream_vibration_temperature = 300.00;
|
||||
|
||||
//int inflowParaType = 1;
|
||||
//double height = 0.001;
|
||||
|
|
@ -280,18 +315,34 @@ double freestream_vibration_temperature = 10000.00;
|
|||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
//The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalDensity = 1.0e3;
|
||||
|
||||
//The velocity, temperature and pressure are fixed.
|
||||
//int inflowParaType = 5;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
//double refDimensionalPressure = 1.0e5;
|
||||
|
||||
//The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
double gridScaleFactor = 1.0;
|
||||
|
||||
int numberOfAerodynamicForceComponents = 1;
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
|
|
@ -303,7 +354,7 @@ double TorqueRefZ = 0.0; // unit of meter.
|
|||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw".
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
|
|
@ -339,14 +390,14 @@ string str_limiter_name = "vanalbada";
|
|||
// 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".
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// 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.
|
||||
// gradientName: Gradient reconstruction method.
|
||||
// -- "default", "ggcell", "ggnode", "lsq".
|
||||
// ivencat: Variation of vencat limiter.
|
||||
// 0 -- org method, it is independent of grid scale.
|
||||
|
|
@ -408,9 +459,15 @@ double roeEntropyScale = 1.0;
|
|||
// 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.
|
||||
// ifStaticsFlowField: Statistical variables for unsteady simulation.
|
||||
// ifStaticsReynoldsStress: Statistical Reynolds stress for unsteady simulation.
|
||||
// startStatisticStep: Outer step when start statistics.
|
||||
// when the value is larger than "maxSimuStep", it is useless.
|
||||
// statisticalTimePeriod: Used as time period of statistic analysis.
|
||||
// when the value is negative, time period is treated as infinite.
|
||||
// statisticMethod: Statistic reynolds stress method.
|
||||
0 --tau = <q^2> - <q>^2
|
||||
1 --tau = <u'u'>
|
||||
// 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.
|
||||
|
|
@ -454,7 +511,10 @@ int iunsteady = 0;
|
|||
double physicalTimeStep = 0.01;
|
||||
int ifStartFromSteadyResults = 0;
|
||||
int ifStaticsFlowField = 0;
|
||||
int ifStaticsReynoldsStress = 0;
|
||||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
|
|
@ -482,8 +542,6 @@ double turbCFLScale = 1.0;
|
|||
double csrv = 2.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int codeOfAleModel = 0;
|
||||
int aleStartStrategy = -1;
|
||||
int maxale = 10;
|
||||
double dtau = 0.001;
|
||||
|
||||
|
|
@ -524,6 +582,7 @@ double lamda[] = 0.5, 1.0;
|
|||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile= "";
|
||||
|
||||
int walldistMethod = 1;
|
||||
|
||||
|
|
@ -536,15 +595,16 @@ string turbfile = "results/turb.dat";
|
|||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string samplefile = "results/sample.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string overset_gridfile = "results/iblank.ovs";
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
||||
int plotFieldType = 0;
|
||||
|
||||
|
|
@ -554,6 +614,11 @@ int plotFieldType = 0;
|
|||
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
// 0 -- dump out every probe/line/surface data for all step intervals.
|
||||
// 1 -- dump out all probe/line/surface data for every step intervals.
|
||||
int samplefileMode = 0;
|
||||
|
||||
// visualSlice: The slice of tecflow.
|
||||
// 0 -- Do not save slice data.
|
||||
// 1 -- comput and save it to sliceFile.
|
||||
|
|
@ -567,11 +632,13 @@ int visualSlice = 0;
|
|||
int sliceAxis = 1;
|
||||
double slicePostion = -0.5;
|
||||
string sliceFile = "results/Slice.plt";
|
||||
int dumpWallFaceCenter = 0;
|
||||
|
||||
// min-max box of the visual block.
|
||||
double lowerPlotFieldBox[] = [0.0 0.0 0.0];
|
||||
double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
||||
|
||||
//-----------the optional parameters list for the flow field output----------------
|
||||
// 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),
|
||||
|
|
@ -582,11 +649,27 @@ double upperPlotFieldBox[] = [1.0 1.0 1.0];
|
|||
// -- 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), iblank(81).
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -transition gamaeff(gamaeff, 48),
|
||||
// -transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -overlap iblank(iblank, 81)
|
||||
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
int nVisualWallVariables = 9;
|
||||
int visualWallVariables[] = [0, 1, 2, 3, 4, 5, 9, 10, 11];
|
||||
|
||||
// dumpStandardModel: Dump many standard model data.
|
||||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
|
@ -644,6 +727,7 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// mod_turb_res: If modify the residuals for the cells next to the wall or not, default is 0.
|
||||
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
|
|
@ -652,6 +736,10 @@ double muoo = 3.0;
|
|||
double kwoo = 5.0;
|
||||
int transitionType = 0;
|
||||
double turbIntensity = -1.0;
|
||||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
|
|
@ -661,8 +749,8 @@ int monitor_vistmax = 0;
|
|||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
// iLES: Create LESSolver or not.
|
||||
// >= 1 - Create LESSolver;
|
||||
// < 1 - 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.
|
||||
|
|
@ -676,8 +764,9 @@ int monitor_vistmax = 0;
|
|||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
// = "smagorinsky";
|
||||
// = "dsm";
|
||||
// = "wale".
|
||||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
|
|
@ -700,9 +789,10 @@ string sgsmodel = "smagorinsky";
|
|||
int deltaFunctionType = 2;
|
||||
int wallDampingFunctionType = 1;
|
||||
int turbViscousCutType = 2;
|
||||
double smagConstant = 0.135;
|
||||
double smagConstant = 0.1;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
double sigmaConstant = 1.35;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [0, 0, 0];
|
||||
double testFilterScale = 2.0;
|
||||
|
|
@ -724,12 +814,42 @@ int monitorNegativeConstant = 0;
|
|||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
// nGasModel: The type of gas.
|
||||
// nGasModel: The type of gas. less than and equal to 1 represents the mixture gas.
|
||||
// Otherwise, the pure gas with one component is used for perfect gas.
|
||||
// 0 -- Earth gas.
|
||||
// 1 -- Mars gas.
|
||||
// 2 -- Argon.
|
||||
// 3 -- Nitrogen.
|
||||
// nEnergyRecycle: The type of EnergyModel Recycle.
|
||||
// 0 -- not used .
|
||||
// 1 -- used.
|
||||
// nDensityModify: The type of densitymodify.
|
||||
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nchem:
|
||||
// 0 -- without chemical reaction flow.
|
||||
// 1 -- the chemical reaction flow is considered.
|
||||
// nEquilibriumGas: the variable is valid when the condition of nchem=0 is satisfied.
|
||||
// 0 -- perfect gas.
|
||||
// 5, 7, 11 -- equilibrium gas, meanwhile, its value denotes the number of gas component.
|
||||
// nPCWCycleStep: the maximum step number of iteration in the module of computing species mass fractions with the partial catalytic wall(PCW) condition.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nRETCycleStep: the maximum step number of iteration in the module of computing radiation equilibrium temperature on wall.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSLIPCycleStep:the maximum step number of iteration in the module of computing slip temperature, slip velocity and slip species mass fraction.
|
||||
// the value equals to or is greater than 1, and 3 is for default value.
|
||||
// nSlipBCModel : The computational model of slip boundary conditions.
|
||||
|
||||
// 0 -- no slip.
|
||||
// 1 -- the conventional Maxwell slip conditions.
|
||||
// 2 -- the Gokcen slip conditions.
|
||||
// 3 -- the Knudsen-layer correction of the standard slip conditions proposed by Lockerby, et al.
|
||||
// 4 -- the Kogan simplified slip conditions.
|
||||
// nMeanFreePathType : the method to the mean free-path for the slip conditions. For the mixture, 0 is suggested.
|
||||
// 0 -- the equivalent mean free-path is calculated by the simple hard sphere model(HS).
|
||||
// 1 -- calculated by the definition that includes the variables of the number density and the molecule diameter.
|
||||
// 2 -- the equivalent mean free-path is calculated by the variable hard sphere model(VHS).
|
||||
// nchemsrc:
|
||||
// 0 -- the source terms are not computed.
|
||||
// 1 -- the source terms are computed.
|
||||
|
|
@ -740,15 +860,72 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the curve fitting method.
|
||||
// parkVDPower: the power of translational-rotational temperature in the Park V-D(vibration-dissociation) coupling model.
|
||||
// The value is in range of [0.0, 1.0], DPLR suggests 0.5, LAURA suggests 0.7, while 0.6 is given as default value.
|
||||
// catalyticCoef:
|
||||
// 0.0 -- full non-catalytic wall boundary condition.
|
||||
// 1.0 -- full catalytic wall boundary condition.
|
||||
// in range of (0.0, 1.0) -- partial catalytic condition, the value indicates the catalytic coefficient.
|
||||
// nIsSuperCatalytic : the super catalytic condition for the fully catalytic wall, and assigned with the value of 1.
|
||||
// 0 -- equilibrium condition for the fully catalytic wall where the mass fractions are assigned with the values of the free stream.
|
||||
// 1 -- super catalytic condition for the fully catalytic wall where all the atomic components combine into molecular components.
|
||||
// nTemperatureJump : the method to calculate the temperature jump.
|
||||
// 0 -- calculated by the variables of heat conductivity and constant volume specific heat for each energy mode.
|
||||
// 1 -- the general method where the iteration is calculated with the translation-rotation temperature.
|
||||
// sigmaVelocity: the coordination coefficient of tangential momentum for computation of slip velocity. The value is in range of (0.0, 2.0].
|
||||
// sigmaTemperature: the heat coordination coefficient for computation of slip temperature. The value is in range of (0.0, 2.0].
|
||||
// sigmaMassFraction: the species coordination coefficient for computation of slip mass fractions. The value is in range of (0.0, 2.0].
|
||||
// velocitySlipCorrectConstant: the correction constant to the velocity slip condition. For the diffuse reflection, 1.0 is used.
|
||||
// 1.0 -- proposed by Maxwell.
|
||||
// sqrt(2/PI)~0.8 -- used for "micro-slip", namely the actual velocity slip at the wall.
|
||||
// 1.146 -- proposed for an additional "fictitious" velocity slip.
|
||||
|
||||
// chemicalRelaxCorf: The value is in range of [0.001, 1.0].
|
||||
// chemicalSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// viscousSpectrumRadiusCoef : The value is in range of [1.0, 3.0].
|
||||
// inviscidSpectrumRadiusCoef: The value is in range of [1.0, 3.0].
|
||||
// staticPressureRelaxCorf: The value is in range of [0.1, 1.0].
|
||||
// nIsChemicalFreeze : the flag to freeze the chemical reactions.
|
||||
// 0 -- not freeze, the chemical reaction sources will be calculated.
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.// veTemperatureMin: The minimum of Tv and Te
|
||||
// nDebug: cout the Wrong place and abort
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
// isInjection:
|
||||
// 0 -- The injection velocity of ablation wall is not computed.
|
||||
// 1 -- The injection velocity of ablation wall is computed.
|
||||
// nViscosityModel:
|
||||
|
||||
// 0 -- Blottner fitting method.
|
||||
// 1 -- Gupta fitting method.
|
||||
// nSutherland:
|
||||
// 0 -- stands for selecting the Blotter curve fits mode.
|
||||
// 1 -- stands for Sutherland relation.
|
||||
// gasfile: Indicates the gas model, 9 models are provided, namely "Gu5", "Gu7", "Gu11", "Pa5", "Pa7", "Pa11", "DK5", "DK7", "DK11".
|
||||
// "Gu" -- indicates the Gupta Model, three-Type Models are embeded in the library, namely, the 5-species-6-reactions, the 7-species-9-reactions, the 11-species-20-reactions.
|
||||
// "Pa" -- indicates the Park Model, three-Type Models are embeded in the library, namely, the 5-species-17-reactions, the 7-species-22-reactions, the 11-species-48-reactions.
|
||||
// "DK" -- indicates the Dunn-Kang Model, three-Type Models are embeded in the library, namely, the 5-species-11-reactions, the 7-species-15-reactions, the 11-species-26-reactions.
|
||||
// "Mars-Pa8" is for Park model of Mars gas, "Mars-Mc8" for McKenzie model of Mars gas.
|
||||
// "Combustion-12" -- indicates the Combustion Chamber Gas Model which includes 12-species-20-reactions.
|
||||
// "Gas-Mixture" -- indicates the process of mixing two species without reacting.
|
||||
// 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.
|
||||
|
|
@ -758,6 +935,10 @@ int dg_high_order = 0;
|
|||
int iapplication = 0;
|
||||
int iCodeBranch = 0;
|
||||
int nm = 5;
|
||||
int nEquilibriumGas = 0;
|
||||
int nPCWCycleStep = 3;
|
||||
int nRETCycleStep = 3;
|
||||
int nSLIPCycleStep= 3;
|
||||
|
||||
double refGama = 1.4;
|
||||
double prl = 0.72;
|
||||
|
|
@ -770,23 +951,73 @@ int nchem = 0;
|
|||
int nchemsrc = 1;
|
||||
int nchemrad = 1;
|
||||
int ntmodel = 1;
|
||||
int nChemicalFlowStep = 0;
|
||||
|
||||
int nEnergyRecycle = 0;
|
||||
int nSlipBCModel = 0;
|
||||
int nDensityModify = 1;
|
||||
int nTEnergyModel = 0;
|
||||
int nMeanFreePathType = 0;
|
||||
int nIsChemicalFreeze = 0;
|
||||
int nIsSuperCatalytic = 1;
|
||||
int nTemperatureJump = 0;
|
||||
|
||||
double parkVDPower = 0.6;
|
||||
double catalyticCoef = 0.0;
|
||||
double sigmaVelocity = 1.0;
|
||||
double sigmaTemperature = 1.0;
|
||||
double sigmaMassFraction = 1.0;
|
||||
double velocitySlipCorrectConstant = 1.0;
|
||||
|
||||
double chemicalRelaxCorf = 1.0;
|
||||
double chemicalSpectrumRadiusCoef = 1.0;
|
||||
double viscousSpectrumRadiusCoef = 1.0;
|
||||
double inviscidSpectrumRadiusCoef = 1.0;
|
||||
double staticPressureRelaxCorf = 1.0;
|
||||
|
||||
double veTemperatureMin = 30.0;
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 0;
|
||||
int nTurblenceForChemical = 0;
|
||||
int nViscosityFluxSublevelModified = 0 ;
|
||||
int nChemcalSourceModified = 0;
|
||||
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.767";
|
||||
|
||||
//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 initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 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";
|
||||
|
||||
//string gasfile = "DK7";
|
||||
//string speciesName = "O, O2, NO, N, NO+, C, C2, CO, CO2, CN, N2, e-";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767, 0.0";
|
||||
|
||||
//string gasfile = "Combustion-12";
|
||||
//string speciesName = "O, O2, NO, N, C, CO, CO2, H, H2, OH, H2O, N2";
|
||||
//string initMassFraction = "0.0, 0.233, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.767";
|
||||
|
||||
//string gasfile = "Gas-Mixture";
|
||||
//string speciesName ="SpeciesA, SpeciesB";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
int nSutherland = 0;
|
||||
double gamaSpeciesA = 1.4;
|
||||
double gamaSpeciesB = 1.3;
|
||||
double molecularWeightSpeciesA = 29.0;
|
||||
double molecularWeightSpeciesB = 30.0;
|
||||
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
|
||||
#########################################################################
|
||||
|
|
@ -841,7 +1072,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
// ifvfd:
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
// SolverStructOrder: Spatial discretisation order of NS equations with struct grid.
|
||||
|
|
@ -856,7 +1087,7 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// -- "roe", "steger".
|
||||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
int isFVMOrFDM = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
|
|
@ -885,8 +1116,12 @@ int allReduceStep = 1;
|
|||
// codeOfOversetGrid: Overlapping(overset) grid or not.
|
||||
// 0 -- NON-overlapping grid.
|
||||
// 1 -- Overlapping grid.
|
||||
// oversetInterpolationMethod: the method of overset interpolation while field simulation
|
||||
// 0 -- set the acceptor cell value by donor cell value.
|
||||
// 1 -- set the acceptor cell value by distance weight of donor cell value.
|
||||
|
||||
int codeOfOversetGrid = 0;
|
||||
int codeOfOversetSlipGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
int symetryOrNot = 0;
|
||||
int readInAuxiliaryInnerGrid = 1;
|
||||
|
|
@ -895,7 +1130,7 @@ int readInSklFileOrNot = 0;
|
|||
string auxiliaryInnerGrid0 = "./grid/aux-upper.fts";
|
||||
string auxiliaryInnerGrid1 = "./grid/aux-lower.fts";
|
||||
string auxiliaryInnerGrid2 = "";
|
||||
string oversetGridFileName = "./grid/overlap.ovs";
|
||||
string oversetGridFileName = "./grid/iblank.ovs";
|
||||
double walldistMainZone = 1.0
|
||||
double toleranceForOversetSearch = 1.0e-3;
|
||||
double toleranceForOversetBox = 1.0e-3;
|
||||
|
|
@ -905,16 +1140,78 @@ int outTecplotOverset = 0;
|
|||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
int codeOfAleModel = 1;
|
||||
int aleStartStrategy = -1;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
|
||||
//0:1st-Admas-Bashforth; 1:2nd-Admas-Bashforth; 2:1st-Implicit-Euler; 3:2nd-Implicit Euler; 4:2nd-Adams-Moulton; 5:3rd-Adams-Moulton
|
||||
int methodForKineticEquation = 0;
|
||||
double relaxParameterOfKinetic = 1.0;
|
||||
|
||||
#########################################################################
|
||||
# motive information #
|
||||
#########################################################################
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
double massMatrix_0[] = 1e-7, 1e-6, 1e-6, 0.0, 0.0, 0.0;
|
||||
//initial six DOF position information of parts. xc yc zc
|
||||
double massCenter_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF position information of parts. angleX angleY angleZ
|
||||
double attitudeAngle_0[] = 0.0 , 0.0, 0.0;
|
||||
//initial six DOF move information of parts. vc vy vz
|
||||
double massCenterVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//initial six DOF move information of parts. omigX omigY omigZ
|
||||
double angularVelocity_0[] = 0.0, 0.0, 0.0;
|
||||
//the object that the parts belong to.
|
||||
int fartherIndex_0 = -1;
|
||||
//the assembly position of the parts. xc yc zc angleX angleY angleZ
|
||||
double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0 ,0.0;
|
||||
//the move pattern of the parts.
|
||||
// -1 given motion partten.
|
||||
// 0 still.
|
||||
// 1 six DOF motion.
|
||||
// 2 three DOF motion.
|
||||
// 11 X-axis forced motion.
|
||||
// 12 Y-axis forced motion.
|
||||
// 13 Z-axis forced motion.
|
||||
// 14 forced pitch motion.
|
||||
// 15 forced yaw motion.
|
||||
// 16 forced roll motion.
|
||||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
double addedForce_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
double addedMoment_0[] = 0.0 ,0.0 ,0.0 ;
|
||||
//the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 2.329418E08;
|
||||
//@double refDimensionalTemperature = 288.144;
|
||||
//@double refDimensionalPressure = 1.01313E05;
|
||||
//@double height = -0.001;
|
||||
//@double refReNumber = 6.5e6;
|
||||
//@double refDimensionalTemperature = 288.15;
|
||||
//@double freestream_vibration_temperature = 300.00;
|
||||
//@double refDimensionalPressure = 0;
|
||||
//@double height = 0;
|
||||
//@int nsubsonicInlet = 0;
|
||||
//@int nsubsonicOutlet = 0;
|
||||
//@string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
|
|
|
|||
|
|
@ -58,9 +58,9 @@ double refDimensionalTemperature = 80;
|
|||
|
||||
double gridScaleFactor = 0.01;
|
||||
|
||||
double forceRefenenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceRefenenceLength = 1.0; // unit of meter.
|
||||
double forceRefenenceArea = 1.0; // unit of meter^2.
|
||||
double forceReferenceLengthSpanWise = 1.0; // unit of meter.
|
||||
double forceReferenceLength = 1.0; // unit of meter.
|
||||
double forceReferenceArea = 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.
|
||||
|
|
|
|||
Loading…
Reference in New Issue