部分算例文件夹命名及参数更新
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@ -162,7 +162,7 @@ int flowInitStep = 100;
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// Please use 'rae2822_hybrid2d__4.fts' here!
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// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
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string gridfile = "./grid/CRM-HL_40-37__Level-B__1024.fts";
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string gridfile = "./grid/CRM-HL_40-37_Nominal_Unstr_LevelB_Q1__1024.fts";
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int plotFieldType = 0;
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// ----------------- Advanced Parameters, DO NOT care it ----------------
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@ -8,6 +8,7 @@
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// Platform for Hybrid Engineering Simulation of Flows +
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// China Aerodynamics Research and Development Center +
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// (C) Copyright, Since 2010 +
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// PHengLEI 2212 +
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//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
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###########################################################################
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# Default parameters for Grid conversion #
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@ -46,19 +47,24 @@ int gridobj = 1;
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int multiblock = 0;
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int iadapt = 0;
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int SymmetryFaceVector = 1;
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int gridReorder = 0;
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int faceReorderMethod = 0;
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// axisup: Type of Cartisien coordinates system, used in grid conversion.
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// 1 -- Y upward. (default)
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// 2 -- Z upward.
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int axisup = 1;
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// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating.
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// axisRotateOrder : axis rotating order.
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// 1 -- X-axis.
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// 2 -- Y-axis.
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// 3 -- Z-axis.
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// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order.
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int nAxisRotateTimes = 0;
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int axisRotateOrder[] = [1, 2, 3];
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double axisRotateAngles[] = [0.0, 0.0, 0.0];
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// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
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// 0 -- Interface. (default)
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// 1 -- Physical boundary condition, used in Hybrid solver.
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int omit_no_bound_bc = 0;
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int omitRepeatInterface = 1;
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//-----------------------------------------------------------------------
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# Grid data type #
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@ -89,7 +95,6 @@ int dumpOldGrid = 0;
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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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@ -178,7 +183,6 @@ double influencePara = 25.0;
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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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@ -192,7 +196,6 @@ double rotationAngle = 0.0;
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// 2 -- refine structured grid.
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// maxproc: The number of partition zones that want to be divided into.
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// numberOfMultifile: The number of partition grid files that want to be dumped out.
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int pgridtype = 0;
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int maxproc = 4;
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int numberOfMultifile = 1;
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@ -207,8 +210,8 @@ int blockIndexOfMark = 0;
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int cellIndexOfMark[] = [185, 30, 1];
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// parallelStrategy:
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//! -# 0 : each zone is assigned to the one that defined in grid partition procedure.
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//! -# 1 : random assigned for each zone or by some else ways.
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// 0 -- each zone is assigned to the one that defined in grid partition procedure.
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// 1 -- random assigned for each zone or by some else ways.
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int parallelStrategy = 1;
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//-----------------------------------------------------------------------
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@ -232,7 +235,6 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
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// 1 -- perfect balance.
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// maxproc -- perfect imbalance.
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// 1.05 -- recommended.
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int omit_no_bound_bc = 0;
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int npartmethod = 1;
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int parallelPartitionMethod = 2;
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@ -253,24 +255,30 @@ int numberOfMultigrid = 1;
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// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
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// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
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// intervalStepRes: The step intervals for residual file 'res.dat' saved.
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// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
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// 0 -- no precondition process. (default, mach > 0.3)
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// 1 -- carry out precondition process. (mach number <= 0.3)
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int maxSimuStep = 20000;
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int intervalStepFlow = 1000;
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int intervalStepPlot = 1000;
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int intervalStepSample = 1000;
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int intervalStepForce = 100;
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int intervalStepRes = 10;
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int ifLowSpeedPrecon = 0;
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// compressible:
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// 0 -- incompressible flow.
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// 1 -- compressible flow. (default)
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int compressible = 1;
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// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
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// 0 -- no precondition process. (default, mach > 0.3)
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// 1 -- carry out precondition process. (mach number <= 0.3)
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// Kprec: The coefficient K for the cut-off velocity.
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// 1.0~3.0 is suggested. (default, 3.0)
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// preconFarfieldBCMethod: The precondition method for farfield boundary condition.
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// 0 -- precondition far-field boundary based on riemann invariants.
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// 1 -- Turkel's simplified far-field boundary condition.
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int ifLowSpeedPrecon = 0;
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double Kprec = 3.0;
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int preconFarfieldBCMethod = 1;
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//-----------------------------------------------------------------------
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# CFD Control Parameter #
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//-----------------------------------------------------------------------
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@ -281,9 +289,12 @@ int compressible = 1;
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// 0 -- the nondimensional conditions.
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// 1 -- the flight conditions.
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// 2 -- the experiment conditions.
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// 3 -- the subsonic boundary conditions.
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// 3 -- the subsonic boundary conditions. (Useless!)
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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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//flowInitMethod: Flow field initialization method.
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// 0 -- The entire flow field is initialized according to Infinite velocity.
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// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
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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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@ -303,11 +314,11 @@ int compressible = 1;
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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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int directionMethod = 0;
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double refMachNumber = 0.73;
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double attackd = 2.79;
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double angleSlide = 0.00;
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int flowInitMethod = 0;
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int inflowParaType = 0;
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double refReNumber = 6.5e6;
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@ -321,14 +332,6 @@ double freestream_vibration_temperature = 300.00;
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//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
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//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
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//int inflowParaType = 3;
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//int nsubsonicInlet = 1;
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//int nsubsonicOutlet = 1;
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//string inLetFileName = "./bin/subsonicInlet.hypara";
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//string outLetFileName = "./bin/subsonicOutlet.hypara";
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//double refDimensionalTemperature = 288.144;
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//double refDimensionalPressure = 1.01313E05;
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// 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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@ -341,9 +344,15 @@ double freestream_vibration_temperature = 300.00;
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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 refDimensionalTemperature = 293.0;
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//double refDimensionalPressure = 8886.06;
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// The velocity, temperature and pressure are read from file.
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//int inflowParaType = 7;
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//string weatherDataFilePath = "./WRFData/";
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//double longitude = 110.95
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//double latitude = 19.61;
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double wallTemperature = -1.0;
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double radiationCoef = 0.8;
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@ -357,35 +366,35 @@ double forceReferenceArea = 1.0; // unit of meter^2.
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double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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double TorqueRefZ = 0.0; // unit of meter.
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double knudsenLength = 1.0; // unit of meter.
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double refMolecularWeight = 28.9644; // unit of g/mol.
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//-----------------------------------------------------------------------
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# Spatial Discretisation #
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//-----------------------------------------------------------------------
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#*******************************************************************
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#************************************************************************
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# Struct Solver *
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#*******************************************************************
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#************************************************************************
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// inviscidSchemeName: Spatial discretisation scheme of struct grid.
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// Using this when solve structered grid or hybrid.
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// -- "vanleer", "steger", "hlle", "lax_f".
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// -- "roe", "modified_roe".
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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", "ausmpw+".
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// isWennScheme: If using WENN Scheme of struct grid.
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// 0 -- NO. (default)
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// 1 -- Yes.
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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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// -- "vanalbada_clz", clz supersonic version.
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// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
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// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth",
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// -- "nolim", no limiter,
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// -- "vanalbada_clz", clz supersonic version,
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// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3".
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string inviscidSchemeName = "roe";
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int isWennScheme = 0;
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string str_limiter_name = "vanalbada";
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#*******************************************************************
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#************************************************************************
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# UnStruct Solver or Common *
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#*******************************************************************
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#************************************************************************
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// viscousType: Viscous model.
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// 0 -- Euler.
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// 1 -- Lamilar.
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@ -410,11 +419,11 @@ string str_limiter_name = "vanalbada";
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// 3 -- IDDES.
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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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// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
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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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// -- "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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@ -442,7 +451,7 @@ string str_limiter_name = "vanalbada";
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// 3 -- Harten type, which is default used.
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// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
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// It is used to scale the default Roe entropy fix coefficients.
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// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
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// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0.
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//int viscousType = 0;
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//string viscousName = "Euler";
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@ -475,9 +484,9 @@ double roeEntropyScale = 1.0;
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double AusmpwPlusLimiter = 1.0;
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//-----------------------------------------------------------------------
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# Temporal Discretisation #
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//-----------------------------------------------------------------------
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#************************************************************************
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# Temporal Discretisation *
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#************************************************************************
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// iunsteady: Steady or unsteady.
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// 0 -- steady.
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// 1 -- unsteay.
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@ -504,11 +513,18 @@ double AusmpwPlusLimiter = 1.0;
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// 6 -- Jacobian iteration.
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// 7 -- Line LU-SGS.
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// 8 -- Matrix LU-SGS.
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// 9 -- GMRES.
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// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
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// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
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// CFLStart: Started cfl number.
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// CFLEnd: End cfl number.
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// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
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// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
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// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
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// useLUSGSprecond: Initialize flow field for GMRES.
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// 0 --Initialize by first order Jacobian matrix.
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// 1 --Initialize by LUSGS.
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// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field.
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// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
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// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
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// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
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@ -533,7 +549,6 @@ double AusmpwPlusLimiter = 1.0;
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// 2 -- Pab3D wall function.
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// RKStage: The number of Runge-Kutta step.
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// lamda: Cofficient of Runge-Kutta step.
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int iunsteady = 0;
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double physicalTimeStep = 0.01;
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double physicalTimeStepDimensional = -0.001;
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@ -543,7 +558,7 @@ 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 linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2.
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int methodOfDualTime = 3;
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int min_sub_iter = 50;
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@ -558,7 +573,10 @@ int isUsePreTwall = 0;
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double CFLStart = 0.01;
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double CFLEnd = 10.0;
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int CFLVaryStep = 500;
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double GMRESCFLScale = 1.0;
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int OriginalTscheme = 9;
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int useLUSGSprecond = 1;
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int GMRESInitStep = 1000;
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double pMaxForCFL = 0.2;
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double pMinForCFL = 0.1;
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double deltaMaxForCFL = 0.2;
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@ -575,7 +593,7 @@ int order = 2;
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double visl_min = 0.01;
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double turbCFLScale = 1.0;
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double csrv = 2.0;
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double csrv = 1.0;
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double timemax = 1.0e10;
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double dtsave = -1.0;
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int maxale = 10;
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@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0];
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//int RKStage = 4;
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//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
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//-----------------------------------------------------------------------
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# File In or Out #
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//-----------------------------------------------------------------------
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#************************************************************************
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# File In or Out *
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#************************************************************************
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// numberOfGridGroups: The number of grid groups.
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// gridfile: The partitioned Grid file path, using relative path,
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// which is relative to the working directory.
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@ -618,10 +635,8 @@ double lamda[] = [0.5, 1.0];
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// nIsComputeWallDist: Whether to compute the wall distance.
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// 0 -- Compute wall distance.
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// 1 -- Not compute.
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//
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// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism.
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// wall_heatfluxfile: The file to output the MaxHeatFlux of wall.
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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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@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0;
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string resSaveFile = "results/res.dat";
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string turbresfile = "results/turbres.dat";
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string transitionResFile = "results/transitionRes.dat";
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string aircoeffile = "results/aircoef.dat";
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string restartNSFile = "results/flow.dat";
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string turbfile = "results/turb.dat";
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string transitionFile = "results/transition.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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@ -645,11 +662,15 @@ string protectionFile0 = "results/flow0.dat";
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string protectionFile1 = "results/flow1.dat";
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string wall_heatfluxfile = "results/wall_heatflux.dat";
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string protectionTurbFile0 = "results/turb0.dat";
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string protectionTurbFile1 = "results/turb1.dat";
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string protectionTransitionFile0 = "results/transition0.dat";
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string protectionTransitionFile1 = "results/transition1.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 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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@ -659,7 +680,8 @@ int plotFieldType = 0;
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// visualfileType: The file type of visualfile.
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// 0 -- Tecplot binary.
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// 1 -- Tecplot ASCII.
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// 2 -- Ensight binary.
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// 3 -- Ensight ASCII.
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int visualfileType = 1;
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// samplefileMode: The dump mode of sample file.
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|
|
@ -697,21 +719,21 @@ 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), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58),
|
||||
// -- overlap iblank(iblank, 81),
|
||||
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4),
|
||||
// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11),
|
||||
// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15),
|
||||
// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19),
|
||||
// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24).
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -739,7 +761,9 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9),
|
||||
// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -761,12 +785,13 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int nProbeVariables = 14;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
||||
#************************************************************************
|
||||
# Turbulence Parameter *
|
||||
#************************************************************************
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
|
|
@ -774,15 +799,12 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition.
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not.
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 3.0;
|
||||
double kwoo = 5.0;
|
||||
|
|
@ -791,28 +813,27 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
// maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# 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.
|
||||
// = 0 - in only first sub-iter;
|
||||
// != 0 - in every sub-iter.
|
||||
// = 0 -- in only first sub-iter;
|
||||
// != 0 -- in every sub-iter.
|
||||
// ipraddisturb: Add density and pressure disturb or not.
|
||||
// ibodyforce: Add body force in source flux of NS equations or not.
|
||||
// = 0 - not;
|
||||
// != 0 - Add body force.
|
||||
// = 0 -- not;
|
||||
// != 0 -- Add body force.
|
||||
// bodyforce: Body force in source flux of NS equations or not.
|
||||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
|
|
@ -820,23 +841,22 @@ int monitor_vistmax = 0;
|
|||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 - no wall function;
|
||||
// = 1 - van Driest;
|
||||
// = 2 - developed by Dr. Deng Xiaobing;
|
||||
// = 3 - developed by Piomelli.
|
||||
// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak);
|
||||
// = 2 -- pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 -- Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 -- no wall function;
|
||||
// = 1 -- van Driest;
|
||||
// = 2 -- developed by Dr. Deng Xiaobing;
|
||||
// = 3 -- developed by Piomelli.
|
||||
// turbViscousCutType: turbulent viscosity cut type.
|
||||
// = 0 - mu_total = mut + mul;
|
||||
// = 1 - mu_total = max(mut-mul,0)+ mul;
|
||||
// = 2 - mu_total = max(mut ,0)+ mul.
|
||||
// = 0 -- mu_total = mut + mul;
|
||||
// = 1 -- mu_total = max(mut-mul, 0) + mul;
|
||||
// = 2 -- mu_total = max(mut , 0) + mul.
|
||||
// smagConstant: constant of smagorinsky model.
|
||||
// waleConstant: constant of wale model.
|
||||
// filterDirection [3]: filter variables in i, j, k direction or not.
|
||||
// averageDirection[3]: average variables in i, j, k direction or not.
|
||||
// isotropicConstant: constant of isotropic part of SGS stress.
|
||||
|
||||
int iLES = 0;
|
||||
string sgsmodel = "smagorinsky";
|
||||
int deltaFunctionType = 2;
|
||||
|
|
@ -852,9 +872,9 @@ double testFilterScale = 2.0;
|
|||
int averageWidth = 1;
|
||||
int monitorNegativeConstant = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameters for Hypersonic Non-equilibrium Gas #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# Other Parameters for Hypersonic Non-equilibrium Gas *
|
||||
#************************************************************************
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
|
|
@ -862,9 +882,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -886,14 +903,13 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
|
|
@ -913,10 +929,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// isUseNoneqCond:
|
||||
// 0 -- compute the source terms without any conditions.
|
||||
// 1 -- compute the source terms using the non-equilibrium condition.
|
||||
// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
|
|
@ -946,14 +965,13 @@ int monitorNegativeConstant = 0;
|
|||
// 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].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// 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
|
||||
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.
|
||||
// veTemperatureMin: The minimum of Tv and Te.
|
||||
// maxViscous: the maximum of Viscous.
|
||||
// trTemperatureMin: the minimum value of trTemperature.
|
||||
// veTemperatureMin: the minimum value of veTemperature.
|
||||
|
|
@ -965,36 +983,34 @@ int monitorNegativeConstant = 0;
|
|||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction.
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// nChemcalSourceModified: Modified on ChemcalSource.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource.
|
||||
// 0 -- approximation algorithm 1 (Ori).
|
||||
// 1 -- approximation algorithm 2 (New).
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nDiagonalModified: Modified on Diagonal.
|
||||
// 0 -- not used.
|
||||
// 1 -- new.
|
||||
// nDiagonalModifiedTurb: Modified on Diagonal for turbulence.
|
||||
// 0 -- not used.
|
||||
// 1 -- new.
|
||||
// nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// 1 -- new.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -1017,8 +1033,8 @@ int monitorNegativeConstant = 0;
|
|||
// "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 gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// for struct solver mixing two species<65><73>SpeciesA, SpeciesB<73><42>.
|
||||
// for unstruct solver mixing multi-species<65><73>O2 NO CO CO2 H2 N2 Air CH4<48><34>.
|
||||
// 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.
|
||||
|
|
@ -1040,13 +1056,16 @@ int monitorNegativeConstant = 0;
|
|||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData: Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// nTvChange: Judge whether the Tv equals Ttr.
|
||||
// 0 -- yes.
|
||||
// 1 -- no.
|
||||
// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions.
|
||||
// nFraction: the initial fractions type of species.
|
||||
// 0 -- mass fraction.
|
||||
// 1 -- mole fraction.
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
|
|
@ -1114,6 +1133,7 @@ double densityMin = 1.0e-8;
|
|||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
int iniSpeedMode = 0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
|
|
@ -1125,18 +1145,21 @@ int nChemcalSourceEsMethod = 1;
|
|||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nDiagonalModifiedTurb = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 0;
|
||||
int nTvChange = 0;
|
||||
int isMoleFractionType = 0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
|
|
@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0;
|
|||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
||||
int nLeakageMonitor = 0;
|
||||
double totalLeakageVolume = 1000.0;
|
||||
double monitorThresholdValue = 0.05;
|
||||
double sprayFactor = 0.0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
|
|
@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0;
|
|||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
|
|
@ -1226,9 +1256,9 @@ string holeFullFileName = "./grid/holeFullFile.dat";
|
|||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
#************************************************************************
|
||||
# High Order Struct Solver *
|
||||
#************************************************************************
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
|
|
@ -1273,10 +1303,29 @@ 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
|
||||
// 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.
|
||||
|
||||
// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in
|
||||
// the current overset grid(only for three dimension).
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// walldistMainZone: The initial value of background grid which does not exist wall boundary condition.
|
||||
// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell.
|
||||
// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region.
|
||||
// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary.
|
||||
// 0 -- one layer.
|
||||
// 1 -- two layers.
|
||||
// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region.
|
||||
// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
int codeOfOversetGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
|
|
@ -1295,7 +1344,6 @@ int twoOrderInterpolationOrNot = 0;
|
|||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
|
|
@ -1306,34 +1354,40 @@ double referenceLength = 1.0;
|
|||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
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
|
||||
// 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 #
|
||||
#########################################################################
|
||||
#************************************************************************
|
||||
# motive information *
|
||||
#************************************************************************
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
// mass of parts.
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
// gravity of parts (along negative direction in Y-axis, eg. 9.8).
|
||||
double gravity_0 = 0.0;
|
||||
// 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
|
||||
// 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
|
||||
// if reset mass center while restart.
|
||||
int resetMassCenter_0 = 0;
|
||||
// position offset of parts. dx dy dz.
|
||||
double massCenterDxyz_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
|
||||
// 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
|
||||
// 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
|
||||
// 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.
|
||||
|
|
@ -1349,23 +1403,24 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// direction of rotation.
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
// dimensional physical time for additional force(s).
|
||||
double addedForceTime_0[] = 0.0;
|
||||
// additional force(inertia system) fX fY fZ.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
double addedMoment_0[] = 0.0, 0.0, 0.0;
|
||||
// the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
// post indentify.
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
@ -1379,18 +1434,34 @@ int integralOrder = 4;
|
|||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
#########################################################################
|
||||
//@string weatherDataFilePath = "./WRFData/";
|
||||
//@double longitude = 110.95
|
||||
//@double latitude = 19.61;
|
||||
#************************************************************************
|
||||
# Old Parameter *
|
||||
#************************************************************************
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
#************************************************************************
|
||||
# partial flow field setting Parameter *
|
||||
#************************************************************************
|
||||
//int nPartialParameter = 0; // 0/1/2
|
||||
//int nNumberOfPartialField = 0; //
|
||||
//int nStartGridIndex[] = [0];
|
||||
//int nEndGridIndex[] = [0];
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
//double partialCFL[] = [0.0];
|
||||
//double partialSpeedCoef[] = [0.0];
|
||||
//double partialSpeed[] = [0.0];
|
||||
//double partialAttackd[] = [0.0];
|
||||
//double partialSlide[] = [0.0];
|
||||
//double partialPressure[] = [0.0];
|
||||
//double partialTemperature[] = [0.0];
|
||||
//double partialMassFractions[] = [0.0];
|
||||
|
||||
#************************************************************************
|
||||
# Incompressible Parameter *
|
||||
#************************************************************************
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -8,6 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2212 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -46,19 +47,24 @@ int gridobj = 1;
|
|||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating.
|
||||
// axisRotateOrder : axis rotating order.
|
||||
// 1 -- X-axis.
|
||||
// 2 -- Y-axis.
|
||||
// 3 -- Z-axis.
|
||||
// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order.
|
||||
int nAxisRotateTimes = 0;
|
||||
int axisRotateOrder[] = [1, 2, 3];
|
||||
double axisRotateAngles[] = [0.0, 0.0, 0.0];
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
int omitRepeatInterface = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
|
|
@ -89,7 +95,6 @@ int dumpOldGrid = 0;
|
|||
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 ------------------------------
|
||||
|
|
@ -178,7 +183,6 @@ double influencePara = 25.0;
|
|||
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;
|
||||
|
|
@ -192,7 +196,6 @@ double rotationAngle = 0.0;
|
|||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
|
@ -207,8 +210,8 @@ int blockIndexOfMark = 0;
|
|||
int cellIndexOfMark[] = [185, 30, 1];
|
||||
|
||||
// parallelStrategy:
|
||||
//! -# 0 : each zone is assigned to the one that defined in grid partition procedure.
|
||||
//! -# 1 : random assigned for each zone or by some else ways.
|
||||
// 0 -- each zone is assigned to the one that defined in grid partition procedure.
|
||||
// 1 -- random assigned for each zone or by some else ways.
|
||||
int parallelStrategy = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -232,7 +235,6 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
|
|
@ -253,24 +255,30 @@ int numberOfMultigrid = 1;
|
|||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
// Kprec: The coefficient K for the cut-off velocity.
|
||||
// 1.0~3.0 is suggested. (default, 3.0)
|
||||
// preconFarfieldBCMethod: The precondition method for farfield boundary condition.
|
||||
// 0 -- precondition far-field boundary based on riemann invariants.
|
||||
// 1 -- Turkel's simplified far-field boundary condition.
|
||||
int ifLowSpeedPrecon = 0;
|
||||
double Kprec = 3.0;
|
||||
int preconFarfieldBCMethod = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -281,9 +289,12 @@ int compressible = 1;
|
|||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 3 -- the subsonic boundary conditions. (Useless!)
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
//flowInitMethod: Flow field initialization method.
|
||||
// 0 -- The entire flow field is initialized according to Infinite velocity.
|
||||
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
|
||||
// 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.
|
||||
|
|
@ -303,11 +314,11 @@ int compressible = 1;
|
|||
// 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.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
int flowInitMethod = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
|
|
@ -321,14 +332,6 @@ double freestream_vibration_temperature = 300.00;
|
|||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
// The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
|
|
@ -341,9 +344,15 @@ double freestream_vibration_temperature = 300.00;
|
|||
|
||||
// The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalTemperature = 293.0;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
// The velocity, temperature and pressure are read from file.
|
||||
//int inflowParaType = 7;
|
||||
//string weatherDataFilePath = "./WRFData/";
|
||||
//double longitude = 110.95
|
||||
//double latitude = 19.61;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
|
|
@ -357,35 +366,35 @@ 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 knudsenLength = 1.0; // unit of meter.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "vanleer", "steger", "hlle", "lax_f",
|
||||
// -- "roe", "modified_roe",
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth",
|
||||
// -- "nolim", no limiter,
|
||||
// -- "vanalbada_clz", clz supersonic version,
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3".
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
|
|
@ -410,11 +419,11 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "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".
|
||||
|
|
@ -442,7 +451,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -475,9 +484,9 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# Temporal Discretisation *
|
||||
#************************************************************************
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
|
|
@ -504,11 +513,18 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// 9 -- GMRES.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
|
||||
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
|
||||
// useLUSGSprecond: Initialize flow field for GMRES.
|
||||
// 0 --Initialize by first order Jacobian matrix.
|
||||
// 1 --Initialize by LUSGS.
|
||||
// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -533,7 +549,6 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
|
|
@ -543,7 +558,7 @@ int ifStaticsReynoldsStress = 0;
|
|||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2.
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
int min_sub_iter = 50;
|
||||
|
|
@ -558,7 +573,10 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 9;
|
||||
int useLUSGSprecond = 1;
|
||||
int GMRESInitStep = 1000;
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -575,7 +593,7 @@ int order = 2;
|
|||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
double csrv = 2.0;
|
||||
double csrv = 1.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int maxale = 10;
|
||||
|
|
@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0];
|
|||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# File In or Out *
|
||||
#************************************************************************
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
|
|
@ -618,10 +635,8 @@ double lamda[] = [0.5, 1.0];
|
|||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile: The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile = "";
|
||||
|
|
@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0;
|
|||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string transitionResFile = "results/transitionRes.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
string transitionFile = "results/transition.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
|
@ -645,11 +662,15 @@ string protectionFile0 = "results/flow0.dat";
|
|||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
string protectionTurbFile0 = "results/turb0.dat";
|
||||
string protectionTurbFile1 = "results/turb1.dat";
|
||||
|
||||
string protectionTransitionFile0 = "results/transition0.dat";
|
||||
string protectionTransitionFile1 = "results/transition1.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
|
@ -659,7 +680,8 @@ int plotFieldType = 0;
|
|||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
|
|
@ -697,21 +719,21 @@ 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), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58),
|
||||
// -- overlap iblank(iblank, 81),
|
||||
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4),
|
||||
// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11),
|
||||
// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15),
|
||||
// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19),
|
||||
// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24).
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -739,7 +761,9 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9),
|
||||
// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -761,12 +785,13 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int nProbeVariables = 14;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
||||
#************************************************************************
|
||||
# Turbulence Parameter *
|
||||
#************************************************************************
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
|
|
@ -774,15 +799,12 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition.
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not.
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 3.0;
|
||||
double kwoo = 5.0;
|
||||
|
|
@ -791,28 +813,27 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
// maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# 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.
|
||||
// = 0 - in only first sub-iter;
|
||||
// != 0 - in every sub-iter.
|
||||
// = 0 -- in only first sub-iter;
|
||||
// != 0 -- in every sub-iter.
|
||||
// ipraddisturb: Add density and pressure disturb or not.
|
||||
// ibodyforce: Add body force in source flux of NS equations or not.
|
||||
// = 0 - not;
|
||||
// != 0 - Add body force.
|
||||
// = 0 -- not;
|
||||
// != 0 -- Add body force.
|
||||
// bodyforce: Body force in source flux of NS equations or not.
|
||||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
|
|
@ -820,23 +841,22 @@ int monitor_vistmax = 0;
|
|||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 - no wall function;
|
||||
// = 1 - van Driest;
|
||||
// = 2 - developed by Dr. Deng Xiaobing;
|
||||
// = 3 - developed by Piomelli.
|
||||
// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak);
|
||||
// = 2 -- pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 -- Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 -- no wall function;
|
||||
// = 1 -- van Driest;
|
||||
// = 2 -- developed by Dr. Deng Xiaobing;
|
||||
// = 3 -- developed by Piomelli.
|
||||
// turbViscousCutType: turbulent viscosity cut type.
|
||||
// = 0 - mu_total = mut + mul;
|
||||
// = 1 - mu_total = max(mut-mul,0)+ mul;
|
||||
// = 2 - mu_total = max(mut ,0)+ mul.
|
||||
// = 0 -- mu_total = mut + mul;
|
||||
// = 1 -- mu_total = max(mut-mul, 0) + mul;
|
||||
// = 2 -- mu_total = max(mut , 0) + mul.
|
||||
// smagConstant: constant of smagorinsky model.
|
||||
// waleConstant: constant of wale model.
|
||||
// filterDirection [3]: filter variables in i, j, k direction or not.
|
||||
// averageDirection[3]: average variables in i, j, k direction or not.
|
||||
// isotropicConstant: constant of isotropic part of SGS stress.
|
||||
|
||||
int iLES = 0;
|
||||
string sgsmodel = "smagorinsky";
|
||||
int deltaFunctionType = 2;
|
||||
|
|
@ -852,9 +872,9 @@ double testFilterScale = 2.0;
|
|||
int averageWidth = 1;
|
||||
int monitorNegativeConstant = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameters for Hypersonic Non-equilibrium Gas #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# Other Parameters for Hypersonic Non-equilibrium Gas *
|
||||
#************************************************************************
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
|
|
@ -862,9 +882,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -886,14 +903,13 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
|
|
@ -913,10 +929,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// isUseNoneqCond:
|
||||
// 0 -- compute the source terms without any conditions.
|
||||
// 1 -- compute the source terms using the non-equilibrium condition.
|
||||
// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
|
|
@ -946,14 +965,13 @@ int monitorNegativeConstant = 0;
|
|||
// 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].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// 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
|
||||
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.
|
||||
// veTemperatureMin: The minimum of Tv and Te.
|
||||
// maxViscous: the maximum of Viscous.
|
||||
// trTemperatureMin: the minimum value of trTemperature.
|
||||
// veTemperatureMin: the minimum value of veTemperature.
|
||||
|
|
@ -965,36 +983,34 @@ int monitorNegativeConstant = 0;
|
|||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction.
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// nChemcalSourceModified: Modified on ChemcalSource.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource.
|
||||
// 0 -- approximation algorithm 1 (Ori).
|
||||
// 1 -- approximation algorithm 2 (New).
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nDiagonalModified: Modified on Diagonal.
|
||||
// 0 -- not used.
|
||||
// 1 -- new.
|
||||
// nDiagonalModifiedTurb: Modified on Diagonal for turbulence.
|
||||
// 0 -- not used.
|
||||
// 1 -- new.
|
||||
// nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// 1 -- new.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -1017,8 +1033,8 @@ int monitorNegativeConstant = 0;
|
|||
// "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 gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// for struct solver mixing two species<65><73>SpeciesA, SpeciesB<73><42>.
|
||||
// for unstruct solver mixing multi-species<65><73>O2 NO CO CO2 H2 N2 Air CH4<48><34>.
|
||||
// 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.
|
||||
|
|
@ -1040,13 +1056,16 @@ int monitorNegativeConstant = 0;
|
|||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData: Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// nTvChange: Judge whether the Tv equals Ttr.
|
||||
// 0 -- yes.
|
||||
// 1 -- no.
|
||||
// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions.
|
||||
// nFraction: the initial fractions type of species.
|
||||
// 0 -- mass fraction.
|
||||
// 1 -- mole fraction.
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
|
|
@ -1114,6 +1133,7 @@ double densityMin = 1.0e-8;
|
|||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
int iniSpeedMode = 0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
|
|
@ -1125,18 +1145,21 @@ int nChemcalSourceEsMethod = 1;
|
|||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nDiagonalModifiedTurb = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 0;
|
||||
int nTvChange = 0;
|
||||
int isMoleFractionType = 0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
|
|
@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0;
|
|||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
||||
int nLeakageMonitor = 0;
|
||||
double totalLeakageVolume = 1000.0;
|
||||
double monitorThresholdValue = 0.05;
|
||||
double sprayFactor = 0.0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
|
|
@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0;
|
|||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
|
|
@ -1226,9 +1256,9 @@ string holeFullFileName = "./grid/holeFullFile.dat";
|
|||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
#************************************************************************
|
||||
# High Order Struct Solver *
|
||||
#************************************************************************
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
|
|
@ -1273,10 +1303,29 @@ 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
|
||||
// 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.
|
||||
|
||||
// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in
|
||||
// the current overset grid(only for three dimension).
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// walldistMainZone: The initial value of background grid which does not exist wall boundary condition.
|
||||
// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell.
|
||||
// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region.
|
||||
// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary.
|
||||
// 0 -- one layer.
|
||||
// 1 -- two layers.
|
||||
// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region.
|
||||
// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
int codeOfOversetGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
|
|
@ -1295,7 +1344,6 @@ int twoOrderInterpolationOrNot = 0;
|
|||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
|
|
@ -1306,34 +1354,40 @@ double referenceLength = 1.0;
|
|||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
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
|
||||
// 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 #
|
||||
#########################################################################
|
||||
#************************************************************************
|
||||
# motive information *
|
||||
#************************************************************************
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
// mass of parts.
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
// gravity of parts (along negative direction in Y-axis, eg. 9.8).
|
||||
double gravity_0 = 0.0;
|
||||
// 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
|
||||
// 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
|
||||
// if reset mass center while restart.
|
||||
int resetMassCenter_0 = 0;
|
||||
// position offset of parts. dx dy dz.
|
||||
double massCenterDxyz_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
|
||||
// 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
|
||||
// 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
|
||||
// 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.
|
||||
|
|
@ -1349,23 +1403,24 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// direction of rotation.
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
// dimensional physical time for additional force(s).
|
||||
double addedForceTime_0[] = 0.0;
|
||||
// additional force(inertia system) fX fY fZ.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
double addedMoment_0[] = 0.0, 0.0, 0.0;
|
||||
// the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
// post indentify.
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
@ -1379,18 +1434,34 @@ int integralOrder = 4;
|
|||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
#########################################################################
|
||||
//@string weatherDataFilePath = "./WRFData/";
|
||||
//@double longitude = 110.95
|
||||
//@double latitude = 19.61;
|
||||
#************************************************************************
|
||||
# Old Parameter *
|
||||
#************************************************************************
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
#************************************************************************
|
||||
# partial flow field setting Parameter *
|
||||
#************************************************************************
|
||||
//int nPartialParameter = 0; // 0/1/2
|
||||
//int nNumberOfPartialField = 0; //
|
||||
//int nStartGridIndex[] = [0];
|
||||
//int nEndGridIndex[] = [0];
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
//double partialCFL[] = [0.0];
|
||||
//double partialSpeedCoef[] = [0.0];
|
||||
//double partialSpeed[] = [0.0];
|
||||
//double partialAttackd[] = [0.0];
|
||||
//double partialSlide[] = [0.0];
|
||||
//double partialPressure[] = [0.0];
|
||||
//double partialTemperature[] = [0.0];
|
||||
//double partialMassFractions[] = [0.0];
|
||||
|
||||
#************************************************************************
|
||||
# Incompressible Parameter *
|
||||
#************************************************************************
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -8,6 +8,7 @@
|
|||
// Platform for Hybrid Engineering Simulation of Flows +
|
||||
// China Aerodynamics Research and Development Center +
|
||||
// (C) Copyright, Since 2010 +
|
||||
// PHengLEI 2212 +
|
||||
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
|
||||
###########################################################################
|
||||
# Default parameters for Grid conversion #
|
||||
|
|
@ -46,19 +47,24 @@ int gridobj = 1;
|
|||
int multiblock = 0;
|
||||
int iadapt = 0;
|
||||
int SymmetryFaceVector = 1;
|
||||
|
||||
int gridReorder = 0;
|
||||
int faceReorderMethod = 0;
|
||||
|
||||
// axisup: Type of Cartisien coordinates system, used in grid conversion.
|
||||
// 1 -- Y upward. (default)
|
||||
// 2 -- Z upward.
|
||||
int axisup = 1;
|
||||
// nAxisRotateTimes: number of axis rotating times, zero (default) meaning without rotating.
|
||||
// axisRotateOrder : axis rotating order.
|
||||
// 1 -- X-axis.
|
||||
// 2 -- Y-axis.
|
||||
// 3 -- Z-axis.
|
||||
// axisRotateAngles: axis rotating angles (degree), which are corresponding to the axis rotating order.
|
||||
int nAxisRotateTimes = 0;
|
||||
int axisRotateOrder[] = [1, 2, 3];
|
||||
double axisRotateAngles[] = [0.0, 0.0, 0.0];
|
||||
|
||||
// omit_no_bound_bc: What's boundary condition for the type of "no_boundary_condition".
|
||||
// 0 -- Interface. (default)
|
||||
// 1 -- Physical boundary condition, used in Hybrid solver.
|
||||
int omit_no_bound_bc = 0;
|
||||
int omitRepeatInterface = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Grid data type #
|
||||
|
|
@ -89,7 +95,6 @@ int dumpOldGrid = 0;
|
|||
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 ------------------------------
|
||||
|
|
@ -178,7 +183,6 @@ double influencePara = 25.0;
|
|||
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;
|
||||
|
|
@ -192,7 +196,6 @@ double rotationAngle = 0.0;
|
|||
// 2 -- refine structured grid.
|
||||
// maxproc: The number of partition zones that want to be divided into.
|
||||
// numberOfMultifile: The number of partition grid files that want to be dumped out.
|
||||
|
||||
int pgridtype = 0;
|
||||
int maxproc = 4;
|
||||
int numberOfMultifile = 1;
|
||||
|
|
@ -207,8 +210,8 @@ int blockIndexOfMark = 0;
|
|||
int cellIndexOfMark[] = [185, 30, 1];
|
||||
|
||||
// parallelStrategy:
|
||||
//! -# 0 : each zone is assigned to the one that defined in grid partition procedure.
|
||||
//! -# 1 : random assigned for each zone or by some else ways.
|
||||
// 0 -- each zone is assigned to the one that defined in grid partition procedure.
|
||||
// 1 -- random assigned for each zone or by some else ways.
|
||||
int parallelStrategy = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -232,7 +235,6 @@ string partition_grid_file = "./grid/sphere_mixed__4.fts";
|
|||
// 1 -- perfect balance.
|
||||
// maxproc -- perfect imbalance.
|
||||
// 1.05 -- recommended.
|
||||
|
||||
int omit_no_bound_bc = 0;
|
||||
int npartmethod = 1;
|
||||
int parallelPartitionMethod = 2;
|
||||
|
|
@ -253,24 +255,30 @@ int numberOfMultigrid = 1;
|
|||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
|
||||
int maxSimuStep = 20000;
|
||||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
||||
// compressible:
|
||||
// 0 -- incompressible flow.
|
||||
// 1 -- compressible flow. (default)
|
||||
int compressible = 1;
|
||||
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
// 0 -- no precondition process. (default, mach > 0.3)
|
||||
// 1 -- carry out precondition process. (mach number <= 0.3)
|
||||
// Kprec: The coefficient K for the cut-off velocity.
|
||||
// 1.0~3.0 is suggested. (default, 3.0)
|
||||
// preconFarfieldBCMethod: The precondition method for farfield boundary condition.
|
||||
// 0 -- precondition far-field boundary based on riemann invariants.
|
||||
// 1 -- Turkel's simplified far-field boundary condition.
|
||||
int ifLowSpeedPrecon = 0;
|
||||
double Kprec = 3.0;
|
||||
int preconFarfieldBCMethod = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# CFD Control Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -281,9 +289,12 @@ int compressible = 1;
|
|||
// 0 -- the nondimensional conditions.
|
||||
// 1 -- the flight conditions.
|
||||
// 2 -- the experiment conditions.
|
||||
// 3 -- the subsonic boundary conditions.
|
||||
// 3 -- the subsonic boundary conditions. (Useless!)
|
||||
// 4 -- the condition that the velocity, temperature and density are given.
|
||||
// 5 -- the condition that the velocity, temperature and pressure are given.
|
||||
//flowInitMethod: Flow field initialization method.
|
||||
// 0 -- The entire flow field is initialized according to Infinite velocity.
|
||||
// 1 -- The velocity near the wall is initialized according to the boundary layer of the plate.
|
||||
// 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.
|
||||
|
|
@ -303,11 +314,11 @@ int compressible = 1;
|
|||
// 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.
|
||||
|
||||
int directionMethod = 0;
|
||||
double refMachNumber = 0.73;
|
||||
double attackd = 2.79;
|
||||
double angleSlide = 0.00;
|
||||
int flowInitMethod = 0;
|
||||
|
||||
int inflowParaType = 0;
|
||||
double refReNumber = 6.5e6;
|
||||
|
|
@ -321,14 +332,6 @@ double freestream_vibration_temperature = 300.00;
|
|||
//double refDimensionalTemperature = 6051.024; // The total temperature, T*(1+(refGama-1)*M*M/2).
|
||||
//double refDimensionalPressure = 4.299696E09; // The total pressure, p*(T0/T)^(refGama/(refGama-1)).
|
||||
|
||||
//int inflowParaType = 3;
|
||||
//int nsubsonicInlet = 1;
|
||||
//int nsubsonicOutlet = 1;
|
||||
//string inLetFileName = "./bin/subsonicInlet.hypara";
|
||||
//string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//double refDimensionalTemperature = 288.144;
|
||||
//double refDimensionalPressure = 1.01313E05;
|
||||
|
||||
// The velocity, temperature and density are fixed.
|
||||
//int inflowParaType = 4;
|
||||
//double refDimensionalVelocity = 1000.0;
|
||||
|
|
@ -341,9 +344,15 @@ double freestream_vibration_temperature = 300.00;
|
|||
|
||||
// The MachNumber, temperature and pressure are fixed.
|
||||
//int inflowParaType = 6;
|
||||
//double refDimensionalTemperature = 293;
|
||||
//double refDimensionalTemperature = 293.0;
|
||||
//double refDimensionalPressure = 8886.06;
|
||||
|
||||
// The velocity, temperature and pressure are read from file.
|
||||
//int inflowParaType = 7;
|
||||
//string weatherDataFilePath = "./WRFData/";
|
||||
//double longitude = 110.95
|
||||
//double latitude = 19.61;
|
||||
|
||||
double wallTemperature = -1.0;
|
||||
|
||||
double radiationCoef = 0.8;
|
||||
|
|
@ -357,35 +366,35 @@ 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 knudsenLength = 1.0; // unit of meter.
|
||||
double refMolecularWeight = 28.9644; // unit of g/mol.
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
# Struct Solver *
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
// inviscidSchemeName: Spatial discretisation scheme of struct grid.
|
||||
// Using this when solve structered grid or hybrid.
|
||||
// -- "vanleer", "steger", "hlle", "lax_f".
|
||||
// -- "roe", "modified_roe".
|
||||
// -- "vanleer", "steger", "hlle", "lax_f",
|
||||
// -- "roe", "modified_roe",
|
||||
// -- "ausm+", "ausm+w", "ausm+up", "ausmdv", "ausmpw", "ausmpw+".
|
||||
// isWennScheme: If using WENN Scheme of struct grid.
|
||||
// 0 -- NO. (default)
|
||||
// 1 -- Yes.
|
||||
// str_limiter_name: Limiter of struct grid.
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth".
|
||||
// -- "nolim", no limiter.
|
||||
// -- "vanalbada_clz", clz supersonic version.
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3"
|
||||
|
||||
// -- "vanalbada", "vanleer", "minmod", "smooth", "minvan", "3rdsmooth", "3rd_minmod_smooth",
|
||||
// -- "nolim", no limiter,
|
||||
// -- "vanalbada_clz", clz supersonic version,
|
||||
// -- "weno3_js", "wenn3_prm211", "wenn3_zm", "wenn3_zes2", "wenn3_zes3".
|
||||
string inviscidSchemeName = "roe";
|
||||
int isWennScheme = 0;
|
||||
string str_limiter_name = "vanalbada";
|
||||
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
#************************************************************************
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
|
|
@ -410,11 +419,11 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- IDDES.
|
||||
// uns_scheme_name: Spatial discretisation scheme of Unstruct grid.
|
||||
// Using this when solve Unstructered grid or hybrid.
|
||||
// -- "vanleer", "roe", "steger", "kfvs", "lax_f", "hlle".
|
||||
// -- "vanleer", "roe", "GMRESRoe", "GMRESSteger", "steger", "kfvs", "lax_f", "hlle",
|
||||
// -- "ausm+", "ausmdv", "ausm+w", "ausmpw", "ausmpw+".
|
||||
// uns_limiter_name: Limiter of Unstruct grid.
|
||||
// -- "barth", "vencat", "vanleer", "minmod".
|
||||
// -- "vanalbada", "smooth", "nnd", "lpz", "1st".
|
||||
// -- "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".
|
||||
|
|
@ -442,7 +451,7 @@ string str_limiter_name = "vanalbada";
|
|||
// 3 -- Harten type, which is default used.
|
||||
// roeEntropyScale: Entropy fix (correction) coefficient scale, default is 1.0.
|
||||
// It is used to scale the default Roe entropy fix coefficients.
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0
|
||||
// AusmpwPlusLimiter: A Limiter to make "function w" not change acutely in AusmpwPlus scheme, default is 1.0.
|
||||
|
||||
//int viscousType = 0;
|
||||
//string viscousName = "Euler";
|
||||
|
|
@ -475,9 +484,9 @@ double roeEntropyScale = 1.0;
|
|||
|
||||
double AusmpwPlusLimiter = 1.0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Temporal Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# Temporal Discretisation *
|
||||
#************************************************************************
|
||||
// iunsteady: Steady or unsteady.
|
||||
// 0 -- steady.
|
||||
// 1 -- unsteay.
|
||||
|
|
@ -504,11 +513,18 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 6 -- Jacobian iteration.
|
||||
// 7 -- Line LU-SGS.
|
||||
// 8 -- Matrix LU-SGS.
|
||||
// 9 -- GMRES.
|
||||
// iSimplifyViscousTerm: Simplify the computation of viscous term in the Block LU-SGS method. The default value assigns 1 that could speed up the computation.
|
||||
// Otherwise, the viscous Jacobian matrix Mv should be computed that will increase the memory and time in iteration of the BLUSGS method.
|
||||
// CFLStart: Started cfl number.
|
||||
// CFLEnd: End cfl number.
|
||||
// CFLVaryStep: The number of step when cfl increase from CFLStart to CFLEnd.
|
||||
// GMRESCFLScale : CFL = CFLStart * GMRESCFLScal^iteration.
|
||||
// OriginalTscheme : Used for LUSGS and GMres hybrid computing.
|
||||
// useLUSGSprecond: Initialize flow field for GMRES.
|
||||
// 0 --Initialize by first order Jacobian matrix.
|
||||
// 1 --Initialize by LUSGS.
|
||||
// GMRESInitStep : the number of iteration step of irst order Jacobian matrix or LUSGS for initialize flow field.
|
||||
// ktmax: Dtratio. dt[i] = MIN(dt[i], ktmax * dtmin / vol[i])
|
||||
// swapDq: Communication dq between forward/backward sweep of LUSGS or not, default is 0.
|
||||
// nLUSGSSweeps: Sub iteration of LU-SGS or Block LU-SGS.
|
||||
|
|
@ -533,7 +549,6 @@ double AusmpwPlusLimiter = 1.0;
|
|||
// 2 -- Pab3D wall function.
|
||||
// RKStage: The number of Runge-Kutta step.
|
||||
// lamda: Cofficient of Runge-Kutta step.
|
||||
|
||||
int iunsteady = 0;
|
||||
double physicalTimeStep = 0.01;
|
||||
double physicalTimeStepDimensional = -0.001;
|
||||
|
|
@ -543,7 +558,7 @@ int ifStaticsReynoldsStress = 0;
|
|||
int startStatisticStep = 800000;
|
||||
double statisticalTimePeriod = -1.0;
|
||||
int statisticMethod = 0;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2;
|
||||
int linearTwoStepMethods = 1; // 1--BDF1; 2--C-N; 3--BDF2.
|
||||
|
||||
int methodOfDualTime = 3;
|
||||
int min_sub_iter = 50;
|
||||
|
|
@ -558,7 +573,10 @@ int isUsePreTwall = 0;
|
|||
double CFLStart = 0.01;
|
||||
double CFLEnd = 10.0;
|
||||
int CFLVaryStep = 500;
|
||||
|
||||
double GMRESCFLScale = 1.0;
|
||||
int OriginalTscheme = 9;
|
||||
int useLUSGSprecond = 1;
|
||||
int GMRESInitStep = 1000;
|
||||
double pMaxForCFL = 0.2;
|
||||
double pMinForCFL = 0.1;
|
||||
double deltaMaxForCFL = 0.2;
|
||||
|
|
@ -575,7 +593,7 @@ int order = 2;
|
|||
|
||||
double visl_min = 0.01;
|
||||
double turbCFLScale = 1.0;
|
||||
double csrv = 2.0;
|
||||
double csrv = 1.0;
|
||||
double timemax = 1.0e10;
|
||||
double dtsave = -1.0;
|
||||
int maxale = 10;
|
||||
|
|
@ -591,10 +609,9 @@ double lamda[] = [0.5, 1.0];
|
|||
|
||||
//int RKStage = 4;
|
||||
//double lamda[] = [0.25, 0.33333333333, 0.5, 1.0];
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# File In or Out #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# File In or Out *
|
||||
#************************************************************************
|
||||
// numberOfGridGroups: The number of grid groups.
|
||||
// gridfile: The partitioned Grid file path, using relative path,
|
||||
// which is relative to the working directory.
|
||||
|
|
@ -618,10 +635,8 @@ double lamda[] = [0.5, 1.0];
|
|||
// nIsComputeWallDist: Whether to compute the wall distance.
|
||||
// 0 -- Compute wall distance.
|
||||
// 1 -- Not compute.
|
||||
//
|
||||
// protectionFile0 and protectionFile1: Two continuation file of the data protection mechanism.
|
||||
// wall_heatfluxfile: The file to output the MaxHeatFlux of wall.
|
||||
|
||||
int numberOfGridGroups = 1;
|
||||
string gridfile = "./grid/rae2822_hybrid2d__4.fts";
|
||||
string wallTemperaturefile = "";
|
||||
|
|
@ -632,10 +647,12 @@ int cellMethodOrNodeMethod = 0;
|
|||
|
||||
string resSaveFile = "results/res.dat";
|
||||
string turbresfile = "results/turbres.dat";
|
||||
string transitionResFile = "results/transitionRes.dat";
|
||||
string aircoeffile = "results/aircoef.dat";
|
||||
|
||||
string restartNSFile = "results/flow.dat";
|
||||
string turbfile = "results/turb.dat";
|
||||
string transitionFile = "results/transition.dat";
|
||||
|
||||
string visualfile = "results/tecflow.plt";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
|
@ -645,11 +662,15 @@ string protectionFile0 = "results/flow0.dat";
|
|||
string protectionFile1 = "results/flow1.dat";
|
||||
string wall_heatfluxfile = "results/wall_heatflux.dat";
|
||||
|
||||
string protectionTurbFile0 = "results/turb0.dat";
|
||||
string protectionTurbFile1 = "results/turb1.dat";
|
||||
|
||||
string protectionTransitionFile0 = "results/transition0.dat";
|
||||
string protectionTransitionFile1 = "results/transition1.dat";
|
||||
|
||||
int nDumpSurfaceInfo = 0;
|
||||
string wall_varfile = "";
|
||||
|
||||
string jetDefineFile = "bin/jet.hypara";
|
||||
|
||||
string sixDofFileName = "results/sixDofInfo.dat";
|
||||
string derivativeFileName = "results/identify.dat";
|
||||
string hysteresisFileName = "results/force_beta.plt";
|
||||
|
|
@ -659,7 +680,8 @@ int plotFieldType = 0;
|
|||
// visualfileType: The file type of visualfile.
|
||||
// 0 -- Tecplot binary.
|
||||
// 1 -- Tecplot ASCII.
|
||||
|
||||
// 2 -- Ensight binary.
|
||||
// 3 -- Ensight ASCII.
|
||||
int visualfileType = 1;
|
||||
|
||||
// samplefileMode: The dump mode of sample file.
|
||||
|
|
@ -697,21 +719,21 @@ 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), streamline_u(45), streamline_v(46), streamline_w(47),
|
||||
// -- transition intermittency(intermittency, 51), -transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- overlap iblank(iblank, 81)
|
||||
|
||||
// -- specific heat ratio(gama, 56)
|
||||
// -- transition intermittency(intermittency, 51), transition momentum thickness reynolds(MomentumThicknessReynolds, 52),
|
||||
// -- local CFL Number(localCFL, 57), minimal CFL Number(minCFL, 58),
|
||||
// -- overlap iblank(iblank, 81),
|
||||
// -- specific heat ratio(gama, 56), Knudsen number(kn, 60), Damkohler number(Da, 61), vibrational nonequilibrium number(Vi, 62).
|
||||
// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
|
||||
// Variables order must from small to big.
|
||||
//-----------the optional parameters list for the wall boundary condition----------------
|
||||
// nVisualWallVariables: The number of visual variables on wall.
|
||||
// visualWallVariables : dumped variable types, listed as following:
|
||||
// -coefficient of pressure(cp, 0), -coefficient of friction(cf, 1), yplus(2), -non-dimensional heat flux(Q_NonDim, 3), -dimensional heat flux(Q_Dim, 4),
|
||||
// -pressure on wall(pw, 5), -temperature on wall(Tw, 6), -density on wall(rhow, 7), -heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -heat flux of species diffusion term(Qs, 9), -heat flux of vibrational temperature term(Qv, 10), -heat flux of electron temperature term(Qe, 11),
|
||||
// -species mass fractions(Ns, 12), -x component of wall velocity(Vx, 13), -y component of wall velocity(Vy, 14), -z component of wall velocity(Vz, 15)
|
||||
// -slip translational-rotational temperature(Tts, 16), -slip vibrational temperature(Tvs, 17), -slip electron temperature(Tes, 18), -absolute wall velocity(Vs, 19)
|
||||
// -Stanton number(St, 20), -coefficient of heat rate(Ch, 21), -temperature jump(deltaT, 22), -Grid Reynolds number on wall(Re_w, 23)
|
||||
// -- coefficient of pressure(cp, 0), coefficient of friction(cf, 1), yplus(2), non-dimensional heat flux(Q_NonDim, 3), dimensional heat flux(Q_Dim, 4),
|
||||
// -- pressure on wall(pw, 5), temperature on wall(Tw, 6), density on wall(rhow, 7), heat flux of translational-rotational temperature term(Qtr, 8),
|
||||
// -- heat flux of species diffusion term(Qs, 9), heat flux of vibrational temperature term(Qv, 10), heat flux of electron temperature term(Qe, 11),
|
||||
// -- species mass fractions(Ns, 12), x component of wall velocity(Vx, 13), y component of wall velocity(Vy, 14), z component of wall velocity(Vz, 15),
|
||||
// -- slip translational-rotational temperature(Tts, 16), slip vibrational temperature(Tvs, 17), slip electron temperature(Tes, 18), absolute wall velocity(Vs, 19),
|
||||
// -- Stanton number(St, 20), coefficient of heat rate(Ch, 21), temperature jump(deltaT, 22), Grid Reynolds number on wall(Re_w, 23), Knudsen number(Kn_wall, 24).
|
||||
int nVisualVariables = 8;
|
||||
int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
||||
|
||||
|
|
@ -739,7 +761,9 @@ int dumpStandardModel = 0;
|
|||
// 1 -- Real cell where the probe is located.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6).
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
|
||||
// -- dimensioanl_density(7), dimensioanl_u(8), dimensioanl_v(9),
|
||||
// -- dimensioanl_w(10), dimensioanl_pressure(11), dimensioanl_temperature(12).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
// probeVariablesInterpolationMethod: Interpolation method used to compute the probe variables.
|
||||
|
|
@ -761,12 +785,13 @@ string probesDefineFile = "bin/probes_XYZ.dat";
|
|||
|
||||
int searchCellsMethod = 0;
|
||||
|
||||
int nProbeVariables = 7;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6];
|
||||
int nProbeVariables = 14;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13];
|
||||
int probeVariablesInterpolationMethod = 0;
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
||||
#************************************************************************
|
||||
# Turbulence Parameter *
|
||||
#************************************************************************
|
||||
// turbInterval: Iteration number of turbulence.
|
||||
// kindOfTurbSource: Kinds of turbulent source.
|
||||
// 0 -- Original.
|
||||
|
|
@ -774,15 +799,12 @@ int probeVariablesInterpolationMethod = 0;
|
|||
// transitionType: transition model type
|
||||
// 0 -- none.
|
||||
// 2 -- gama-re-theta.
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not
|
||||
|
||||
|
||||
// turbIntensity: (valid while greater than 0.0 ) turbulent intensity of free stream(*100) in transition.
|
||||
// freeturbIntensitySRModify: to use SR modify in free stream turbulent intensity decay or not.
|
||||
int turbInterval = 1;
|
||||
int turbOrderStruct = 2;
|
||||
int kindOfTurbSource = 0;
|
||||
int mod_turb_res = 0;
|
||||
double turb_relax = 1.0;
|
||||
double freeStreamViscosity = 1.0e-3;
|
||||
double muoo = 3.0;
|
||||
double kwoo = 5.0;
|
||||
|
|
@ -791,28 +813,27 @@ double turbIntensity = -1.0;
|
|||
int freeturbIntensitySRModify = 0;
|
||||
double freeDecayXLocation = 0.0;
|
||||
int compressibleCorrection = 0;
|
||||
int prandtlNumberCorrection = 0;
|
||||
int transitionMaFix = 1;
|
||||
|
||||
# maximum eddy viscosity (myt/my) max.
|
||||
// maximum eddy viscosity (myt/my) max.
|
||||
double eddyViscosityLimit = 1.0e10;
|
||||
int monitor_vistmax = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# LES Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# 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.
|
||||
// = 0 - in only first sub-iter;
|
||||
// != 0 - in every sub-iter.
|
||||
// = 0 -- in only first sub-iter;
|
||||
// != 0 -- in every sub-iter.
|
||||
// ipraddisturb: Add density and pressure disturb or not.
|
||||
// ibodyforce: Add body force in source flux of NS equations or not.
|
||||
// = 0 - not;
|
||||
// != 0 - Add body force.
|
||||
// = 0 -- not;
|
||||
// != 0 -- Add body force.
|
||||
// bodyforce: Body force in source flux of NS equations or not.
|
||||
// utau: friction velocity, using in DNSDisturb.
|
||||
// sgsmodel: subgrid scale model.
|
||||
|
|
@ -820,23 +841,22 @@ int monitor_vistmax = 0;
|
|||
// = "dsmCom";
|
||||
// = "wale";
|
||||
// = "sigma".
|
||||
// deltaFunctionType: = 1 - MAX(deltai, deltaj, deltak);
|
||||
// = 2 - pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 - Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 - no wall function;
|
||||
// = 1 - van Driest;
|
||||
// = 2 - developed by Dr. Deng Xiaobing;
|
||||
// = 3 - developed by Piomelli.
|
||||
// deltaFunctionType: = 1 -- MAX(deltai, deltaj, deltak);
|
||||
// = 2 -- pow(deltai * deltaj *deltak, 1/3);
|
||||
// = 3 -- Devloped by Scotti.
|
||||
// wallDampingFunctionType: = 0 -- no wall function;
|
||||
// = 1 -- van Driest;
|
||||
// = 2 -- developed by Dr. Deng Xiaobing;
|
||||
// = 3 -- developed by Piomelli.
|
||||
// turbViscousCutType: turbulent viscosity cut type.
|
||||
// = 0 - mu_total = mut + mul;
|
||||
// = 1 - mu_total = max(mut-mul,0)+ mul;
|
||||
// = 2 - mu_total = max(mut ,0)+ mul.
|
||||
// = 0 -- mu_total = mut + mul;
|
||||
// = 1 -- mu_total = max(mut-mul, 0) + mul;
|
||||
// = 2 -- mu_total = max(mut , 0) + mul.
|
||||
// smagConstant: constant of smagorinsky model.
|
||||
// waleConstant: constant of wale model.
|
||||
// filterDirection [3]: filter variables in i, j, k direction or not.
|
||||
// averageDirection[3]: average variables in i, j, k direction or not.
|
||||
// isotropicConstant: constant of isotropic part of SGS stress.
|
||||
|
||||
int iLES = 0;
|
||||
string sgsmodel = "smagorinsky";
|
||||
int deltaFunctionType = 2;
|
||||
|
|
@ -852,9 +872,9 @@ double testFilterScale = 2.0;
|
|||
int averageWidth = 1;
|
||||
int monitorNegativeConstant = 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameters for Hypersonic Non-equilibrium Gas #
|
||||
//-----------------------------------------------------------------------
|
||||
#************************************************************************
|
||||
# Other Parameters for Hypersonic Non-equilibrium Gas *
|
||||
#************************************************************************
|
||||
// dg_high_order:
|
||||
// 0 -- generic order accuracy.
|
||||
// 1 -- high order accuracy.
|
||||
|
|
@ -862,9 +882,6 @@ int monitorNegativeConstant = 0;
|
|||
// 0 -- gas model is fixed in the codes.
|
||||
// 1 -- gas model is imported from library files.
|
||||
// isAdaptiveSolver: isAdaptiveSolver = 0 indicates the generic Navier-Stokes solver,
|
||||
// isAdaptiveSolver>0 indicates the HyFlow self-adaptive solver.
|
||||
// 1 -- using HyFlow self-adaptive solver where the switch is controlled by the total iteration steps.
|
||||
// 2 -- using HyFlow self-adaptive solver where the switch is controlled by variation of the key residual.
|
||||
// nm: Equation number of the physics, but is out of commision now.
|
||||
// 4 -- for 2D.
|
||||
// 5 -- for 3D.
|
||||
|
|
@ -886,14 +903,13 @@ int monitorNegativeConstant = 0;
|
|||
// 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.
|
||||
// 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.
|
||||
|
|
@ -913,10 +929,13 @@ int monitorNegativeConstant = 0;
|
|||
// 1 -- One-temperature model.
|
||||
// 2 -- Two-temperature model.
|
||||
// 3 -- Three-temperature model.
|
||||
// isUseNoneqCond:
|
||||
// 0 -- compute the source terms without any conditions.
|
||||
// 1 -- compute the source terms using the non-equilibrium condition.
|
||||
// frozenCondition: the threshold value of frozen chemical flow condition, 0.1 is the default value.
|
||||
// nIdealState: whether take all gas species as ideal gas for gas-mixture process.
|
||||
// 0 -- No.
|
||||
// 1 -- Yes.
|
||||
// nTEnergyModel: the method to computing temperature energy model.
|
||||
// 1 -- Yes. // nTEnergyModel: the method to computing temperature energy model.
|
||||
// 0 -- the energy term is computed using the conventional method.
|
||||
// 1 -- the energy term is computed using the polynomial fitting method.
|
||||
// 2 -- the energy term is computed using the piecewise polynomial fitting method.
|
||||
|
|
@ -946,14 +965,13 @@ int monitorNegativeConstant = 0;
|
|||
// 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].
|
||||
// spectrumRadiusCoef: The value is in range of [0.0, 2.0].
|
||||
// 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
|
||||
|
||||
// 1 -- freezes the chemical reactions, the chemical reaction sources will not be calculated.
|
||||
// veTemperatureMin: The minimum of Tv and Te.
|
||||
// maxViscous: the maximum of Viscous.
|
||||
// trTemperatureMin: the minimum value of trTemperature.
|
||||
// veTemperatureMin: the minimum value of veTemperature.
|
||||
|
|
@ -965,36 +983,34 @@ int monitorNegativeConstant = 0;
|
|||
// nSpeciesLimit: limitter of gas species
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction
|
||||
// nTurblenceForChemical: the coupled mode of Turblence and Chemical reaction.
|
||||
// 0 -- method 0.
|
||||
// 1 -- method 1.
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid
|
||||
// nViscosityFluxSublevelModified: Modified for ViscosityFlux on Sublevel grid.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef
|
||||
// nViscosityPeModified: Pe Modified for ViscosityCoef.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceModified: Modified on ChemcalSource
|
||||
// nChemcalSourceModified: Modified on ChemcalSource.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource
|
||||
// 0 -- approximation algorithm 1 (Ori.)
|
||||
// 1 -- approximation algorithm 2 (New)
|
||||
|
||||
// nChemcalSourceEsMethod: Modified on ChemcalSource.
|
||||
// 0 -- approximation algorithm 1 (Ori).
|
||||
// 1 -- approximation algorithm 2 (New).
|
||||
// nMaxStepTemperature: the iterative steps of temperature.
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs
|
||||
// 0 -- not used
|
||||
// 1 -- used
|
||||
|
||||
// nDiagonalModified: Modified on Diagonal
|
||||
// 0 -- not used
|
||||
// 1 -- Ori.
|
||||
// 2 -- new
|
||||
|
||||
// veTemperatureMinModified: Modified on the minimum of Tve for Cvvs.
|
||||
// 0 -- not used.
|
||||
// 1 -- used.
|
||||
// nDiagonalModified: Modified on Diagonal.
|
||||
// 0 -- not used.
|
||||
// 1 -- new.
|
||||
// nDiagonalModifiedTurb: Modified on Diagonal for turbulence.
|
||||
// 0 -- not used.
|
||||
// 1 -- new.
|
||||
// nGradPrimtiveMethod:
|
||||
// 0 -- Ori.
|
||||
// 1 -- new
|
||||
// 1 -- new.
|
||||
// nAblation:
|
||||
// 0 -- The wall ablation is not computed.
|
||||
// 1 -- The wall ablation is computed.
|
||||
|
|
@ -1017,8 +1033,8 @@ int monitorNegativeConstant = 0;
|
|||
// "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 gas without reacting.
|
||||
// for struct solver mixing two species£¨SpeciesA, SpeciesB£©.
|
||||
// for unstruct solver mixing multi-species£¨O2 NO CO CO2 H2 N2 Air CH4£©.
|
||||
// for struct solver mixing two species<65><73>SpeciesA, SpeciesB<73><42>.
|
||||
// for unstruct solver mixing multi-species<65><73>O2 NO CO CO2 H2 N2 Air CH4<48><34>.
|
||||
// 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.
|
||||
|
|
@ -1040,13 +1056,16 @@ int monitorNegativeConstant = 0;
|
|||
// firstStepError : the residual error of the first step iteration for the self-adaptive calculation.
|
||||
// secondStepError : the residual error of the second step iteration for the self-adaptive calculation.
|
||||
// thirdStepError : the residual error of the third step iteration for the self-adaptive calculation.
|
||||
// useHyflowSetting : Setting for HyFLOW GUI.
|
||||
// 0 -- PHengLEI
|
||||
// 1 -- HyFLOW
|
||||
// nProtectData: Use the continuation file data protection mechanism.
|
||||
// 0 -- no
|
||||
// 1 -- yes
|
||||
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// nTvChange: Judge whether the Tv equals Ttr.
|
||||
// 0 -- yes.
|
||||
// 1 -- no.
|
||||
// isMoleFractionType: 1 indicates the mass fractions, or else the mole fractions.
|
||||
// nFraction: the initial fractions type of species.
|
||||
// 0 -- mass fraction.
|
||||
// 1 -- mole fraction.
|
||||
int dg_high_order = 0;
|
||||
int iapplication = 0;
|
||||
int isAdaptiveSolver = 0;
|
||||
|
|
@ -1114,6 +1133,7 @@ double densityMin = 1.0e-8;
|
|||
double densityMinFactor = 0.1;
|
||||
double tAdjustmentFactor = 10.0;
|
||||
double iniSpeedCoef = 1.0;
|
||||
int iniSpeedMode = 0;
|
||||
|
||||
int nDebug = 0;
|
||||
int nSpeciesLimit = 1;
|
||||
|
|
@ -1125,18 +1145,21 @@ int nChemcalSourceEsMethod = 1;
|
|||
int nMaxStepTemperature = 5;
|
||||
int veTemperatureMinModified = 1;
|
||||
int nDiagonalModified = 0;
|
||||
int nDiagonalModifiedTurb = 0;
|
||||
int nGradPrimtiveMethod = 1;
|
||||
int nInviscidFluxModify = 1;
|
||||
int nQlLimitMethod = 2;
|
||||
int nSpeciesForWallMethod = 1;
|
||||
int nDensityForWallMethod = 0;
|
||||
int wallMultiTemperature = 0;
|
||||
|
||||
int nProtectData = 0;
|
||||
int useHyflowSetting = 0;
|
||||
int nAblation = 0;
|
||||
int isInjection = 0;
|
||||
int nViscosityModel = 0;
|
||||
int nMarsModel = 0;
|
||||
int nTvChange = 0;
|
||||
int isMoleFractionType = 0;
|
||||
string gasfile = "DK5";
|
||||
//string gasfile = "./chemical/Dunn-Kang_air5s11r.dat";
|
||||
string speciesName = "O, O2, NO, N, N2";
|
||||
|
|
@ -1173,9 +1196,17 @@ double molecularWeightSpeciesB = 30.0;
|
|||
//string speciesName = "O2, N2";
|
||||
//string initMassFraction = "1.0, 0.0";
|
||||
|
||||
int nFraction = 0;
|
||||
int nContinueModel = 0;
|
||||
int nChemicalFlowStep = 0;
|
||||
int ifStartFromPerfectGasResults = 0;
|
||||
int isUseNoneqCond = 0;
|
||||
double frozenCondition = 0.01;
|
||||
|
||||
int nLeakageMonitor = 0;
|
||||
double totalLeakageVolume = 1000.0;
|
||||
double monitorThresholdValue = 0.05;
|
||||
double sprayFactor = 0.0;
|
||||
|
||||
#########################################################################
|
||||
// Multi-Grid parameters.
|
||||
|
|
@ -1196,7 +1227,6 @@ int ifStartFromPerfectGasResults = 0;
|
|||
// 1 -- zero order.
|
||||
// 2 -- first-order. (default)
|
||||
// mgCorrectionLimit: Multi-grid correction limit.
|
||||
|
||||
int nMGLevel = 1;
|
||||
int MGCoarsestIteration = 1;
|
||||
int MGPreIteration = 1;
|
||||
|
|
@ -1226,9 +1256,9 @@ string holeFullFileName = "./grid/holeFullFile.dat";
|
|||
string linkFileName = "./grid/topology.dat";
|
||||
string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
||||
|
||||
#########################################################################
|
||||
# High Order Struct Solver #
|
||||
#########################################################################
|
||||
#************************************************************************
|
||||
# High Order Struct Solver *
|
||||
#************************************************************************
|
||||
// isFVMOrFDM:
|
||||
// 0 -- NSSolverStruct using Finite Volume Method.
|
||||
// 1 -- NSSolverStruct using Finite Differ Method.
|
||||
|
|
@ -1273,10 +1303,29 @@ 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
|
||||
// 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.
|
||||
|
||||
// readOversetFileOrNo: Whether to read overset-file(.ovs) that has been generated.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// symetryOrNot: If there exist symetryplanes(XY plane, the coordinate of Z direction is 0) in
|
||||
// the current overset grid(only for three dimension).
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// readInAuxiliaryInnerGrid: Whether to read auxiliary inner grid.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
// walldistMainZone: The initial value of background grid which does not exist wall boundary condition.
|
||||
// toleranceForOversetSearch: The tolerance of overset searching zone to judge whether the obtained node is in the current computing cell.
|
||||
// toleranceForOversetBox: The tolerance of building the minimum box of computing cells in the overlapping region.
|
||||
// twoOrderInterpolationOrNot: The number of interpolated cell layers in the overlapping boundary.
|
||||
// 0 -- one layer.
|
||||
// 1 -- two layers.
|
||||
// keyEnlargeOfActiveNodes: The number of enlarged overset-boundary layers in the buffer region.
|
||||
// outTecplotOverset: Whether to dump out the flowfield data after the progress of overset configure.
|
||||
// 0 -- no.
|
||||
// 1 -- yes.
|
||||
int codeOfOversetGrid = 0;
|
||||
int oversetInterpolationMethod = 0;
|
||||
int readOversetFileOrNot = 0;
|
||||
|
|
@ -1295,7 +1344,6 @@ int twoOrderInterpolationOrNot = 0;
|
|||
int keyEnlargeOfActiveNodes = 0;
|
||||
int outTecplotOverset = 0;
|
||||
int outPutOversetVisualization = 0;
|
||||
|
||||
int numberOfMovingBodies = 2;
|
||||
|
||||
// ----------------- ALE configuration ------------------------------
|
||||
|
|
@ -1306,34 +1354,40 @@ double referenceLength = 1.0;
|
|||
double referenceVelocity = 1.0;
|
||||
double referenceDensity = 1.0;
|
||||
|
||||
int strategyForFaceNormalVelocity = 0; //0-By Sweeping volume; 1-By face center 1st; 2-By face center 2nd;
|
||||
int strategyForGCLSource = 0; //0-present; 1-Ahn;
|
||||
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
|
||||
// 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 #
|
||||
#########################################################################
|
||||
#************************************************************************
|
||||
# motive information *
|
||||
#************************************************************************
|
||||
int numberOfMovingBodies = 1;
|
||||
|
||||
############################## body0 ##############################
|
||||
//mass of parts
|
||||
// mass of parts.
|
||||
double mass_0 = 1.0;
|
||||
//mass matrix of parts Ixx Iyy Izz Ixy Ixz Iyz
|
||||
// gravity of parts (along negative direction in Y-axis, eg. 9.8).
|
||||
double gravity_0 = 0.0;
|
||||
// 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
|
||||
// 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
|
||||
// if reset mass center while restart.
|
||||
int resetMassCenter_0 = 0;
|
||||
// position offset of parts. dx dy dz.
|
||||
double massCenterDxyz_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
|
||||
// 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
|
||||
// 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
|
||||
// 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.
|
||||
|
|
@ -1349,23 +1403,24 @@ double configPamameter_0[] = 0.0 ,0.0 ,0.0 ,0.0 ,0.0
|
|||
int RBDMethod_0 = 0;
|
||||
double amplitude_0 = 0.0;
|
||||
double reduceFrequency_0 = 0.0;
|
||||
//direction of rotation
|
||||
// direction of rotation.
|
||||
// 1 -- clockwise from the point of view along the positive x axis.
|
||||
// -1 -- anticlockwise from the point of view along the positive x axis.
|
||||
int direction_0 = -1;
|
||||
double rotateFrequency_0 = 0.0;
|
||||
//string uDFSixDofFileName_0 = "./Bin/UDFSixDof.Parameter";
|
||||
//additional force (system axis) fX fY fZ
|
||||
// dimensional physical time for additional force(s).
|
||||
double addedForceTime_0[] = 0.0;
|
||||
// additional force(inertia system) fX fY fZ.
|
||||
double addedForce_0[] = 0.0, 0.0, 0.0;
|
||||
//additional moment of Force (system axis) mX mY mZ
|
||||
// additional moment(inertia system) mX mY mZ.
|
||||
double addedMoment_0[] = 0.0, 0.0, 0.0;
|
||||
// the deformation method of the parts.
|
||||
int morphing_0 = 0;
|
||||
|
||||
// post indentify
|
||||
// post indentify.
|
||||
int integralOrder = 4;
|
||||
|
||||
|
||||
// ---------------- ATP read --------------------------------------------
|
||||
//@int inflowParaType = 0;
|
||||
//@double refReNumber = 6.5e6;
|
||||
|
|
@ -1379,18 +1434,34 @@ int integralOrder = 4;
|
|||
//@string outLetFileName = "./bin/subsonicOutlet.hypara";
|
||||
//@double refDimensionalVelocity = 0;
|
||||
//@double refDimensionalDensity = 0;
|
||||
|
||||
#########################################################################
|
||||
# Old Parameter #
|
||||
#########################################################################
|
||||
//@string weatherDataFilePath = "./WRFData/";
|
||||
//@double longitude = 110.95
|
||||
//@double latitude = 19.61;
|
||||
#************************************************************************
|
||||
# Old Parameter *
|
||||
#************************************************************************
|
||||
int isPlotVolumeField = 0;
|
||||
|
||||
#************************************************************************
|
||||
# partial flow field setting Parameter *
|
||||
#************************************************************************
|
||||
//int nPartialParameter = 0; // 0/1/2
|
||||
//int nNumberOfPartialField = 0; //
|
||||
//int nStartGridIndex[] = [0];
|
||||
//int nEndGridIndex[] = [0];
|
||||
|
||||
#########################################################################
|
||||
# Incompressible Parameter #
|
||||
#########################################################################
|
||||
//double partialCFL[] = [0.0];
|
||||
//double partialSpeedCoef[] = [0.0];
|
||||
//double partialSpeed[] = [0.0];
|
||||
//double partialAttackd[] = [0.0];
|
||||
//double partialSlide[] = [0.0];
|
||||
//double partialPressure[] = [0.0];
|
||||
//double partialTemperature[] = [0.0];
|
||||
//double partialMassFractions[] = [0.0];
|
||||
|
||||
#************************************************************************
|
||||
# Incompressible Parameter *
|
||||
#************************************************************************
|
||||
int isSolveEnergyEquation = 0;
|
||||
int isSolveTurbEquation = 0;
|
||||
int isSolveSpeciesEquation = 0;
|
||||
|
||||
|
|
|
|||
|
|
@ -190,7 +190,7 @@ int flowInitStep = 100;
|
|||
// Please use 'rae2822_hybrid2d__4.fts' here!
|
||||
// plotFieldType: If dump out the whole field results to tecplot or not, 0 / 1.
|
||||
|
||||
string gridfile = "../grid/multi-species.fts";
|
||||
string gridfile = "./grid/multi-species.fts";
|
||||
int plotFieldType = 0;
|
||||
|
||||
// ----------------- Advanced Parameters, DO NOT care it ----------------
|
||||
|
|
|
|||
|
|
@ -0,0 +1,5 @@
|
|||
红山开源风雷算例库原始网格获取百度网盘链接：
|
||||
链接：http://pan.baidu.com/s/1aZ9cdkp6CkT9il4fEpnTcA
|
||||
提取码：w47m
|
||||
|
||||
注：plot3D格式网格需同时下载.grd和.inp文件
|
||||
31
README.md
31
README.md
|
|
@ -49,6 +49,9 @@ A 结构
|
|||
| 二维结构30p30n翼型低速绕流(熵修正) | A27_TwoD_30p30n_SA_Entropyfix6_Struct_4CPU |
|
||||
| 二维结构圆柱超声速绕流(熵修正) | A28_TwoD_Cylinder_Inv_Ma3d0_Entropyfix6_Struct_1CPU |
|
||||
| 二维结构Rae2822翼型跨声速绕流(熵修正) | A29_TwoD_Rae2822_SA_Entropyfix6_Struct_4CPU |
|
||||
| 二维结构圆柱高超声速绕流(熵修正) | A30_TwoD_Cylinder_Inv_Ma10d0_Entropyfix6_Struct_1CPU |
|
||||
| 三维结构CHNT跨声速流动(Matrix LUSGS) | A31_ThreeD_CHNT_SST_MatrixLUSGS_Struct_256CPU |
|
||||
| 二维结构NACA0012翼型低速绕流（低速预处理） | A32_TwoD_NACA0012_Inv_Ma0d2_Precondition_Struct_1CPU |
|
||||
|
||||
B 非结构
|
||||
|
||||
|
|
@ -71,7 +74,10 @@ B 非结构
|
|||
| 二维非结构NLR7301翼型低速绕流 | B15_TwoD_NLR7301_SA_Unstruct_4CPU |
|
||||
| 三维非结构空心圆柱裙 | B16_ThreeD_Hollow_Cylinder_Flare_Laminar_Unstruct_16CPU |
|
||||
| 二维非结构S-K低速平板转捩模拟 | B17_TwoD_Plate_S-KSR_SST_Unstruct_4CPU |
|
||||
| 三维非结构CRM-HL高升力外形模拟 | B18-ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU |
|
||||
| 三维非结构CRM-HL高升力外形模拟 | B18_ThreeD_CRM-HL_Level-B_SA_Unstruct_1024CPU |
|
||||
| 三维非结构TrapWing外形模拟 | B19_ThreeD_TrapWing_SA_AoA13_256CPU |
|
||||
| 二维非结构NACA0012低速绕流（Gmresh） | B20_TwoD_NACA0012_SA_Gmresh_Unstruct_1CPU |
|
||||
| 三维非结构球头高速绕流（Gmresh） | B21_ThreeD_Sphere_Laminar_Gmresh_Unstruct_1CPU |
|
||||
|
||||
C 混合
|
||||
|
||||
|
|
@ -104,7 +110,7 @@ F 重叠网格、动网格
|
|||
|
||||
| 中文 | 英文 |
|
||||
| :------------------------- | :--------------------------------- |
|
||||
| 三维结构30p30n重叠网格装配 | F01_ThreeD_30p30n_OversetGrid_SA_Struct_4CPU |
|
||||
| 二维结构30p30n重叠网格装配 | F01_TwoD_30p30n_OversetGrid_SA_Struct_4CPU |
|
||||
| 三维结构多弹体重叠网格装配 | F02_ThreeD_duodan_OversetGrid_SA_Struct_8CPU |
|
||||
| 二维非结构双0012重叠网格装配 | F03_TwoD_Dual0012_OversetConfig_Unstruct_4CPU |
|
||||
| 二维非结构双0012重叠网格计算 | F04_TwoD_Dual0012_OversetGrid_InvisCal_Unstruct_4CPU |
|
||||
|
|
@ -127,16 +133,25 @@ G 非平衡
|
|||
| 二维非结构高速圆柱两气体组分预混 | G05_TwoD_Cylinder_N2-O2_Premixing-Unstruct_1CPU |
|
||||
| 三维非结构高速球头两气体组分预混 | G06_ThreeD_Sphere_N2-O2_Premixing-Unstruct_1CPU |
|
||||
| 二维非结构管道喷流两气体组分预混 | G07_TwoD_Pipe_Air-CH4_Mixing-Unstruct_1CPU |
|
||||
| 二维储气罐泄漏非定常模拟 | G08_TwoD_TankLeak_NG_Multispecies_Unstruct_Unsteady_4CPU |
|
||||
|
||||
H 不可压
|
||||
|
||||
| 中文 | 英文 |
|
||||
| :----------------------------------- | :-------------------------------------------------------- |
|
||||
| 二维非结构不可压层流后台阶流动 | H01_PBSolver_TwoD_Backstep_Laminar_Re95_Unstruct_1CPU |
|
||||
| 二维非结构不可压层流方腔自然对流 | H02_PBSolver_TwoD_Cavity_Boussinesq_Laminar_Unstruct_1CPU |
|
||||
| 二维非结构不可压层流方腔流动 | H03_PBSolver_TwoD_Cavity_Laminar_Re1000_Unstruct_1CPU |
|
||||
| 三维非结构不可压圆管湍流压降模拟 | H04_PBSolver_ThreeD_Pipe_Turb_Unstruct_1CPU |
|
||||
| 三维非结构不可压AFF-1 半艇外流场模拟 | H05_PBSolver_ThreeD_Suboff_Laminar_Re225_1CPU |
|
||||
| :---------------------------------- | :--------------------------------------- |
|
||||
| 二维后台阶流动 | H01_TwoD_BackStep_KE_QUICK_4CPU |
|
||||
| 二维方腔驱动流 | H02_TwoD_Cavitity_Re100_SUDS_4CPU |
|
||||
| 二维两组分混合气体模拟 | H03_TwoD_GasLeakage_Steady_QUICK_4CPU |
|
||||
| NACA0012翼型低速绕流PISO方法模拟 | H04_TwoD_NACA0012_PISO_SA_4CPU |
|
||||
| NACA0012翼型高速流动SIMPLEC方法模拟 | H05_TwoD_NACA0012_SIMPLEC_4CPU |
|
||||
| 二维自然对流模拟 | H06_TwoD_NaturalConvection_CDS_4CPU |
|
||||
| 二维湍流平板模拟 | H07_TwoD_Plate_Turb_QUICK_4CPU |
|
||||
| 二维湍流多组分混合气体模拟 | H08_TwoD_Species_Turb_QUICK_4CPU |
|
||||
| 三维小车湍流模拟 | H09_ThreeD_Car_Turb_QUICK_4CPU |
|
||||
| 三维CHNT模型层流模拟 | H10_ThreeD_Chnt_Lam_UPWIND_4CPU |
|
||||
| 三维多组分泄漏非定常流动模拟 | H11_ThreeD_GasLeakage_Unsteady_SUDS_4CPU |
|
||||
| 三维多组分扩散非定常流动模拟 | H12_ThreeD_Species_Transient_QUICK_4CPU |
|
||||
| 三维半艇绕流模拟 | H13_ThreeD_SUBOFF_UPWIND_4CPU |
|
||||
|
||||
X 用户分享算例
|
||||
|
||||
|
|
|
|||
Loading…
Reference in New Issue