forked from PHengLEI/PHengLEI-TestCases
"v7407"
This commit is contained in:
hechao
parent
7f8e0990db
commit
7774cb2a9a
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@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
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double influenceRadius = 20;
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int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
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// ----------------- Periodic Parameters --------------------------------
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// Notice:Rotational periodicity only support rotation along the X axis!
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// periodicType: Which periodic boundary is used.
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// 0 -- without Periodic Boundary.
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// 1 -- Translational periodicity.
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// 2 -- Rotational periodicity.
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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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#########################################################################
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# Default parameters for Partition #
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#########################################################################
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@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
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// maxSimuStep: The max simulation step, don't care simulation is restart or not.
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// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
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// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
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// 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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@ -215,6 +226,7 @@ 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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@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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double TorqueRefZ = 0.0; // unit of meter.
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// directionMethod: The method of determining direction.
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// 1 -- using direciton.
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// 2 -- using face normal.
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// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
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// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
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// direction_inlet: The direction of inlet.
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// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
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// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
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// direction_outlet: The direction of outlet.
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int directionMethod = 2;
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double subsonicInletTotalPressure = 1.2e6;
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double subsonicInletTotalTemperature = 1300;
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double direction_inlet[] = 1, 0, 0;
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double subsonicOutletTotalPressure = 17.8571428;
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double subsonicOutletTotalTemperature = 1.0;
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double direction_outlet[] = 1, 0, 0;
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//-----------------------------------------------------------------------
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# Spatial Discretisation #
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//-----------------------------------------------------------------------
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@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
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string visualfile = "results/tecflow.plt";
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string Qwall_file = "results/Qwall.dat";
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string wall_aircoefile = "results/wall_aircoef.dat";
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string probesflowfile = "results/sample.dat";
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string surfacefile = "";
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string wall_varfile = "";
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@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
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// 1 -- Turbulent flat plate.
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int dumpStandardModel = 0;
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// ifSetProbesToMonitor: Set probes location to Monitor.
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// 0 -- Do not monitor.
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// 1 -- To monitor and save data to files.
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// probesDefineFile: probes location information file.
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// nProbeVariables: Number of variables want to be dumped for probes monitered.
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// probeVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
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// probeVariables order must from small to big.
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int ifSetProbesToMonitor = 0;
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string probesDefineFile = "bin/probes_location.hypara";
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int nProbeVariables = 6;
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int probeVariables[] = [0, 1, 2, 3, 4, 5];
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//-----------------------------------------------------------------------
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# Turbulence Parameter #
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//-----------------------------------------------------------------------
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@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
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// structhighordergradient:
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// -- "conservation", "chain_rule".
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int ifvfd = 0;
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string str_highorder_solver = "WCNS";
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int SolverStructOrder = 0;
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double str_highorder_interpolation_epsilon = 1.0e-6;
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string str_highorder_interpolation_type = "test";
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string str_highorder_flux_name = "steger";
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string structhighordergradient = "conservation";
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double coefofstrflux = 0.5;
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double limitcoefofinterface = 0.0;
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// ----------------- Advanced choices -----------------------------------
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// outtimesc: Time stepping scheme for the outer loop.
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@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
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double influenceRadius = 20;
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int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
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// ----------------- Periodic Parameters --------------------------------
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// Notice:Rotational periodicity only support rotation along the X axis!
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// periodicType: Which periodic boundary is used.
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// 0 -- without Periodic Boundary.
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// 1 -- Translational periodicity.
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// 2 -- Rotational periodicity.
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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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#########################################################################
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# Default parameters for Partition #
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#########################################################################
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@ -205,18 +215,20 @@ int numberOfMultigrid = 1;
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// maxSimuStep: The max simulation step, don't care simulation is restart or not.
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// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
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// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
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// 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 'res.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 = 3000;
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int maxSimuStep = 20000;
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int intervalStepFlow = 100;
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int intervalStepPlot = 100;
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int intervalStepForce = 1;
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int intervalStepRes = 1;
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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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@ -247,18 +259,24 @@ int compressible = 1;
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// 2 -- dump out wall Q & the typical position Q of ball.
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// 3 -- dump out wall Q & the typical position Q of cone.
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// 4 -- dump out wall Q & the typical position Q of double sphere.
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// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.
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// gridScaleFactor: The customizable unit of the grid, default value is 1.0 for meter.Common dimensions like:
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// 1 dm = 0.1 m.
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// 1 cm = 0.01 m.
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// 1 mm = 0.001m.
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// 1 inch = 0.0254m.
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// 1 foot = 12 inches = 0.3048m.
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// 1 yard = 3 feet = 0.9144m.
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// forceRefenenceLength, forceRefenenceLengthSpanWise, forceRefenenceArea: Reference length, SpanWise length and area, independent of grid unit.
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// TorqueRefX, TorqueRefY, TorqueRefZ: Reference point, independent of grid unit.
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// radiationCoef: the radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
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// radiationCoef: The radiation coefficient on wall, it is used to compute the radiation heat flux on wall when the boundary
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// condition is radiation equilibrium temperature, and 0.8 is the default value.
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double refMachNumber = 0.20;
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double attackd = 0.00;
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double refMachNumber = 0.73;
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double attackd = 2.79;
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double angleSlide = 0.00;
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int inflowParaType = 0;
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double refReNumber = 3900;
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double refReNumber = 6.5e6;
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double refDimensionalTemperature = 288.15;
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double freestream_vibration_temperature = 10000.00;
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@ -290,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
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double TorqueRefY = 0.0; // unit of meter.
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double TorqueRefZ = 0.0; // unit of meter.
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// directionMethod: The method of determining direction.
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// 1 -- using direciton.
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// 2 -- using face normal.
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// subsonicInletTotalPressure: The total pressure of subsonic inlet.
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// subsonicInletTotalTemperature: The total temperature of subsonic inlet.
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// direction_inlet: The direction of inlet.
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// subsonicOutletTotalPressure: The total pressure of subsonic outlet.
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// subsonicOutletTotalTemperature: The total temperature of subsonic outlet.
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// direction_outlet: The direction of outlet.
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int directionMethod = 2;
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double subsonicInletTotalPressure = 1.2e6;
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double subsonicInletTotalTemperature = 1300;
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double direction_inlet[] = 1, 0, 0;
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double subsonicOutletTotalPressure = 17.8571428;
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double subsonicOutletTotalTemperature = 1.0;
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double direction_outlet[] = 1, 0, 0;
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//-----------------------------------------------------------------------
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# Spatial Discretisation #
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//-----------------------------------------------------------------------
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@ -329,7 +329,7 @@ string str_limiter_name = "vanalbada";
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#*******************************************************************
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# UnStruct Solver or Common *
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#*******************************************************************
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// iviscous: Viscous model.
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// viscousType: Viscous model.
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// 0 -- Euler.
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// 1 -- Lamilar.
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// 2 -- Algebraic.
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@ -369,7 +369,7 @@ string str_limiter_name = "vanalbada";
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// 4 -- Ustar limiter model, without grid size unitary.
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// 7 -- default used.
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// venkatCoeff: Cofficient of vencat, when using vencat limter.
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// limitVariables: Limit model.
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// limitVariables: Limit model (It is useful only if limitVector is 0).
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// 0 -- limit only for pressure and denstiny, then get the min value.
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// 1 -- limit for every variables, then get the min value.
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// limitVector:
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@ -386,16 +386,16 @@ string str_limiter_name = "vanalbada";
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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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//int iviscous = 0;
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//int viscousType = 0;
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//string viscousName = "Euler";
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int viscousType = 1;
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string viscousName = "laminar";
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//int viscousType = 1;
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//string viscousName = "laminar";
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//int iviscous = 3;
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//string viscousName = "1eq-sa";
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int viscousType = 3;
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string viscousName = "1eq-sa";
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//int iviscous = 4;
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//int viscousType = 4;
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//string viscousName = "2eq-kw-menter-sst";
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int DESType = 0;
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@ -466,14 +466,14 @@ double roeEntropyScale = 1.0;
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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 = 1;
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double physicalTimeStep = 0.005;
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int iunsteady = 0;
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double physicalTimeStep = 0.01;
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int ifStartFromSteadyResults = 0;
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int ifStaticsFlowField = 0;
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int startStatisticStep = 0;
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int startStatisticStep = 800000;
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int min_sub_iter = 20;
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int max_sub_iter = 20;
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int min_sub_iter = 50;
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int max_sub_iter = 50;
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double tol_sub_iter = 0.01;
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int tscheme = 4;
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@ -502,10 +502,10 @@ int maxale = 10;
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double dtau = 0.001;
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double dtau_max = 1E-01;
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int wallFunctionType = 1;
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int wallFunctionType = 0;
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int RKStage = 2;
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double [] = 0.5, 1.0;
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double lamda[] = 0.5, 1.0;
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//int RKStage = 1;
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//double lamda[] = 1.0;
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@ -535,7 +535,7 @@ double [] = 0.5, 1.0;
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// visualfile: The visualization file path of flowfield , write data for every default (intervalStepPlot) steps.
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// wall_aircoefile: The file path to save flowfield variables of wall, write data for every default steps.
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int numberOfGridGroups = 1;
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string gridfile = "./grid/cylinder_Re3900_270w_split120.fts";
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string gridfile = "./grid/rae2822_hybrid2d__4.fts";
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int walldistMethod = 1;
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@ -549,7 +549,7 @@ string turbfile = "results/turb.dat";
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string visualfile = "results/tecflow.plt";
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string Qwall_file = "results/Qwall.dat";
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string wall_aircoefile = "results/wall_aircoef.dat";
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string probesflowfile = "results/sample.dat";
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string surfacefile = "";
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string wall_varfile = "";
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@ -561,13 +561,13 @@ string componentforcefile = "results/component_aircoef.dat";
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string overset_gridfile = "iblank.ovs";
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int isPlotVolumeField = 1;
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int isPlotVolumeField = 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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int visualfileType = 0;
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int visualfileType = 1;
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// visualSlice: The slice of tecflow.
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// 0 -- Do not save slice data.
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@ -588,17 +588,35 @@ double lowerPlotFieldBox[] = [0.0 0.0 0.0];
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double upperPlotFieldBox[] = [1.0 1.0 1.0];
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// nVisualVariables: Number of variables want to be dumped for tecplot visualization.
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// visualVariables : variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6)
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// visualVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5), mach(6),
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// -- viscosityLaminar(7), viscosityTurbulent(8),
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// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12), strain_rate(13), Q_criteria(14)
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// -- Cp(15), timeStep(16), volume(17)
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// -- modeledTKE(18),modeleddissipationrate(19), SSTF1(20), SSTF2(21) ,vibration temperature(33), electron temperature(34)
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// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!.
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// Arriables order must from small to larger.
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int nVisualVariables = 10;
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int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 11, 12, 15];;
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// -- vorticity_x(9), vorticity_y(10), vorticity_z(11), vorticityMagnitude(12),
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// -- strain_rate(13), Q_criteria(14), Cp(15), timeStep(16), volume(17),
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// -- modeledTKE(18), modeleddissipationrate(19), SSTF1(20), SSTF2(21), vibration temperature(33), electron temperature(34),
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// -- gradientUx(41), gradientUy(42), gradientVx(43), gradientVy(44).
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// Important Warning: Array size of visualVariables MUST be equal to nVisualVariables!!!
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// Variables order must from small to big.
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int nVisualVariables = 8;
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int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
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// dumpStandardModel: Dump many standard model data.
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// 1 -- Turbulent flat plate.
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int dumpStandardModel = 0;
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// ifSetProbesToMonitor: Set probes location to Monitor.
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// 0 -- Do not monitor.
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// 1 -- To monitor and save data to files.
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// probesDefineFile: probes location information file.
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// nProbeVariables: Number of variables want to be dumped for probes monitered.
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// probeVariables : Variable types dumped, listed as following:
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// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
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// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
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// probeVariables order must from small to big.
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int ifSetProbesToMonitor = 0;
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string probesDefineFile = "bin/probes_location.hypara";
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int nProbeVariables = 6;
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int probeVariables[] = [0, 1, 2, 3, 4, 5];
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//-----------------------------------------------------------------------
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# Turbulence Parameter #
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//-----------------------------------------------------------------------
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@ -620,51 +638,11 @@ double muoo = 1.0e-1;
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double kwoo = 1.0;
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# maximum eddy viscosity (myt/my) max.
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double eddyViscosityLimit = 1.0e5;
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double eddyViscosityLimit = 1.0e10;
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double sdilim = 1.0e20;
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double coef_kvist = 1.0;
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int monitor_vistmax = 0;
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//-----------------------------------------------------------------------
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# LES Parameter #
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//-----------------------------------------------------------------------
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// iLES : Create LESSolver or not.
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// >= 1 - Create LESSolver;
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// < 1 - not;
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// sgsmodel : subgrid scale model
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// = "smagorinsky" ;
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// = "dsm" ;
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// = "wale" ;
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// deltaFunctionType : = 1 - MAX(deltai, deltaj, deltak)
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// = 2 - pow(deltai * deltaj *deltak, 1/3)
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// = 3 - Devloped by Scotti
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// wallDampingFunctionType : = 0 - no wall function
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// = 1 - van Driest
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// = 2 - developed by Dr. Deng Xiaobing
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// = 3 - developed by Piomelli
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// turbViscousCutType : turbulent viscosity cut type
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// = 0 - mu_total = mut + mul
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// = 1 - mu_total = max(mut-mul,0)+ mul
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// = 2 - mu_total = max(mut ,0)+ mul
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// smagConstant : constant of smagorinsky model.
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// waleConstant : constant of wale model
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// filterDirection[3] : filter variables in i, j, k direction or not;
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// averageDirection[3] : average variables in i, j, k direction or not;
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// isotropicConstant : constant of isotropic part of SGS stress
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int iLES = 1;
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string sgsmodel = "smagorinsky";
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int deltaFunctionType = 2;
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int wallDampingFunctionType = 1;
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int turbViscousCutType = 2;
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double smagConstant = 0.135;
|
||||
double isotropicConstant = 0.0;
|
||||
double waleConstant = 0.6;
|
||||
int filterDirection[] = [1, 1, 0];
|
||||
int averageDirection[] = [1, 1, 0];
|
||||
double testFilterScale = 2.0;
|
||||
int averageWidth = 1;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Other Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -805,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
@ -822,7 +803,7 @@ string structhighordergradient = "conservation";
|
|||
// 0 -- the effect of the limiter is cancelled, means the first-order interpolations.
|
||||
// allReduceStep: Iteration intervals for MPI AllReduce operation, default is 1.
|
||||
string outtimesc = "impbd2";
|
||||
double MUSCLCoefXk = 0.8;
|
||||
double MUSCLCoefXk = -1;
|
||||
double MUSCLCoefXb = 1.0;
|
||||
int allReduceStep = 1;
|
||||
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
|
|
@ -146,6 +146,16 @@ int numberOfReferenceCP = 10;
|
|||
double influenceRadius = 20;
|
||||
int symmetryPlane = 3; // 1: plane of x=0; 2: plane of y=0; 3: plane of z=0;
|
||||
|
||||
// ----------------- Periodic Parameters --------------------------------
|
||||
// Notice:Rotational periodicity only support rotation along the X axis!
|
||||
// periodicType: Which periodic boundary is used.
|
||||
// 0 -- without Periodic Boundary.
|
||||
// 1 -- Translational periodicity.
|
||||
// 2 -- Rotational periodicity.
|
||||
int periodicType = 0;
|
||||
double translationLength[] = [0.0,0.0,0.0];
|
||||
double rotationAngle = 0.0;
|
||||
|
||||
#########################################################################
|
||||
# Default parameters for Partition #
|
||||
#########################################################################
|
||||
|
|
@ -205,6 +215,7 @@ int numberOfMultigrid = 1;
|
|||
// maxSimuStep: The max simulation step, don't care simulation is restart or not.
|
||||
// intervalStepFlow: The step intervals for flow variables file 'flow.dat' saved.
|
||||
// intervalStepPlot: The step intervals for tecplot visual file 'tecflow.dat' saved.
|
||||
// intervalStepSample: The step intervals for monitored probes variables file 'sample.dat' saved.
|
||||
// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.dat' saved.
|
||||
// intervalStepRes: The step intervals for residual file 'res.dat' saved.
|
||||
// ifLowSpeedPrecon: Precondition process to accelerate convergence for low speed flow.
|
||||
|
|
@ -215,6 +226,7 @@ int maxSimuStep = 20000;
|
|||
|
||||
int intervalStepFlow = 1000;
|
||||
int intervalStepPlot = 1000;
|
||||
int intervalStepSample = 1000;
|
||||
int intervalStepForce = 100;
|
||||
int intervalStepRes = 10;
|
||||
int ifLowSpeedPrecon = 0;
|
||||
|
|
@ -296,24 +308,6 @@ double TorqueRefX = 0.0; // unit of meter.
|
|||
double TorqueRefY = 0.0; // unit of meter.
|
||||
double TorqueRefZ = 0.0; // unit of meter.
|
||||
|
||||
// directionMethod: The method of determining direction.
|
||||
// 1 -- using direciton.
|
||||
// 2 -- using face normal.
|
||||
// subsonicInletTotalPressure: The dimensional total pressure of subsonic inlet if height > 0, else non-dimensional.
|
||||
// subsonicInletTotalTemperature: The dimensional total temperature of subsonic inlet if height > 0, else non-dimensional.
|
||||
// direction_inlet: The direction of inlet.
|
||||
// subsonicOutletTotalPressure: The dimensional total pressure of subsonic outlet if height > 0, else non-dimensional.
|
||||
// subsonicOutletTotalTemperature: The dimensional total temperature of subsonic outlet if height > 0, else non-dimensional.
|
||||
// direction_outlet: The direction of outlet.
|
||||
int directionMethod = 2;
|
||||
double subsonicInletTotalPressure = 1.2e6;
|
||||
double subsonicInletTotalTemperature = 1300;
|
||||
double direction_inlet[] = 1, 0, 0;
|
||||
|
||||
double subsonicOutletTotalPressure = 17.8571428;
|
||||
double subsonicOutletTotalTemperature = 1.0;
|
||||
double direction_outlet[] = 1, 0, 0;
|
||||
|
||||
//-----------------------------------------------------------------------
|
||||
# Spatial Discretisation #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -335,7 +329,7 @@ string str_limiter_name = "vanalbada";
|
|||
#*******************************************************************
|
||||
# UnStruct Solver or Common *
|
||||
#*******************************************************************
|
||||
// iviscous: Viscous model.
|
||||
// viscousType: Viscous model.
|
||||
// 0 -- Euler.
|
||||
// 1 -- Lamilar.
|
||||
// 2 -- Algebraic.
|
||||
|
|
@ -555,7 +549,7 @@ string turbfile = "results/turb.dat";
|
|||
string visualfile = "results/tecflow.plt";
|
||||
string Qwall_file = "results/Qwall.dat";
|
||||
string wall_aircoefile = "results/wall_aircoef.dat";
|
||||
|
||||
string probesflowfile = "results/sample.dat";
|
||||
string surfacefile = "";
|
||||
|
||||
string wall_varfile = "";
|
||||
|
|
@ -610,6 +604,19 @@ int visualVariables[] = [0, 1, 2, 3, 4, 5, 6, 15];
|
|||
// 1 -- Turbulent flat plate.
|
||||
int dumpStandardModel = 0;
|
||||
|
||||
// ifSetProbesToMonitor: Set probes location to Monitor.
|
||||
// 0 -- Do not monitor.
|
||||
// 1 -- To monitor and save data to files.
|
||||
// probesDefineFile: probes location information file.
|
||||
// nProbeVariables: Number of variables want to be dumped for probes monitered.
|
||||
// probeVariables : Variable types dumped, listed as following:
|
||||
// -- density(0), u(1), v(2), w(3), pressure(4), temperature(5).
|
||||
// Important Warning: Array size of probeVariables MUST be equal to nProbeVariables!!!
|
||||
// probeVariables order must from small to big.
|
||||
int ifSetProbesToMonitor = 0;
|
||||
string probesDefineFile = "bin/probes_location.hypara";
|
||||
int nProbeVariables = 6;
|
||||
int probeVariables[] = [0, 1, 2, 3, 4, 5];
|
||||
//-----------------------------------------------------------------------
|
||||
# Turbulence Parameter #
|
||||
//-----------------------------------------------------------------------
|
||||
|
|
@ -776,11 +783,14 @@ string zoneInverseFileName = "./grid/zoneInverseMapping.inp";
|
|||
// structhighordergradient:
|
||||
// -- "conservation", "chain_rule".
|
||||
int ifvfd = 0;
|
||||
string str_highorder_solver = "WCNS";
|
||||
int SolverStructOrder = 0;
|
||||
double str_highorder_interpolation_epsilon = 1.0e-6;
|
||||
string str_highorder_interpolation_type = "test";
|
||||
string str_highorder_flux_name = "steger";
|
||||
string structhighordergradient = "conservation";
|
||||
double coefofstrflux = 0.5;
|
||||
double limitcoefofinterface = 0.0;
|
||||
|
||||
// ----------------- Advanced choices -----------------------------------
|
||||
// outtimesc: Time stepping scheme for the outer loop.
|
||||
|
|
|
|||
Loading…
Reference in New Issue