forked from PHengLEI/PHengLEI-TestCases
更新算例
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@ -6,10 +6,10 @@
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//! 2 -- Flat plate boundary layer with 1 part.
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//! 3 -- Flat plate boundart later with 2 parts.
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//! 4 -- Poiseuille flow.
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//int gridDataBaseIndex = 1;
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//string gridDataBaseFileName = "./bin/GridDataBase_TaylorGreenVortex.hypara";
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int gridDataBaseIndex = 2;
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string gridDataBaseFileName = "./bin/GridDataBase_Flat_Plate_Boundary_Layer_1_part.hypara";
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int gridDataBaseIndex = 1;
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string gridDataBaseFileName = "./bin/GridDataBase_TaylorGreenVortex.hypara";
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//int gridDataBaseIndex = 2;
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//string gridDataBaseFileName = "./bin/GridDataBase_Flat_Plate_Boundary_Layer_1_part.hypara";
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//! gridOutputFile: The name of output grid.
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string gridOutputFile = "./grid/test_grid.fts";
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@ -1,7 +1,7 @@
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int nBlocks = 1;
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int nNodeX = 32;
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int nNodeY = 32;
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int nNodeX = 64;
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int nNodeY = 64;
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int nNodeZ = 1;
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double lengthX = 6.283185307179586476925286766559;
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@ -921,4 +921,8 @@ int numberOfMovingBodies = 2;
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#########################################################################
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int isPlotVolumeField = 0;
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#########################################################################
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# user define parameter #
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#########################################################################
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int UDFInitFluid = 1;
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string UDFInitFluidType = "TGV";
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@ -7,9 +7,9 @@
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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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int maxSimuStep = 15000;
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int maxSimuStep = 5000;
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int intervalStepFlow = 1;
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int intervalStepFlow = 5;
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int intervalStepPlot = 100;
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int intervalStepForce = 100;
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int intervalStepRes = 10;
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@ -17,7 +17,7 @@ int intervalStepRes = 10;
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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 ifLowSpeedPrecon = 0;
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int ifLowSpeedPrecon = 1;
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#########################################################################
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# Inflow Parameter #
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@ -44,12 +44,12 @@ int ifLowSpeedPrecon = 0;
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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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double refMachNumber = 0.1;
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double refMachNumber = 0.3;
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double attackd = 0.00;
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double angleSlide = 0.00;
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int inflowParaType = 0;
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double refReNumber = 2.0e5;
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double refReNumber = 100;
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double refDimensionalTemperature = 288.15;
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//int inflowParaType = 1;
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@ -62,17 +62,17 @@ int useSlipVelocityType =0;
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int forceDragType = 1;
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//! The lift force
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int forceMagnusType = 1;
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int forceSaffmanType = 1;
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int forceMagnusType = 0;
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int forceSaffmanType = 0;
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//! The stress-gradient force
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int forceFluidAccelerationType = 1;
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int forceFluidAccelerationType = 0;
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//! The added-mass force
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int forceAddedMassType = 1;
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int forceAddedMassType = 0;
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//! The Basset history force;
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int forceBassetType = 1;
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int forceBassetType = 0;
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//! #########################################################################
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//! # Output Variable #
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