forked from PHengLEI/PHengLEI-TestCases
G07算例参数及说明文档更新
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# nBoundaryConditons : Number of global boundary conditions.
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# nBoundaryConditions: Number of global boundary conditions.
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# bcName : Boundary condition name.
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# bcName : Boundary condition name.
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# bcType(in PHengLEI): Boundary condition type.
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# bcType(in PHengLEI): Boundary condition type.
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@ -44,7 +44,7 @@ string bcName = "inlet";
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{
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{
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int bcType = 5;
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int bcType = 5;
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int inflowParaType = 5;
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int inflowParaType = 5;
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double refDimensionalVelocity = 9.2;
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double refDimensionalVelocity = 68.9;
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double refDimensionalPressure = 101325.0;
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double refDimensionalPressure = 101325.0;
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string speciesName ="Air, CH4";
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string speciesName ="Air, CH4";
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double initMassFraction[2] = [1.0, 0.0];
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double initMassFraction[2] = [1.0, 0.0];
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@ -53,7 +53,7 @@ string bcName = "jet";
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{
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{
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int bcType = 5;
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int bcType = 5;
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int inflowParaType = 5;
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int inflowParaType = 5;
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double refDimensionalVelocity = 68.9;
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double refDimensionalVelocity = 340.5;
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double refDimensionalPressure = 101325.0;
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double refDimensionalPressure = 101325.0;
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string speciesName ="Air, CH4";
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string speciesName ="Air, CH4";
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double initMassFraction[2] = [0.0, 1.0];
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double initMassFraction[2] = [0.0, 1.0];
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@ -7,7 +7,7 @@
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// intervalStepForce: The step intervals for aerodynamics coefficients file 'aircoef.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 'res.dat' saved.
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int maxSimuStep = 50000;
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int maxSimuStep = 30000;
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int intervalStepFlow = 1000;
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int intervalStepFlow = 1000;
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int intervalStepPlot = 1000;
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int intervalStepPlot = 1000;
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int intervalStepForce = 100;
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int intervalStepForce = 100;
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