pointwise划分了地形网格计算域为3000*3000*1000 ，用openFoam中simpleFoam求解计算错误？
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我在这个问题这儿卡了2个月了，我用pointwise划分了一个复杂地型网格，计算域300030001000，最小网格长宽为30*30，第一层网格高度为50cm,我计算的时候出现如下现象,到最后一行，算例自动停止。
我最初的想法是将of自带的一个例子里的网格替换成用pointwise生成的网格，进行计算，不知道出了什么问题，希望能得到各位老师的帮助，谢谢！/*---------------------------------------------------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ Build : 6-e29811f5dff8 Exec : simpleFoam Date : Jun 07 2019 Time : 18:39:08 Host : "DESKTOP-K2TDLI2" PID : 434 I/O : uncollated Case : /home/dyb/turbineSiting nProcs : 1 sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 10) allowSystemOperations : Allowing user-supplied system call operations // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 SIMPLE: Convergence criteria found p: tolerance 0.001 U: tolerance 0.0001 "(k|epsilon)": tolerance 0.0001 Reading field p Reading field U Reading/calculating face flux field phi Selecting incompressible transport model Newtonian Selecting turbulence model type RAS Selecting RAS turbulence model kEpsilon kEpsilonCoeffs { Cmu 0.09; C1 1.44; C2 1.92; sigmaEps 1.11; C3 0; sigmak 1; } No MRF models present No finite volume options present Starting time loop Time = 0.5 smoothSolver: Solving for Ux, Initial residual = 1, Final residual = 0.130925946068, No Iterations 1000 smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 0.305787562946, No Iterations 1000 smoothSolver: Solving for Uz, Initial residual = 1, Final residual = 1.18059515052, No Iterations 1000如下是我的一些设置
fvSolution/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object fvSolution; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // solvers { p { solver GAMG; tolerance 1e-7; relTol 0.1; smoother GaussSeidel; } U { solver smoothSolver; smoother GaussSeidel; tolerance 1e-8; relTol 0.1; nSweeps 1; } k { solver smoothSolver; smoother GaussSeidel; tolerance 1e-8; relTol 0.1; nSweeps 1; } epsilon { solver smoothSolver; smoother GaussSeidel; tolerance 1e-8; relTol 0.1; nSweeps 1; } } SIMPLE { nNonOrthogonalCorrectors 0; residualControl { p 1e-3; U 1e-4; "(k|epsilon)" 1e-4; } } relaxationFactors { fields { p 0.3; } equations { U 0.7; k 0.7; epsilon 0.7; } } cache { grad(U); } // ************************************************************************* //fvSchemes
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object fvSchemes; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // ddtSchemes { default steadyState; } gradSchemes { default Gauss linear; } divSchemes { default none; div(phi,U) bounded Gauss upwind; div(phi,epsilon) bounded Gauss upwind; div(phi,k) bounded Gauss upwind; div((nuEff*dev2(T(grad(U))))) Gauss linear; } laplacianSchemes { default Gauss linear limited corrected 0.33; } interpolationSchemes { default linear; } snGradSchemes { default limited corrected 0.33; } // ************************************************************************* //controlDict
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object controlDict; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // application simpleFoam; startFrom latestTime; startTime 0; stopAt endTime; endTime 1000; deltaT 0.5; writeControl timeStep; writeInterval 50; purgeWrite 0; writeFormat binary; writePrecision 12; writeCompression off; timeFormat general; timePrecision 6; runTimeModifiable yes; libs ("libatmosphericModels.so"); // ************************************************************************* //
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看起来像是边界条件设置有问题
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李老师，我把我的边界条件发过来，您帮忙看一下。大概是压力项可能出错了
epsilon
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object epsilon; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 2 -3 0 0 0 0]; #include "include/initialConditions" internalField uniform $turbulentEpsilon; boundaryField { terrain { type epsilonWallFunction; Cmu 0.09; kappa 0.4; E 9.8; value $internalField; } outlet { type inletOutlet; inletValue uniform $turbulentEpsilon; value $internalField; } inlet { type atmBoundaryLayerInletEpsilon; #include "include/ABLConditions" } ground { type zeroGradient; } top { type slip; } sides { type slip; } } // ************************************************************************* //k
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; object k; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // #include "include/initialConditions" dimensions [0 2 -2 0 0 0 0]; internalField uniform $turbulentKE; boundaryField { outlet { type inletOutlet; inletValue uniform $turbulentKE; value $internalField; } inlet { type atmBoundaryLayerInletK; #include "include/ABLConditions" } terrain { type kqRWallFunction; value uniform 0.0; } ground { type zeroGradient; } top { type slip; } sides { type slip; } } // ************************************************************************* // nut /*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object nut; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 2 -1 0 0 0 0]; internalField uniform 0; boundaryField { #include "include/ABLConditions" inlet { type calculated; value uniform 0; } outlet { type calculated; value uniform 0; } terrain { type nutkAtmRoughWallFunction; z0 $z0; value uniform 0.0; } ground { type calculated; value uniform 0; } top { type slip; } sides { type slip; } } // ************************************************************************* //P
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; object p; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // #include "include/initialConditions" dimensions [0 2 -2 0 0 0 0]; internalField uniform $pressure; boundaryField { inlet { type zeroGradient; } outlet { type uniformFixedValue; uniformValue $internalField; } terrain { type zeroGradient; } ground { type zeroGradient; } top { type slip; } sides { type slip; } } // ************************************************************************* //u
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volVectorField; location "0"; object U; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // #include "include/initialConditions" dimensions [0 1 -1 0 0 0 0]; internalField uniform $flowVelocity; boundaryField { outlet { type inletOutlet; inletValue uniform (0 0 0); value $internalField; } inlet { type atmBoundaryLayerInletVelocity; #include "include/ABLConditions" } terrain { type uniformFixedValue; uniformValue (0 0 0); value uniform (0 0 0); } ground { type uniformFixedValue; value uniform (0 0 0); uniformValue constant (0 0 0); } top { type slip; } sides { type slip; } } // ************************************************************************* //说明文件ABL
========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ Uref 10.0; Zref 20; zDir (0 0 1); flowDir (1 0 0); z0 uniform 0.1; zGround uniform 0; // ************************************************************************* //initialConditions
/*--------------------------------*- C++ -*----------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | Website: https://openfoam.org \\ / A nd | Version: 6 \\/ M anipulation | \*---------------------------------------------------------------------------*/ flowVelocity (0 0 0); pressure 0; turbulentKE 1.3; turbulentEpsilon 0.01; // ************************************************************************* //fixedInlet
inlet { type fixedValue; value $internalField; }
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解决了，不同尺度的网格对应压力求解方法的平滑smoother有问题，初始条件也没有错，
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