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Problem with a airFoil2D case with another mesh |
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June 27, 2018, 10:36 |
Problem with a airFoil2D case with another mesh
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New Member
Iman Sabahi
Join Date: May 2018
Posts: 17
Rep Power: 8 |
Dear all
I'm running a case similar to airFoil2D case on OpenFOAM 5.0, and the residuals aren't converging. I've also turned the turbulence off in order to accelerate my solution, I plan to turn it on once i get results without turbulence. Here is the link to my case file: https://drive.google.com/open?id=1OC...T_hC-FrZL941Jn My residuals' plot is in the attachment. Also my boundary conditions and fvSolution are as follows: Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 3.0.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volVectorField; object U; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 1 -1 0 0 0 0]; internalField uniform (2.9886 0 0.2615); boundaryField { inlet { type freestream; freestreamValue uniform (2.9886 0 0.2615); } outlet { type freestream; freestreamValue uniform (2.9886 0 0.2615); } topAndBottom { type freestream; freestreamValue uniform (2.9886 0 0.2615); } airfoil { type noSlip; } defaultFaces { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 3.0.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; object p; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 2 -2 0 0 0 0]; internalField uniform 0; boundaryField { inlet { type freestreamPressure; } outlet { type freestreamPressure; } topAndBottom { type freestreamPressure; } airfoil { type zeroGradient; } defaultFaces { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 3.0.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; object nuTilda; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 2 -1 0 0 0 0]; internalField uniform 0.14; boundaryField { inlet { type freestream; freestreamValue uniform 0.14; } outlet { type freestream; freestreamValue uniform 0.14; } topAndBottom { type freestream; freestreamValue uniform 0.14; } airfoil { type fixedValue; value uniform 0; } defaultFaces { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 3.0.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; object nut; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 2 -1 0 0 0 0]; internalField uniform 0.14; boundaryField { inlet { type freestream; freestreamValue uniform 0.14; } outlet { type freestream; freestreamValue uniform 0.14; } topAndBottom { type freestream; freestreamValue uniform 0.14; } airfoil { type nutUSpaldingWallFunction; value uniform 0; } defaultFaces { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 3.0.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; location "system"; object fvSolution; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // solvers { p { solver GAMG; tolerance 1e-06; relTol 0.1; smoother GaussSeidel; nPreSweeps 0; nPostSweeps 2; cacheAgglomeration true; nCellsInCoarsestLevel 10; agglomerator faceAreaPair; mergeLevels 1; } U { solver smoothSolver; smoother GaussSeidel; nSweeps 2; tolerance 1e-08; relTol 0.1; } nuTilda { solver smoothSolver; smoother GaussSeidel; nSweeps 2; tolerance 1e-08; relTol 0.1; } } SIMPLE { nNonOrthogonalCorrectors 0; pRefCell 0; pRefValue 0; residualControl { p 1e-10; U 1e-10; nuTilda 1e-10; } } relaxationFactors { fields { p 0.3; } equations { U 0.7; nuTilda 0.7; } } // ************************************************************************* // |
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