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Unphysical pressure in channel Poiseuille flow |
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June 21, 2023, 09:08 |
Unphysical pressure in channel Poiseuille flow
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Nikos Vasileiadis
Join Date: May 2022
Posts: 5
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Hi guys,
I'm trying to solve the steady-state laminar compresible Poiseuille flow through a 2D channel using rhoSimpleFoam. The rhoSimpleFoam solver converges and for the most part the solution looks reasonable as seen in the attached images. However, taking a closer look at the outlet, a weird behaviour is seen for the pressure. I have tried using a finer mesh and also played around with fvSchemes and fvSolution controls but this behaviour persists and even becomes worse in some cases. I have also tried rhoPimpleFoam. In that case, when steady-state is reached, I don't get the exact same behaviour seen with rhoSimpleFoam but the pressure shows a "wavy" profile near the outlet. Since this is a pretty simple case I expect that someone else has encountered something similar? Any help will be greatly appreciated. Thanks! blockMeshDict Code:
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 1.7.1 | | \\ / A nd | Web: www.OpenFOAM.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; root ""; case ""; instance ""; local ""; class dictionary; object blockMeshDict; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // scale 1e0; vertices ( (0 0 0) (2e-5 0 0) (2e-5 5e-7 0) (0 5e-7 0) (0 0 5e-8) (2e-5 0 5e-8) (2e-5 5e-7 5e-8) (0 5e-7 5e-8) ); blocks ( hex (0 1 2 3 4 5 6 7) dsmcZone (1000 50 1) simpleGrading (1 1 1) ); boundary ( inlet { type patch; faces ( (0 4 7 3) ); } outlet { type patch; faces ( (1 2 6 5) ); } wall { type wall; faces ( (7 6 2 3) ); } symmetry { type symmetryPlane; faces ( (4 5 1 0) ); } empty { type empty; faces ( (4 5 6 7) (0 3 2 1) ); } ); mergePatchPairs ( ); // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.4.0 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; location "constant"; object thermophysicalProperties; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // thermoType { type hePsiThermo; mixture pureMixture; transport const; thermo hConst; equationOfState perfectGas; specie specie; energy sensibleInternalEnergy; } mixture { specie { molWeight 39.93; } thermodynamics { Cp 520.33; Hf 0; } transport { mu 2.117e-5; Pr 0.666667; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2206 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; arch "LSB;label=32;scalar=64"; class volScalarField; location "0"; object p; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [1 -1 -2 0 0 0 0]; internalField uniform 20000; boundaryField { inlet { type totalPressure; gamma 1.66667; p0 uniform 100000; value uniform 100000; } outlet { type fixedValue; value uniform 20000; } wall { type zeroGradient; } symmetry { type symmetryPlane; } empty { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2206 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; arch "LSB;label=32;scalar=64"; class volScalarField; location "0"; object T; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 0 0 1 0 0 0]; internalField uniform 300; boundaryField { inlet { type totalTemperature; gamma 1.66667; T0 uniform 300; value uniform 300; } outlet { type zeroGradient; } wall { type fixedValue; value uniform 300; } symmetry { type symmetryPlane; } empty { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2206 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; arch "LSB;label=32;scalar=64"; class volVectorField; location "0"; object U; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 1 -1 0 0 0 0]; internalField uniform (0 0 0); boundaryField { inlet { type pressureInletVelocity; value uniform (0 0 0); } outlet { type zeroGradient; } wall { type fixedValue; value uniform (0 0 0); } symmetry { type symmetryPlane; } empty { type empty; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: v2206 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object fvSchemes; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // ddtSchemes { default steadyState; } gradSchemes { default Gauss linear; } divSchemes { default Gauss linear; div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear; } laplacianSchemes { default Gauss linear corrected; } interpolationSchemes { default linear; } snGradSchemes { default corrected; } wallDist { method meshWave; } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: v2206 | | \\ / A nd | Website: www.openfoam.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object fvSolution; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // solvers { p { solver GAMG; smoother GaussSeidel; nSweeps 2; tolerance 1e-06; relTol 0.0; minIter 3; maxIter 100; nCellsInCoarsestLevel 100; } "(U|e)" { solver PBiCGStab; preconditioner DILU; minIter 3; maxIter 100; tolerance 1e-8; relTol 0.0; } } SIMPLE { momentumPredictor yes; transonic yes; nNonOrthogonalCorrectors 1; turbOnFinalIterOnly false; residualControl { p 1e-5; U 1e-7; e 1e-6; } } relaxationFactors { equations { p 0.3; U 0.7; e 0.7; } } // ************************************************************************* // |
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Tags |
perfectgas, poiseuille flow, rhopimplefoam, rhosimplefoam error |
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