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"FOAM FATAL IO ERROR: Cannot find patchField entry for NACA6409_patch24311" |
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October 7, 2019, 05:57 |
"FOAM FATAL IO ERROR: Cannot find patchField entry for NACA6409_patch24311"
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#1 |
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Dear Foamers,
I made a case of the NACA_6409 Airfoil. As I run the solver, the error below has appeared; FOAM FATAL IO ERROR: Cannot find patchField entry for NACA6409_patch24311 I checked all the files in boundary conditions and especially in 0 folder and nothing seemed to be faulty in me. Below, you will find the blockesh.dict and the p file from the boundary conditions. I can't find where the problem is, so every help would be priceless. Thank you very much ! blockMesh.dict /*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: dev | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object blockMeshDict; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // convertToMeters 0.01; vertices ( (-75 -10 210)//0 (315 -10 210)//1 (315 -10 -180)//2 (-75 -10 -180)//3 (-75 10 210)//4 (315 10 210)//5 (315 10 -180)//6 (-75 10 -180)//7 ); blocks ( hex (0 1 2 3 4 5 6 7) (120 90 150) simpleGrading ( ( (0.05 10 20)//inflow (0.14 10 1)//front_from_flap (0.047 30 3)//flap (0.71 40 1.2)//back_from_flap (0.05 10 0.1)//outflow ) ( (0.49 25 5) (0.1 50 1) (0.48 25 0.5) ) ( (0.4 10 1) (0.2 80 1) (0.4 10 1) ) ) ); edges ( ); boundary ( inlet { type patch; faces ( (0 3 7 4) ); } outlet { type patch; faces ( (1 2 6 5) ); } upperWall { type wall; faces ( (4 5 6 7) ); } lowerWall { type wall; faces ( (0 1 2 3) ); } rightWall { type symmetry; faces ( (0 1 5 4) ); } leftWall { type symmetry; faces ( (3 2 6 7) ); } ); mergePatchPairs ( ); // ************************************************** *********************** // p file (0/p) /*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: dev | | \\ / 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; freestreamValue $internalField; } outlet { type freestreamPressure; freestreamValue $internalField; } upperWall { type zeroGradient; } lowerWall { type zeroGradient; } NACA6409 { type zeroGradient; } rightWall { type symmetry; } leftWall { type symmetry; } } // ************************************************** *********************** // |
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