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Cp distribution around OneraM6 wing simpleFoam |
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November 15, 2017, 02:45 |
Cp distribution around OneraM6 wing simpleFoam
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New Member
Join Date: May 2017
Location: Japan, Kitakyushu
Posts: 19
Rep Power: 9 |
Hello,
I'm currently trying to validate a simulation around the OmeraM6 wing at M=0.7 and alpha=3.06 deg. However, my pressure distribution doesn't match the experimental result (cf pictures). It seems both the lower and upper side give the same distribution, that means there is no pressure difference between both sides. I computed cp using the pressure function in my controlDict file : Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 4.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; location "system"; object controlDict; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // application simpleFoam; startFrom startTime; startTime 0; stopAt endTime; endTime 500; deltaT 1; writeControl timeStep; writeInterval 50; purgeWrite 0; writeFormat ascii; writePrecision 6; writeCompression off; timeFormat general; timePrecision 6; runTimeModifiable true; functions { pressureTools1 { type pressure; functionObjectLibs ("libfieldFunctionObjects.so"); enabled yes; region region0; calcTotal no; calcCoeff yes; timeStart 500; timeEnd 500; writeControl outputTime; writeInterval 1; rhoInf 1.17663; pInf 0; UInf (242.6835 0 12.9734); } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 4.1 | | \\ / 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 (242.6835 0 12.9734); boundaryField { inlet { type freestream; freestreamValue uniform (242.6835 0 12.9734); } outlet { type zeroGradient; } box { type slip; } oneraM6 { type noSlip; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 4.1 | | \\ / 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 zeroGradient; } box { type zeroGradient; } oneraM6 { type zeroGradient; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 4.1 | | \\ / 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; } box { type zeroGradient; } oneraM6 { type fixedValue; value uniform 0; } } // ************************************************************************* // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 4.1 | | \\ / 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; } box { type calculated; value uniform 0.14; } oneraM6 { type nutUSpaldingWallFunction; value uniform 0; } } // ************************************************************************* // The experimental results come from AGARD Advisory Report No. 138. Thank you, Dorian Last edited by Dorian1504; November 15, 2017 at 04:50. |
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