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31 lines
1.0 KiB
C++
31 lines
1.0 KiB
C++
/*--------------------------------*- C++ -*----------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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| \\ / O peration | Version: plus |
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| \\ / A nd | Web: www.OpenFOAM.com |
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\\/ M anipulation |
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-------------------------------------------------------------------------------
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Description
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Calculates lift, drag and moment coefficients by summing forces on
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specified patches for a case where the solver is compressible (pressure is
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in units M/(LT^2), e.g. Pa).
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\*---------------------------------------------------------------------------*/
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patches (patch1 patch2);
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magUInf 20;
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rhoInf 1.225;
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lRef 1;
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Aref 1;
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liftDir (0 0 1);
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dragDir (1 0 0);
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CofR (0 0 0);
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pitchAxis (0 1 0);
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#includeEtc "caseDicts/postProcessing/forces/forceCoeffs.cfg"
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// ************************************************************************* //
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