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simulating flow over aerofoil(naca0012)using openfoam

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Old   August 29, 2018, 22:21
Default simulating flow over aerofoil(naca0012)using openfoam
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zein elserfy
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I have tried to model flow over the aerofoil using SA model and the result for lift and drag coefficient using not matching the experimental data, then I try to use K-w SST model and I have problems in convergence espically at the angle of attack higher than 10

have anyone tried this case on openfoam?

so we can share our result
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