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NACA0012 does not get the result of the stall

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Old   May 9, 2021, 05:18
Default NACA0012 does not get the result of the stall
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Hello everyone, I am now using openfoam to compare with experimental data. The results compare well before the stall. But when there is a stall situation and the lift coefficient should decrease, my lift coefficient is still increasing. Can someone tell me why this is. I am using simpleFoam, SA model.
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Old   May 9, 2021, 12:17
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I don't think there is a RANS or even hybrid RANS-LES setup that can predict the polar coefficients correctly for a given airfoil at stall and post-stall regions.
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Old   May 9, 2021, 15:28
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Quote:
Originally Posted by cheng1 View Post
I am using simpleFoam, SA model.
I think that you answered your own question there - it's not an OpenFOAM issue. Have a read up around the subject and you'll learn how difficult the problem is.
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