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NACA0012 does not get the result of the stall |
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May 9, 2021, 05:18 |
NACA0012 does not get the result of the stall
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#1 |
New Member
cheng
Join Date: Apr 2021
Posts: 5
Rep Power: 5 |
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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May 9, 2021, 12:17 |
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#2 |
Senior Member
Herpes Free Engineer
Join Date: Sep 2019
Location: The Home Under The Ground with the Lost Boys
Posts: 931
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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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May 9, 2021, 15:28 |
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#3 |
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Location: UK
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openfoam,stall,sa |
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