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Fluctuating residuals at high angle of attack for NACA0018 |
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Anand Thamban
Join Date: Jun 2016
Posts: 1
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Hello!
I am currently doing an analysis on NACA 0018 to find the stall angle. I have used k-kl-w turbulence model and Re=100,000. After around 18 degrees, the residuals keep fluctuating and so do the Cl values. Even after increasing the AoA, the Cl values fluctuate at a high value and do not seem to drop, like how it is usually supposed to. Can anyone explain the problem with this? I have tried many types of mesh and still encounter the same problem. |
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| aerofoil, fluctuating residuals, naca 0018 |
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