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Turbulance Model for Prediction of Stall Characteristics |
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August 11, 2022, 05:46
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Turbulance Model for Prediction of Stall Characteristics
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Join Date: Aug 2022
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Hello.,
I'm trying to simulate the model between the range of RE = 3.5E-05 to 4.5E-05. I tried k-omega SST model with y+ of 30 for the velocity range of 25-35 m/s and Ange attack of -10 to 20 with the step of 5. But some reference discussions preferred k-epsilon with Grid independent studies. As per my knowledge, K-omega also uses the base scheme as k-epsilon in addition to wall functions. Is it preferable to use k-omega(which basically captures adverse pressure gradient)at higher angle of attack to validate CL, CD and CM ? Thank you.. Last edited by KDG; August 12, 2022 at 02:55. |
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| cfd aerospace, low re, stall angle, turbule model |
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