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Revered flow for lower angles of attack range |
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May 22, 2022, 08:12 |
Revered flow for lower angles of attack range
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Ankit Kumawat
Join Date: Dec 2021
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I was performing simulations on NACA0003 airfoil at a Reynold number of 1e05 with the k-w SST turbulence model. The simulations are running perfectly fine for high angles of attack(>8 degrees) but it is showing a reversed flow for low angles of attack range. I have tried doing grid refinement as well but nothing worked. Any idea why is this happening? (Domain size: 10c both in the streamwise and crosswise direction; BC: Velocity inlet, Pressure outlet)
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