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Member
Jason
Join Date: May 2013
Location: South Africa
Posts: 32
Rep Power: 14 ![]() |
I am getting relatively accurate Lift measurements but my drag values are all negative for my airfoil.
I have tried a number of turbulence models and all give the negative drag. I have obtained some form of mesh independence by using the Adapt Gradient tools. I think I might have a problem with my reference values? Does anyone know how I could change my coordinate system? |
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Tags |
airfoil, ansys, lift, negative drag |
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