|October 1, 2013, 06:23||
Negative Drag on Airfoil
Join Date: May 2013
Location: South Africa
Posts: 32Rep Power: 4
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?
|airfoil, ansys, lift, negative drag|
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