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Search: Posts Made By: madad2005
Forum: OpenFOAM Running, Solving & CFD December 5, 2008, 09:02
Replies: 7
Views: 4,732
Posted By madad2005
"- if the airfoil is on 0deg a

"- if the airfoil is on 0deg and your inlet-stream is 3 degrees angle of attack, then you also need to correct the lift-drag vector in the controlDict (or afterwards divide by cos(alpha) ) "
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