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Search: Posts Made By: thinkagain
Forum: OpenFOAM Running, Solving & CFD November 23, 2011, 19:42
Replies: 0
Views: 1,619
Posted By thinkagain
DRAG coefficient prediction

Hello

I'm trying to determinate the polars for an airfoil 2D and I created a test case with a NACA 0012 on openFOAM 2.0.1

I obtained very good value for lift and moment coefficient, while the...
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