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Showing results 1 to 1 of 1 Search took 0.00 seconds. Search: Posts Made By: MadsR

Forum: OpenFOAM September 13, 2010, 11:48

Replies: 19 liftDrag Views: 8,271 Posted By MadsR So for an airfoil with a chord of 1.0 and a span... So for an airfoil with a chord of 1.0 and a span of 0.5 you would set lRef = 1.0 Aref = 0.5 right? It would make sense since the lift and drag forces need the area and the corresponding...

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