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Search: Posts Made By: Borjinho
Forum: FLUENT June 27, 2013, 21:18
Replies: 1
Views: 1,340
Posted By Borjinho
cd and cl parameters

I am simulating Naca 0012 airfoil in 2D with with 10 degrees of angle of attack. I donīt know where I have to check the values obtained for cl and cd. In the picture attached I show where I am...
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