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[Commercial meshers] help for Naca 0015 in Gambit & Fluent !! |
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September 19, 2010, 16:50 |
help for Naca 0015 in Gambit & Fluent !!
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Rayan
Join Date: Sep 2010
Posts: 2
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HI Everybody I used Gambit and Fluent for naca 0015 to find CL at angle of attack 6 deg but the result was wroung and its comes about CL= 0.008 and the correct one is 0.7 and i dont know where the problem is. can anyone help us how to find lift coffiecient for NACA 0015 by using Gambit and Fluent ???? Thank u
Rayan |
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