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help for Naca 0015 in Gambit & Fluent !!

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Old   September 19, 2010, 16:50
Default help for Naca 0015 in Gambit & Fluent !!
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Rayan
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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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Old   September 20, 2010, 03:34
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Are you using Gambit / Fluent or OpenFOAM?
This it the OpenFOAM forum.
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Old   September 27, 2010, 07:38
Default Naca 0015
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Quote:
Originally Posted by sega View Post
Are you ?
This it the OpenFOAM forum.
i'm using Gambit / Fluent or OpenFOAM yes dear
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Old   October 27, 2010, 02:26
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did you define reference values correctly in fluent?
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