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-   -   help for Naca 0015 in Gambit & Fluent !! (http://www.cfd-online.com/Forums/openfoam-meshing-other/80222-help-naca-0015-gambit-fluent.html)

rayyan53 September 19, 2010 16:50

help for Naca 0015 in Gambit & Fluent !!
 
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

sega September 20, 2010 03:34

Are you using Gambit / Fluent or OpenFOAM?
This it the OpenFOAM forum.

rayyan53 September 27, 2010 07:38

Naca 0015
 
Quote:

Originally Posted by sega (Post 275781)
Are you ?
This it the OpenFOAM forum.

i'm using Gambit / Fluent or OpenFOAM yes dear

kdrbrk October 27, 2010 02:26

did you define reference values correctly in fluent?


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