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[Commercial meshers] help for Naca 0015 in Gambit & Fluent !! |
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September 19, 2010, 16:50
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help for Naca 0015 in Gambit & Fluent !!
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#1 |
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New Member
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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September 20, 2010, 03:34
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#2 |
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Senior Member
Sebastian Gatzka
Join Date: Mar 2009
Location: Frankfurt, Germany
Posts: 729
Rep Power: 20 |
Are you using Gambit / Fluent or OpenFOAM?
This it the OpenFOAM forum.
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Schrödingers wife: "What did you do to the cat? It's half dead!" |
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September 27, 2010, 07:38
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Naca 0015
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#3 | |
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New Member
Rayan
Join Date: Sep 2010
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Quote:
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October 27, 2010, 02:26
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#4 |
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Burak
Join Date: May 2009
Posts: 90
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did you define reference values correctly in fluent?
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