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December 24, 2005, 00:29
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how to model a NACA0012 aerofoil in GAMBIT
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Guest
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As I'm doing my project on Turbulent pitching past NACA0012 Aerofoil, using 3D-URANS code, at NAL, I would like to do the same using FLUENT, for comparison purpose, so kindly can anyone help to start up my things right, Thanks in advance...
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January 5, 2006, 12:22
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Re: how to model a NACA0012 aerofoil in GAMBIT
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Guest
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a good tutorial about that is given in fluent tutorials, u can find them at www.fluentusers.com
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January 6, 2006, 02:56
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Re: CFD analysis of an aerofoil
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Guest
Posts: n/a
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Hi i am going to begin my master project on CFD analysis of an aerofoil using finite element collocated grid method. It is based upon the assumption of a half aerofoil and half cylinder problem. I am having problems concerning the boundary conditions for the subject under investigation. Kindly help me on this. I would be greatly obliged if anyone can offer solution to my problem
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