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turbolent models for wings

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Old   July 18, 2000, 08:54
Default turbolent models for wings
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Maria Teresa Milesi
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Hi, I am studyng some NACA wings with Fluent 5.3, I've chosen k-e realizable models and the non equilibrium wall functions, I've found good results for Cl but I've some problems with Cd (the sperimental value is about 0.0055 and mine is 0.011). I tried also the RNG models with the differential viscosity models, I've found Cd=0.006 (a good value) but the distribution of velocity vectors is very strange (there is a distact in the end). Can you tell me which is the best turbulent models to use?
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