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2d Fluent and Airfoil

Thread starter SkyEng
Start date Feb 25, 2004

Status: Not open for further replies.

Feb 25, 2004

SkyEng

New member

Hi everyone,

I need to make some visous calculations on Fluent (Cl, Cd, Cm, Cp) for an NACA 0012 type airfoil and I would like to know which geometry coul be the most apropriate for your opinion between, C, O and H and moreover which type of structure (unstructured, algebric, hyperbolic or elliptic).

if you have done such type of simulation before and if you have some tips to get better results modifying the settings please let me know...

Thanks