NACA0015 or aerofoil FLUENT 5 Model Help?
I am a final year MEng student carrying out a NACA0015 wing test with a rotating leading edge on the aerofoil. I wish to carry out CFD modelling using FLUENT 5 and Gambit and require input files/mesh files to gain an idea of how to set up this problem. Can anyone supply me with any of these files of a NACA0015 or any other wing section that has been modelled so I can gain an idea of how to set up this model.
My email is firstname.lastname@example.org
Thanks in advance.
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