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gerardo3105 February 9, 2011 00:54

CFD Fluent Question
Hi everyone, im doing a Tesis with a NACA 0015 airfoil, and im studing the lift and drag coefficients, i need in my objectives comparate a grafic Cl vs angle of attack, and the same thing with the drag coefficient, i need a suport grafic to comparate my experimental results with the theoretical, who knows a page or something that contains this data? please! thanks

DoHander February 9, 2011 01:32

Abbott - Theory of Wing sections

gerardo3105 February 9, 2011 15:10

Thank´s, i really appreciate that reference, please if someone knows another page or book i will return the favor. :)

yossarian88 February 14, 2011 12:09

That is the kind of thing you should easily be able to find in the above mentioned book.

Otherwise, google is your friend.

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