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Old   February 9, 2011, 00:54
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Gerardo Montano Uzcátegui
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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
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Old   February 9, 2011, 01:32
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Abbott - Theory of Wing sections
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Old   February 9, 2011, 15:10
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Gerardo Montano Uzcátegui
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Thank´s, i really appreciate that reference, please if someone knows another page or book i will return the favor.
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Old   February 14, 2011, 12:09
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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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