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Need Cl,Cd for high angles of attack

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Old   October 18, 2013, 07:07
Default Need Cl,Cd for high angles of attack
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dynamic
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Hi
I am a final year student working on numerical modelling of Darrieus turbine. I require Cl,Cd as a function of angle of attack for angles - 0 to 60 deg. Can you please direct me to a source where I can find experimental/any reliable Cl Cd values for some symmetric NACA profiles.
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Old   October 23, 2013, 14:44
Default UIUC airfoil database
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Muhammad Maaz Siddiqui
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http://aerospace.illinois.edu/m-seli..._database.html
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Old   October 24, 2013, 01:01
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Thanks for replying But I want Cl, Cd values of NACA airfoils for angles of attack 0-60 deg but I am finding results only for angles till 20deg and very few for NACA...Can u help?
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