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Old   March 4, 2000, 06:32
Default Windtunnel Experiment Data
Yap Wen Jiun
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I am a newcomer in this forum. I don't know this question has been asked before or not.

Where do I get the most accurate or fundamental windtunnel result for an airfoil (such as NACA 23012) so that I can compare to my CFD solutions (using PHOENICS).

For example, at Reynold number of 5 x 10+6, there will be different lift curve for NACA 23012 in different books. So there must be some kind of references. Please tell me.
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Old   March 5, 2000, 15:46
Default Re: Windtunnel Experiment Data
Ahmed Al-otaibi
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You can check in one of the famous books"Wing sections">>

I suggest you using NACA0012 section to validate your code..much more popular and data is available in most of journals and aerodynamics books.. hope you good luck..
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