Can anybody help me obtain the CL and CD vs alpha for a standard NACA 0015 aerofoil section? I am in my final year of study at university and require this information for my final year thesis but cannot track it down on ESDU etc. Have heard of a book called Theory of Wing Sections but cannot track it down.

Any help or info from this book would be much appreciated.

Cheers

I think you can find some information on: http://www.engr.utk.edu/~rbond/airfoil.html

Regards MATEUS

Thanks but I require a specific aerofoil section namely a NACA 0015. Can anyone help?!!

Hi,

Got the data you require; will email it to you when i have scanned it.

Jim

Cheers. You are a lifesaver!