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Old December 7th 09, 10:21 PM posted to rec.aviation.homebuilt
Jim Logajan
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Posts: 1,958
Default NACA profile calculations

jan olieslagers wrote:
And also, less poignant but still:
How do I calculate from the basic parameters the behaviour of the
profile, i.e. the Cl curves? And perhaps other nice info like the
leading edge diameter?

Generally: any pointers to in-depth information that a non-engineer can
mentally digest?


Have you checked out some of the links at CFD Online:

http://www.cfd-online.com/

In particular, they have links to various software around the web:

http://www.cfd-online.com/Links/