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Old December 8th 09, 12:00 AM posted to rec.aviation.homebuilt
Brian Whatcott
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Posts: 915
Default NACA profile calculations

jan olieslagers wrote:
/snip/
I think you would be best served by a 2-D flow visualizer of which
there are several out there. I don't think hand computation of
reasonable values for lift n drag are reasonable objectives.


/snip/
As for the flow visualisers: I'll be grateful for a suggestion of one I
can run from the Linux command line.

Thanks again,
KA


I tried an early version of Drela's Xfoil. It is available now in
several suitable flavors he
http://web.mit.edu/drela/Public/web/xfoil/

Can't remember whether these distributions include the data for the many
foils held by U.Illinois. Probably do?

Brian W