Hi All,
I am looking for a some sugestions for a symetrical airfoil that I can
use on a 60" aerobatic slope plane. I figure on an 8" root, 6" tip
chord, and a 60" span. I think that the min. Reynolds # would be about
200,000 at landing speed. Other than that, I am considering a wingeron
design. I want it to be fast and have good inverted performance. It
seems that a design like this might be a good DS plane also.
I have alot of .dat and .cor files and also the ability to generate
NACA sections but I'm not really sure of what to look for in a
symetrical airfoil that would give me what I want.
Thanks,
Chris
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