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Old 08-28-2012, 08:38 PM   #37 (permalink)
arcosine
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You should use some updated air-foils instead of the 1930's Dymaxion cross section.

http://www.ae.illinois.edu/m-selig/a..._database.html

naca66-18 ( laminar flow airf0il)


http://www.desktop.aero/appliedaero/...ksections.html



I am searching the database for a thick airfoil:






Oh this applet is cool:

http://www.ppart.de/aerodynamics/profiles/NACA4.html
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Last edited by arcosine; 08-28-2012 at 09:15 PM..
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