-2.53* Ideal angle of attack +1.16* Robert Steinhaus wrote: > I would be grateful to find out if anyone knows the zero lift angle for the > S3010 airfoil. I would particularly be interested in experimental actual > wind tunnel values above computed estimates (Compufoil, etc.). I hope to use > S3010 on a wing tip operating at a reynolds number around 60,000. > Thanks! > ______________________________________________________ > Get Your Private, Free Email at http://www.hotmail.com > > RCSE-List facilities provided by Model Airplane News. Send "subscribe" and >"unsubscribe" requests to [EMAIL PROTECTED] -- Rich Border Marguerite Prunyi http://www.netlabs.net/hp/soarrich Those who pound their swords into plows will plow for those who did not. RCSE-List facilities provided by Model Airplane News. Send "subscribe" and "unsubscribe" requests to [EMAIL PROTECTED]
