| Subject: Prop blade twist distribution |
| From: Paul |
| Date: 4/5/2000, 8:26 AM |
Pine Pienaar wrote:
Hi Does the blade airfoil have anything to do with the blade twist distribution. ??? Anyone !! Pine Pienaar pine@cpro.co.za Lancair 360 #664
Somewhat. Depends on the camber of the blade. High camber blades generate higher lift coeff. at lower angles of attack. Paul Lamar The Aircraft Rotary Engine Newsletter. Powered by Linux. http://home.earthlink.net/~rotaryeng/ http://www.linux.org