| Subject: Shifting gears. |
| From: Paul |
| Date: 2/5/2000, 8:44 PM |
Opps. That should be further down on the right side of the lift to drag curve. As RPM increases with a fixed pitch prop at a given speed the angle attack of the blades increase. The drag shoots up faster than the lift so the efficiency of the prop is reduced. Paul Lamar The Aircraft Rotary Engine Newsletter. Powered by Linux. http://home.earthlink.net/~rotaryeng/ http://www.linux.org