sbav8r
I do deny them my essence
- Joined
- Mar 10, 2003
- Posts
- 185
I'm not following you on the power setting for load factor thing. I could see a power setting for various maneuvers, but for G's. The amount of available load factor will be a factor of airspeed. Granted power settings will control airspeed, but having fixed power settings for G's just doesn't make sense to me. During aerobatics the exchange of potential and kinetic energy (altitude and airspeed) will be varying widely. One power setting would certainly not protect the aircraft from over stress in a straight dive compared to the same aircraft at straight and level. It just seems to me that using the markings for G's would only work in one pitch attitude. Everything above or below that pitch attitude would change the airspeed and therefore the amount of available G's.
Example: 2200 RPM at straight and level produces about 120 kts. At 120 kts I coulld briefly pull 6 G's, anything above that would increase the angle of attack beyond the critical angle of attack and the wing would stall. If I took the same aircraft in the same power setting, except this time, I put it in a dive. That same power setting would now produce much more airspeed and therefore have more available G's. It could overstress the airframe if the aircraft can't handle a structural load limit of more then 6 G's. Same power settings on both, but due to the changes in potentail energy for kinetic energy, the aircraft can now very easily exceed 6 G's.
Example: 2200 RPM at straight and level produces about 120 kts. At 120 kts I coulld briefly pull 6 G's, anything above that would increase the angle of attack beyond the critical angle of attack and the wing would stall. If I took the same aircraft in the same power setting, except this time, I put it in a dive. That same power setting would now produce much more airspeed and therefore have more available G's. It could overstress the airframe if the aircraft can't handle a structural load limit of more then 6 G's. Same power settings on both, but due to the changes in potentail energy for kinetic energy, the aircraft can now very easily exceed 6 G's.