Jean Claude
Junior Member
- Joined
- Jan 2, 2009
- Messages
- 2,182
- Location
- Centre FRANCE
- Aircraft
- I piloted gliders C800, Bijave, C 310, airplanes Piper J3 , PA 28, Jodel D117, DR 220, Cessna 150, C
- Total Flight Time
- About 500 h (FW + ultra light)
Its rudder has a very low effect, not only because of the small surface area, but also because extended by the fuselage over almost the entire height, the center of pressure is moved very far in front of the hinge. Unfortunate effect discovered around 1927 on Couzinet aircraft
In spite of this, the designer could have placed the passenger's feet under the heavy engine, and the pilot's feet on either side of the passenger's buttocks. This could help to reduce the yaw inertia
The tank located far in front of the center of thrust of the rotor would probably have significantly modified the pitch balance depending on the remaining amount .
In spite of this, the designer could have placed the passenger's feet under the heavy engine, and the pilot's feet on either side of the passenger's buttocks. This could help to reduce the yaw inertia
The tank located far in front of the center of thrust of the rotor would probably have significantly modified the pitch balance depending on the remaining amount .