Jean Claude
Junior Member
- Joined
- Jan 2, 2009
- Messages
- 2,646
- 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)
Q1, Q2: It is the speed difference (left / right) which produced the flapping angle. Not the position of the stick. The position of the stick lift rates by the average angle (i.e the axial component of Vo through the rotor)
Q3 Q4: The flapping angle is stabilized automatically: If> then the balance of lift decreases the angle. If <, then the balance of lift increases the angle. The flapping angle depends axial component of Vo, and RPM) . No possibility to hit the stops flapping, unless the retreating blade stalles (RPM too low and axial component of Vo too great
Q6 : fig 4 Yes , fig 5 No.
Jean Claude
Q3 Q4: The flapping angle is stabilized automatically: If> then the balance of lift decreases the angle. If <, then the balance of lift increases the angle. The flapping angle depends axial component of Vo, and RPM) . No possibility to hit the stops flapping, unless the retreating blade stalles (RPM too low and axial component of Vo too great
Q6 : fig 4 Yes , fig 5 No.
Jean Claude