THE nature of the instability of helicopters is described here by Mr. Kelley, who also enumerates factors that contribute to it.Two of Arthur M. Young's early attempts to solve the problem are discussed by the author, who states that the final solution is a device that makes model helicopters perfectly stable in flight.The application of this device to full-scale helicopters is also described.
HELICOPTER STABILITY with Young's Lifting Rotor
Sae Technical Papers
Pre-1964 SAE Technical Papers ; 1906
1945-01-01
Aufsatz (Konferenz)
Englisch
Helicopter stability with Young's lifting rotor
Engineering Index Backfile | 1945
|Non-linear helicopter rotor lifting surface theory
Tema Archiv | 1974
|Rotor Dynamics and Helicopter Stability
Emerald Group Publishing | 1964
|Rotor Dynamics and Helicopter Stability
Emerald Group Publishing | 1964
|Rotor Dynamics and Helicopter Stability
Emerald Group Publishing | 1963
|