Attention drawn to powerful influence of Coriolis forces and flapping pin offset on stability; for conventional rotor of small offset, damping in pitch and flight stability are greatly reduced by absence of drag hinges.
Helicopter stability in hovering flight
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 59 , n 537
1955
6 pages
Aufsatz (Zeitschrift)
Englisch
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Helicopter control and stability in hovering flight
Engineering Index Backfile | 1948
|Helicopter hovering performance
Engineering Index Backfile | 1949
|