It is shown that possibility exists of improving both damping and static stability of helicopter by relatively minor modification of blade mass and aerodynamic characteristics, together with use of spring and viscous restraint in control system.
Method for improving inherent stability and control characteristics of helicopters
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 17 , n 6
1950
12 pages
Aufsatz (Zeitschrift)
Englisch
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Inherent Stability of Helicopters
NTRS | 1923
|The case for inherent stability of helicopters
NTRS | 1966
|The Case for Inherent Stability of Helicopters
NTIS | 1966
|The case for inherent stability of helicopters
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|Control and stability of helicopters
Engineering Index Backfile | 1949
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