Equations of motion developed by R.P.COLEMAN evaluated for particular configuration and large number of different combinations of rotor and fuselage damping; results, displayed graphically, reveal dependence of unstable range on rotor and fuselage damping; ground resonance stated to be stability problem, closely analogous to problem of flutter.
Helicopter ground resonance
Aircraft Eng
Aircraft Engineering ; 31 , n 360
1959
8 pages
Aufsatz (Zeitschrift)
Englisch
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