Rotor damping analysis based on helicopter dynamic requirement with rotor/fuselage coupling
JOURNAL- BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS ; 37 , 9 ; 1147-1150
01.01.2011
4 pages
Aufsatz (Zeitschrift)
Unbekannt
DDC: | 629.4 |
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Unsteady Helicopter Rotor: Fuselage Interaction Analysis
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