Rotor damping analysis based on helicopter dynamic requirement with rotor/fuselage coupling
JOURNAL- BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS ; 37 , 9 ; 1147-1150
2011-01-01
4 pages
Article (Journal)
Unknown
DDC: | 629.4 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Unsteady Helicopter Rotor: Fuselage Interaction Analysis
NTIS | 1988
|Coupling technique of rotor-fuselage dynamic analysis
Tema Archive | 1983
|Helicopter Fuselage Vibrations Induced by the Rotor
British Library Conference Proceedings | 1996
|