Optimizing tuning masses for helicopter rotor blade vibration reduction including computed airloads and comparison with test data
33rd Structures, Structural Dynamics and Materials Conference ; 1992 ; Dallas , TX , U.S.A.
01.01.1992
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
EFFECTS OF HELICOPTER ROTOR WAKE CHARACTERISTICS ON BLADE AIRLOADS
British Library Conference Proceedings | 2006
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