An analytical model for ACSR* approach to vibration reductin in a helicopter rotor/flexible fuselage system

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dc.contributor.authorChiu, T.
dc.contributor.authorFriedmann, P.P.
dc.date.accessioned2016-08-15T13:51:31Z
dc.date.available2016-08-15T13:51:31Z
dc.date.issued1996
dc.identifier.otherERF-1996-Vol1-11
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3216
dc.language.isoen
dc.titleAn analytical model for ACSR* approach to vibration reductin in a helicopter rotor/flexible fuselage system

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