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

dc.contributor.author Chiu, T.
dc.contributor.author Friedmann, P.P.
dc.date.accessioned 2016-08-15T13:51:31Z
dc.date.available 2016-08-15T13:51:31Z
dc.date.issued 1996
dc.identifier.other ERF-1996-Vol1-11
dc.identifier.uri http://hdl.handle.net/20.500.11881/3216
dc.language.iso en
dc.title An analytical model for ACSR* approach to vibration reductin in a helicopter rotor/flexible fuselage system
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