Influence of the number of rotor blades on helicopter active vibration reduction potential

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dc.contributor.authorMannchen, T.
dc.contributor.authorWell, K.H.
dc.date.accessioned2016-06-29T16:51:13Z
dc.date.available2016-06-29T16:51:13Z
dc.date.issued2002
dc.identifier.otherERF200281
dc.identifier.urihttp://hdl.handle.net/20.500.11881/456
dc.language.isoen
dc.subject.otherDynamics
dc.titleInfluence of the number of rotor blades on helicopter active vibration reduction potential

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