Influence of the number of rotor blades on helicopter active vibration reduction potential
Influence of the number of rotor blades on helicopter active vibration reduction potential
dc.contributor.author | Mannchen, T. | |
dc.contributor.author | Well, K.H. | |
dc.date.accessioned | 2016-06-29T16:51:13Z | |
dc.date.available | 2016-06-29T16:51:13Z | |
dc.date.issued | 2002 | |
dc.identifier.other | ERF200281 | |
dc.identifier.uri | http://hdl.handle.net/20.500.11881/456 | |
dc.language.iso | en | |
dc.subject.other | Dynamics | |
dc.title | Influence of the number of rotor blades on helicopter active vibration reduction potential |
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