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Volumn 33, Issue 10-11, 2001, Pages 1055-1083
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New developments in vibration reduction with actively controlled trailing edge flaps
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Author keywords
Achieve control of vibrations; Archive control of blade vortex interaction (BVI); Vibration suppression in helicopter roters
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Indexed keywords
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EID: 0035810114
PISSN: 08957177
EISSN: None
Source Type: Journal
DOI: 10.1016/S0895-7177(00)00300-9 Document Type: Article |
Times cited : (71)
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References (33)
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