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Volumn 33, Issue 10-11, 2001, Pages 1055-1083

New developments in vibration reduction with actively controlled trailing edge flaps

Author keywords

Achieve control of vibrations; Archive control of blade vortex interaction (BVI); Vibration suppression in helicopter roters

Indexed keywords


EID: 0035810114     PISSN: 08957177     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0895-7177(00)00300-9     Document Type: Article
Times cited : (71)

References (33)
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  • 18
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  • 19
    • 0006095497 scopus 로고
    • L'Azione aerodinamica sul profilo oscillante in un fluido compressibile a velocita iposonora, (Also available as British Ministry of Aircraft Production R.T.P translation 987)
    • April
    • (1938) L' Aerotecnica , vol.18 , Issue.4
    • Possio, C.1
  • 24
    • 0020649648 scopus 로고
    • Formulation and solution of rotary-wing aeroelastic stability and response problems
    • (1983) Vertica , vol.7 , Issue.2 , pp. 101-141
    • Friedmann, P.P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.