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Volumn 21, Issue 4, 2006, Pages 700-705

Analysis and control of transient aero-elastic response of teetering rotor on the shipboard

Author keywords

Aero elastic response; Aerospace propulsion system; Control method; Shipboard; Teetering rotor

Indexed keywords

FUSELAGES; INSTALLATION; PROPULSION; ROTATION; ROTORS; SPEED; TRANSIENTS;

EID: 33750422643     PISSN: 10008055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (2)

References (12)
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  • 2
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    • Chinese source
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    • The verification of a theoretical helicopter rotor blade sailing method by means of windtunnel testing
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    • Aeroelastic analysis of transient blade dynamics during shipboard engage/disengage operations
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    • Geyer, W.P.1    Smith, E.C.2    Keller, J.A.3
  • 5
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    • Analysis and control of the transient aeroelastic response of rotors during shipboard engagement and disengagement operations
    • Pennsylvania State University
    • Keller J A. Analysis and control of the transient aeroelastic response of rotors during shipboard engagement and disengagement operations[D]. Pennsylvania State University: 2001.
    • (2001)
    • Keller, J.A.1
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    • Modeling and simulation of rotor engagement and disengagement during shipboard operations
    • Maryland: Baltimore
    • Hao Kang, Chengjian He. Modeling and simulation of rotor engagement and disengagement during shipboard operations[C]. Proceedings of the American Helicopter Society 60th Annual Forum, Maryland: Baltimore, 2004.
    • (2004) Proceedings of the American Helicopter Society 60th Annual Forum
    • Kang, H.1    He, C.2
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  • 10
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    • Aeroelastic response and stability of helicopter rotor blades in forward flight
    • Wang Haowen, Gao Zheng, Zheng Zhaochang. Aeroelastic response and stability of helicopter rotor blades in forward flight[J]. Journal of Vibration Engineering, 1999, 12(4): 521-528.
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  • 11
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  • 12
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    • Wang, H.1    Gao, Z.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.