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Volumn 49, Issue 3, 2004, Pages 250-270

Performance analysis of a utility helicopter with standard and advanced rotors

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AIRFRAMES; CALCULATIONS; COMPUTER SIMULATION; DRAG; FLIGHT DYNAMICS; FUSELAGES; HELICOPTER ROTORS; PERFORMANCE; TURBOMACHINE BLADES;

EID: 4344606344     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.49.250     Document Type: Article
Times cited : (131)

References (11)
  • 4
    • 0034296927 scopus 로고    scopus 로고
    • The effects of control system stiffness models on the dynamic stall behavior of a helicopter
    • October
    • Kufeld, R. M., and Johnson, W., "The Effects of Control System Stiffness Models on the Dynamic Stall Behavior of a Helicopter," Journal of the American Helicopter Society, Vol. 45, (4), October 2000.
    • (2000) Journal of the American Helicopter Society , vol.45 , Issue.4
    • Kufeld, R.M.1    Johnson, W.2
  • 5
    • 4344635803 scopus 로고
    • YUH-60A/T700 IR Suppressor Full Scale Prototype Test Report by Bernard, R., SER 70094, Appendix III, Sikorsky Aircraft, April
    • Flemming, R. J., and Rorke, J. B., "UH-60A Quarter Scale Infrared Suppressor Wind Tunnel Tests," YUH-60A/T700 IR Suppressor Full Scale Prototype Test Report by Bernard, R., SER 70094, Appendix III, Sikorsky Aircraft, April 1977.
    • (1977) UH-60A Quarter Scale Infrared Suppressor Wind Tunnel Tests
    • Flemming, R.J.1    Rorke, J.B.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.