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Volumn , Issue , 2001, Pages

Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS;

EID: 85067319807     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1433     Document Type: Conference Paper
Times cited : (3)

References (9)
  • 1
    • 0029346745 scopus 로고
    • Vibration Reduction in Rotorcraft Using Active Control: A Comparison of Various Approaches
    • July-August
    • Friedmann, P.P., and Millot, T.A., Vibration Reduction in Rotorcraft Using Active Control: A Comparison of Various Approaches, Journal of Guidance, Control, and Dynamics, Vol.18, No.4, July-August 1995.
    • (1995) Journal of Guidance, Control, and Dynamics , vol.18 , Issue.4
    • Friedmann, P.P.1    Millot, T.A.2
  • 7
    • 0029723297 scopus 로고    scopus 로고
    • An Accelerometer-Based Instrumentation System for Measurement of Helicopter Rotor Motion and Loads
    • Washington, D.C., June 4-6
    • McKillip, R.M., An Accelerometer-Based Instrumentation System for Measurement of Helicopter Rotor Motion and Loads, Proceedings of the American Helicopter Society 52nd Annual Forum, Washington, D.C., June 4-6, 1996.
    • (1996) Proceedings of the American Helicopter Society 52nd Annual Forum
    • McKillip, R.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.