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Volumn , Issue , 2011, Pages 241-250

Multiple input describing function for non-linear analysis of ground and air resonance

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC STABILITY; AIR RESONANCE; GROUND RESONANCE; LEAD-LAG; MULTIINPUT; MULTIPLE INPUTS; NON-LINEAR MODEL; NONLINEAR COMPONENTS; STABILITY ANALYSIS;

EID: 84861600049     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (3)

References (20)
  • 4
    • 0030195218 scopus 로고    scopus 로고
    • Analysis of bearingless main rotor aeroelasticity using an improved time domain nonlinear elastomeric damper model
    • F. Gandhi and I. Chopra. Analysis of bearingless main rotor aeroelasticity using an improved time domain nonlinear elastomeric damper model. Journal of the American Helicopter Society, 39:267-277, 1996. (Pubitemid 126599403)
    • (1996) Journal of the American Helicopter Society , vol.41 , Issue.3 , pp. 267-277
    • Gandhi, F.1    Chopra, I.2
  • 6
    • 0016115509 scopus 로고
    • An application of Floquet theory to prediction of mechanical instability
    • C. Hammond. An application of Floquet theory to prediction of mechanical instability. Journal of the American Helicopter Society, 19:14, 1974.
    • (1974) Journal of the American Helicopter Society , vol.19 , pp. 14
    • Hammond, C.1
  • 7
    • 0023994287 scopus 로고
    • CONSTRUCTION AND ANALYSIS OF A SIMPLIFIED NON-LINEAR GROUND RESONANCE MODEL
    • M. Janowski and B. Tongue. Construction and analysis of a simplified non-linear ground resonance model. Journal of Sound and Vibration, 122(2):233-241, 1988. (Pubitemid 18608956)
    • (1988) Journal of Sound and Vibration , vol.122 , Issue.2 , pp. 233-241
    • Janowski, M.D.1    Tongue, B.H.2
  • 10
    • 73649133316 scopus 로고    scopus 로고
    • Numerical evaluation of limit cycles of aeroelastic systems
    • M. Manetti, G. Quaranta, and P. Mantegazza. Numerical evaluation of limit cycles of aeroelastic systems. Journal of Aircraft, 46(5): 1759-1769, 2009.
    • (2009) Journal of Aircraft , vol.46 , Issue.5 , pp. 1759-1769
    • Manetti, M.1    Quaranta, G.2    Mantegazza, P.3
  • 15
    • 0022661228 scopus 로고
    • INFLUENCE OF NONLINEAR BLADE DAMPING ON HELICOPTER GROUND RESONANCE INSTABILITY
    • D. Tang and E. Dowell. Influence on nonlinear blade damping on helicopter ground resonance. Journal of Aircraft, 23:104-110, 1986. (Pubitemid 16486993)
    • (1986) Journal of Aircraft , vol.23 , Issue.2 , pp. 104-110
    • Tang, D.M.1    Dowell, E.H.2
  • 16
    • 0023089315 scopus 로고
    • Effects of non-linear damping in landing gear on helicopter limit cycle response in ground resonance
    • D. Tang and E. Dowell. Effects of non-linear damping in landing gear on helicopter limit cycle response in ground resonance. Journal of the American Helicopter Society, 1987.
    • (1987) Journal of the American Helicopter Society
    • Tang, D.1    Dowell, E.2
  • 18
    • 0021458506 scopus 로고
    • LIMIT CYCLE OSCILLATIONS OF A NONLINEAR ROTORCRAFT MODEL
    • B. Tongue. Limit cycle oscillations of a non-linear rotorcraft model. AIAA Journal, 22:967-974, 1984. (Pubitemid 14606900)
    • (1984) AIAA journal , vol.22 , Issue.7 , pp. 967-974
    • Tongue, B.H.1
  • 19
    • 0022161189 scopus 로고
    • Response of a rotorcraft with damping non-linearities
    • B. Tongue. Response of a rotorcraft with damping non-linearities. Journal of Sound and Vibration, 103:211-221, 1985.
    • (1985) Journal of Sound and Vibration , vol.103 , pp. 211-221
    • Tongue, B.1
  • 20
    • 0023561615 scopus 로고
    • Simulation and correlation of a helicopter air-oil strut dynamic response
    • St Louis, Missouri, May 18-20
    • W. Welsh. Simulation and correlation of a helicopter air-oil strut dynamic response. In 43rd AHS Annual Forum, pages 977-999, St Louis, Missouri, May 18-20 1987.
    • (1987) 43rd AHS Annual Forum , pp. 977-999
    • Welsh, W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.