Citation: | Xue Haifeng, Xiang Jinwu, Zhang Xiaoguet al. Coupled helicopter rotor/propulsion/transmission system torsional vibration analytical model and coupled influence investigation[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(05): 438-443. (in Chinese) |
[1] Twomey W J, Ham E H. Review of engine/airframe/drive train dynamic interface development problems . AD A057932, 1978 [2]Richardson D A, Alwang J H. Engine/airframe/drive train dynamic interface documentation . U.S. Army Res and Tech Labs, TR 78-11,1978 [3]Needham J F, Banerjee D. Engine/airframe/drive train dynamic interface documentation . U.S. Army Res and Tech Labs, TR 78-12,1978 [4]Bowes M A. Engine/airframe/drive train dynamic interface documentation . U.S.Army Res and Tech Labs,TR 78-14,1978 [5]Hanson H W, Edwards R D, Riley W W, et al. Engine/airframe/drive train dynamic interface documentation . U.S. Army Res and Tech Labs, TR 78-15,1978 [6]Warmbrodt W, Hull R. Development of a helicopter rotor/propulsion system dynamics analysis . AIAA Paper 82-1078,1982 [7]Thibert F, Maquin F. Dynamic behavior of transmission systems . In:European Rotorcraft Forum , 1982 [8]Hansford R E. Considerations in the development of the couples rotor fuselage model . In:American Helicopter Society 48th Annual National Forum .Washington D C, 1992
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