A SIMPLIFIED METHOD OF DETERMINING VIBRATION FREQUENCY OF HELICOPTER ROTOR BLADES

被引:0
|
作者
TCHUIKO, AN
PAVLJUK, NI
SHANIN, IV
机构
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:64 / 66
页数:3
相关论文
共 50 条
  • [1] Smart Spring Control of Vibration on Helicopter Rotor Blades
    Oxley, Gregory
    Nitzsche, Fred
    Feszty, Daniel
    JOURNAL OF AIRCRAFT, 2009, 46 (02): : 692 - 696
  • [2] Overview of rotor blades optimum design for helicopter vibration reduction
    Xiang, J.W.
    Guo, J.X.
    Zhang, X.G.
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2001, 27 (01): : 32 - 35
  • [3] A MULTIDISCIPLINARY OPTIMIZATION APPROACH FOR VIBRATION REDUCTION IN HELICOPTER ROTOR BLADES
    CHATTOPADHYAY, A
    MCCARTHY, TR
    COMPUTERS & MATHEMATICS WITH APPLICATIONS, 1993, 25 (02) : 59 - 72
  • [4] MINIMUM WEIGHT DESIGN OF HELICOPTER ROTOR BLADES WITH FREQUENCY CONSTRAINTS
    CHATTOPADHYAY, A
    WALSH, JL
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1989, 34 (04) : 77 - 82
  • [5] MINIMUM DESIGN OF HELICOPTER ROTOR BLADES WITH FREQUENCY CONSTRAINTS - REPLY
    CHATTOPADHYAY, A
    WALSH, JL
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1990, 35 (02) : 69 - 69
  • [6] Effect of Uncertainty on Hub Vibration Response of Composite Helicopter Rotor Blades
    You, Young Hyun
    Jung, Sung Nam
    Pawar, Prashant A.
    Shin, Eui Sup
    JOURNAL OF AIRCRAFT, 2010, 47 (01): : 151 - 160
  • [7] OPTIMAL PLACEMENT OF TUNING MASSES FOR VIBRATION REDUCTION IN HELICOPTER ROTOR BLADES
    PRITCHARD, JI
    ADELMAN, HM
    AIAA JOURNAL, 1990, 28 (02) : 309 - 315
  • [8] Novel Controller Design Demonstration for Vibration Alleviation of Helicopter Rotor Blades
    Ulker, Fatma Demet
    Nitzsche, Fred
    ACTIVE AND PASSIVE SMART STRUCTURES AND INTEGRATED SYSTEMS 2012, 2012, 8341
  • [10] DYNAMICS OF HELICOPTER ROTOR BLADES
    MAGARI, PJ
    SHULTZ, LA
    MURTHY, VR
    COMPUTERS & STRUCTURES, 1988, 29 (05) : 763 - 776