FLUTTER OF A HELICOPTER ROTOR BLADE IN FORWARD FLIGHT

被引:4
|
作者
STAMMERS, CW
机构
来源
AERONAUTICAL QUARTERLY | 1970年 / 21卷
关键词
D O I
10.1017/S0001925900005217
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:18 / &
相关论文
共 50 条
  • [11] A COMPARISON OF THE CALCULATED AND OBSERVED FLUTTER CHARACTERISTICS OF A HELICOPTER ROTOR BLADE
    GOLAND, L
    PERLMUTTER, AA
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (04): : 281 - &
  • [12] Wake structure of a helicopter rotor in forward flight
    Briassulis, G.
    Andreopoulos, J.
    Journal of Aircraft, 1993, 30 (04): : 459 - 466
  • [13] Numerical Research on the Unsteady Evolution Characteristics of Blade Tip Vortex for Helicopter Rotor in Forward Flight
    Zhou Ye
    Fengjiang Zhan
    Guohua Xu
    International Journal of Aeronautical and Space Sciences, 2020, 21 : 865 - 878
  • [15] Numerical Research on the Unsteady Evolution Characteristics of Blade Tip Vortex for Helicopter Rotor in Forward Flight
    Ye, Zhou
    Zhan, Fengjiang
    Xu, Guohua
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 21 (04) : 865 - 878
  • [16] Effects of rotor blade icing on helicopter flight performance
    Xu Y.-M.
    Lü S.-J.
    Cao Y.-H.
    Chen R.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2016, 31 (02): : 399 - 404
  • [17] Periodic flap control of a helicopter blade in forward flight
    Pandiyan, R
    Sinha, SC
    JOURNAL OF VIBRATION AND CONTROL, 1999, 5 (05) : 761 - 777
  • [18] CHAOTIC STALL RESPONSE OF HELICOPTER ROTOR IN FORWARD FLIGHT
    TANG, DM
    DOWELL, EH
    JOURNAL OF FLUIDS AND STRUCTURES, 1992, 6 (03) : 311 - 335
  • [19] Technical note aerodynamic design of helicopter rotor blade in forward flight using response surface methodology
    Sun, HS
    Kim, YS
    Lee, SG
    Lee, DH
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2003, 48 (04) : 300 - 304
  • [20] Helicopter rotor blade optimum design for multiple flight conditions
    Chang, Y.K.
    Wang, Y.-R.
    Hung, C.-C.
    Transactions of the Aeronautical and Astronautical Society of the Republic of China, 1997, 29 (03): : 227 - 237