APPLICATION OF THE LIFTING LINE CONCEPT TO HELICOPTER BLADE COMPUTATION

被引:0
|
作者
COSTES, JJ
机构
来源
RECHERCHE AEROSPATIALE | 1978年 / 06期
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:355 / 364
页数:10
相关论文
共 50 条
  • [1] PRESSURE DISTRIBUTION COMPUTATION ON A NON-LIFTING SYMMETRICAL HELICOPTER BLADE IN FORWARD FLIGHT
    CHATTOT, JJ
    PHILIPPE, JJ
    RECHERCHE AEROSPATIALE, 1980, (05): : 317 - 330
  • [2] LIFTING LINE THEORY OF A HELICOPTER ROTOR
    ISAY, WH
    ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1969, 49 (09): : 533 - &
  • [3] APPLYING THE LIFTING SURFACE METHOD TO THE BLADE TIP OF A HOVERING HELICOPTER
    ISSER, A
    ROSEN, A
    COMPUTERS & MATHEMATICS WITH APPLICATIONS, 1989, 17 (11) : 1455 - 1466
  • [4] EXTENSION OF LIFTING LINE MODEL FOR HELICOPTER ROTOR
    HILLE, R
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1975, 23 (03): : 77 - 95
  • [5] Extension of the Lifting Line Model for the Helicopter Rotor.
    Hille, Ralf
    Zeitschrift fuer Flugwissenschaften, 1975, 23 (03): : 77 - 95
  • [6] Computation of dynamic response of helicopter blade under bird impact
    Lin, Chang-Liang
    Wang, Yi-Feng
    Wang, Hao-Wen
    Chen, Ren-Liang
    Shang, Xiao-Dong
    Zhendong yu Chongji/Journal of Vibration and Shock, 2013, 32 (10): : 62 - 68
  • [7] APPLICATION OF A LIFTING SURFACE THEORY FOR A HELICOPTER IN FORWARD FLIGHT
    RUNYAN, HL
    TAI, H
    VERTICA, 1986, 10 (3-4): : 269 - 280
  • [8] Helicopter blade droop as an application of simple beam theory
    Shayak, B.
    EUROPEAN JOURNAL OF PHYSICS, 2019, 40 (02)
  • [9] APPLICATION OF OPTIMIZATION METHODS TO HELICOPTER ROTOR BLADE DESIGN
    CHATTOPADHYAY, A
    WALSH, JL
    STRUCTURAL OPTIMIZATION, 1990, 2 (01): : 11 - 22
  • [10] A novel smart spring concept for helicopter blade vibration and noise suppression
    Yong, C
    Wickramasinghe, VK
    Zimcik, DG
    PRICM 5: THE FIFTH PACIFIC RIM INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS AND PROCESSING, PTS 1-5, 2005, 475-479 : 2095 - 2098