COMPUTATION OF TRANSONIC FLOW ABOUT HELICOPTER ROTOR BLADES

被引:2
|
作者
ARIELI, R
TAUBER, ME
SAUNDERS, DA
CAUGHEY, DA
机构
[1] NASA, AMES RES CTR, MOFFETT FIELD, CA 94035 USA
[2] INFORMAT GEN CORP, PALO ALTO, CA USA
[3] CORNELL UNIV, ITHACA, NY 14853 USA
关键词
CENTRIFUGAL FORCES - COMPUTER CODES - CORIOLIS FORCES - HELICOPTER ROTOR BLADES - ROT22 FLOW CODE;
D O I
10.2514/3.9338
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:722 / 727
页数:6
相关论文
共 50 条
  • [41] Damage detection for helicopter rotor blades in operative conditions
    Corbelli, A
    Mastroddi, F
    Gennaretti, M
    NOISE AND VIBRATION ENGINEERING, VOLS 1 - 3, PROCEEDINGS, 2001, : 179 - 186
  • [42] Stabilizing helicopter rotor blades using delayed feedback
    Krodkiewski, JM
    Faragher, JS
    ACTIVE CONTROL IN MECHANICAL ENGINEERING, 2000, : 191 - 202
  • [43] Dynamic model of elastic impact of helicopter rotor blades
    Wang, Yi-Feng
    Wang, Hao-Wen
    Gao, Zheng
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (09): : 2046 - 2050
  • [44] Composite technology development based on helicopter rotor blades
    Kozaczuk, Konrad Jerzy
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2020, 92 (03): : 273 - 284
  • [45] INTEGRATED AERODYNAMIC DYNAMIC OPTIMIZATION OF HELICOPTER ROTOR BLADES
    CHATTOPADHYAY, A
    WALSH, JL
    RILEY, MF
    AIAA/ASME/ASCE/AHS/ASC 30TH STRUCTURES, STRUCTURAL DYNAMICS AND MATERIALS CONFERENCE, PTS 1-4: A COLLECTION OF TECHNICAL PAPERS, 1989, : 946 - 958
  • [46] Noise Reduction of Helicopter Rotor Blades by Using Spoiler
    Islam, M. T.
    Rabbi, M. S.
    Uddin, M. S.
    8TH BSME INTERNATIONAL CONFERENCE ON THERMAL ENGINEERING, 2019, 2121
  • [48] DESIGN OF HELICOPTER ROTOR BLADES FOR OPTIMUM DYNAMIC CHARACTERISTICS
    PETERS, DA
    ROSSOW, MP
    KORN, A
    KO, T
    COMPUTERS & MATHEMATICS WITH APPLICATIONS-PART A, 1986, 12 (01): : 85 - 109
  • [49] EQUIVALENT G/E OF HELICOPTER ROTOR BLADES - REPLY
    HODGES, DH
    AIAA JOURNAL, 1983, 21 (03) : 479 - 480
  • [50] Automatic shearography inspection system for helicopter rotor blades
    Walz, T
    Ettemeyer, A
    NONDESTRUCTIVE EVALUATION OF AGING AIRCRAFT, AIRPORTS, AND AEROSPACE HARDWARE II, 1998, 3397 : 187 - 192