Lagrangian formulation for the rapid estimation of helicopter rotor blade vibration characteristics

被引:0
|
作者
机构
[1] Goulos, I.
[2] Pachidis, V.
[3] Pilidis, P.
来源
| 1600年 / Royal Aeronautical Society卷 / 118期
关键词
D O I
10.1017/S000192400000960X
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [31] The phenomenon of helicopter rotor blade sailing
    Newman, S
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 1999, 213 (G6) : 347 - 363
  • [32] HELICOPTER ROTOR-BLADE INJURIES
    KIEL, FW
    AEROSPACE MEDICINE, 1965, 36 (07): : 668 - &
  • [33] SPECIAL VORTICES AT A HELICOPTER ROTOR BLADE
    MULLER, RHG
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1990, 35 (04) : 16 - 22
  • [34] Failure of a helicopter main rotor blade
    Amura, Mikael
    Aiello, Lorenzo
    Colavita, Mario
    De Paolis, Fabrizio
    Bernabei, Manuele
    20TH EUROPEAN CONFERENCE ON FRACTURE, 2014, 3 : 726 - 731
  • [35] Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
    Ozgumus, Ozge Ozdemzr
    Kaya, Metin O.
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2007, 79 (02): : 177 - 183
  • [36] Analysis of loading tail sections of helicopter main rotor blade and their influence on elastic blade characteristics
    Liss, AY
    Ismagilov, AN
    IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA, 1999, (03): : 16 - 19
  • [37] Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: part II. Results of flutter stability and vibration analysis of a hingeless helicopter blade in hover
    Ozgumus, Ozge Ozdemir
    Kaya, Metin O.
    AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2007, 79 (03): : 231 - 237
  • [38] HELICOPTER ROTOR VIBRATION ISOLATION
    DESJARDINS, RA
    HOOPER, WE
    VERTICA, 1978, 2 (02): : 145 - 159
  • [39] OPTIMIZING TUNING MASSES FOR HELICOPTER ROTOR BLADE VIBRATION REDUCTION AND COMPARISON WITH TEST DATA
    PRITCHARD, JI
    ADELMAN, HM
    WALSH, JL
    WILBUR, ML
    JOURNAL OF AIRCRAFT, 1993, 30 (06): : 906 - 910
  • [40] Structurally coupled characteristics of rotor blade geometrically exact formulation
    Jie WU
    Yijiang MA
    Zhidong WANG
    Zhihao YU
    Chinese Journal of Aeronautics, 2022, 35 (06) : 186 - 197