Analysis of the computational method and the helicopter blade characteristics with coupled rigid and elastic motions

被引：0
|
作者：
National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China [1 ]
不详 [2 ]
机构：
来源：
Hangkong Dongli Xuebao | 2006年 / 1卷 / 36-40期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [1] 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
  • [2] Nonlinear Helicopter Rigid-Elastic Coupled Modeling with Its Applications on Aeroservoelasticity Analysis
    Wang, Luofeng
    Chen, Renliang
    AIAA JOURNAL, 2022, 60 (01) : 102 - 112
  • [3] Response calculation method for the rotor blade with arbitrary rigid motions
    Wang, Hao-Wen
    Han, Dong
    Gao, Zheng
    Zhendong Gongcheng Xuebao/Journal of Vibration Engineering, 2006, 19 (01): : 46 - 50
  • [4] Determination of Elastic Characteristics of the Helicopter Blade Attachment Based on the Strength Tests Results
    Kostin V.A.
    Garaev A.M.
    Kostin, V.A. (vakostin@mail.ru), 1600, Pleiades journals (64): : 800 - 804
  • [5] Rigid-elastic coupled flight dynamic modeling and air resonance stability analysis for heavy lift helicopter
    Wang L.
    Chen R.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2021, 42 (12):
  • [6] Computational method for elastic contact near rigid inclusion
    Fujimoto, K
    Stronge, WJ
    COMPUTATIONAL METHODS IN CONTACT MECHANICS IV, 1999, : 153 - 162
  • [7] Finite element method analysis of rotating blade with consideration of the coupling of rigid body motion and elastic motion
    2000, Sci Publ House (17):
  • [8] Computational method for interaction between rigid indenter and elastic inclusion
    Fujimoto, K
    COMPUTATIONAL METHODS IN CONTACT MECHANICS VI, 2003, 8 : 83 - 92
  • [9] DYNAMIC CHARACTERISTICS OF COMPOSITE HELICOPTER BLADE SOLVED BY USING THE DIFFERENTIAL QUADRATURE METHOD
    Kuang, J. H.
    Hsu, M. H.
    Hung, T. P.
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 5, PT A, 2008, : 289 - 297
  • [10] BIFURCATION METHOD TO CALCULATE FLUTTER CHARACTERISTICS OF A HELICOPTER BLADE HAVING COMPLEX DAMPING
    THORNTON, BS
    JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 1975, 300 (5-6): : 365 - 375
12345