The dynamic stability of a rotating pre-twisted asymmetric cross-section blade subjected to lateral parametric excitation

被引:9
|
作者
Sabuncu, Mustafa [1 ]
Evran, Kaan [1 ]
机构
[1] Dokuz Eylul Univ, Dept Mech Engn, TR-35100 Izmir, Turkey
关键词
dynamic stability; coupling; lateral; rotating; pretwist; asymmetric;
D O I
10.1016/j.finel.2006.04.004
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
The dynamic stability of a pre-twisted rotating blade having asymmetric aerofoil cross-section subjected to lateral parametric excitation is studied by using the finite element method. The Bernoulli-Euler theory is employed in the analysis. Solutions referred to as combination resonance are investigated. The effects of coupling due to centre of flexure distance from the centroid, rotation and the stagger angle on the stability are considered. The change in these effects due to pretwist angle is investigated. It is concluded from the results that the pretwist angle has an influence on the effects of coupling and rotation. (c) 2006 Elsevier B.V. All rights reserved.
引用
收藏
页码:1113 / 1122
页数:10
相关论文
共 33 条
  • [21] Coupled bending-bending-torsion vibration of a pre-twisted beam with aerofoil cross-section by the finite element method
    Yardimoglu, B
    Inman, DJ
    SHOCK AND VIBRATION, 2003, 10 (04) : 223 - 230
  • [22] Coupled flapwise-chordwise-axial-torsional dynamic responses of rotating pre-twisted and inclined cantilever beams subject to the base excitation
    Jin ZENG
    Hui MA
    Kun YU
    Zhitao XU
    Bangchun WEN
    AppliedMathematicsandMechanics(EnglishEdition), 2019, 40 (08) : 1053 - 1082
  • [23] Coupled flapwise-chordwise-axial-torsional dynamic responses of rotating pre-twisted and inclined cantilever beams subject to the base excitation
    Zeng, Jin
    Ma, Hui
    Yu, Kun
    Xu, Zhitao
    Wen, Bangchun
    APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2019, 40 (08) : 1053 - 1082
  • [24] Coupled flapwise-chordwise-axial-torsional dynamic responses of rotating pre-twisted and inclined cantilever beams subject to the base excitation
    Jin Zeng
    Hui Ma
    Kun Yu
    Zhitao Xu
    Bangchun Wen
    Applied Mathematics and Mechanics, 2019, 40 : 1053 - 1082
  • [25] Dynamic stability analysis for rotating pre-twisted FG-CNTRC beams with geometric imperfections restrained by an elastic root in thermal environment
    Lin, Baichuan
    Chen, Bo
    Zhu, Bo
    Li, Ji-an
    Li, Yinghui
    THIN-WALLED STRUCTURES, 2021, 164
  • [26] STABILITY OF A ROTATING, PRE-TWISTED, NON-UNIFORM CANTILEVER BEAM WITH TIP MASS AND THERMAL-GRADIENT SUBJECTED TO A NON-CONSERVATIVE FORCE
    KAR, RC
    NEOGY, S
    COMPUTERS & STRUCTURES, 1989, 33 (02) : 499 - 507
  • [27] Investigation on the 1:2:3 internal resonance of high dimensional nonlinear dynamic system for FGGP reinforced rotating pre-twisted blade under the aerodynamic forces
    Gu, X. J.
    Zhang, Y. F.
    Zhang, W.
    Bi, Q. S.
    Lu, S. F.
    COMMUNICATIONS IN NONLINEAR SCIENCE AND NUMERICAL SIMULATION, 2024, 130
  • [28] APPLICATION OF REISSNER METHOD TO FREE VIBRATIONS OF A TAPERED, TWISTED, AEROFOIL CROSS-SECTION TURBINC BLADE, MOUNTED AT A STAGGER ANGLE ON A ROTATING DISC.
    Rao, J.S.
    Vyas, N.S.
    Defence Science Journal, 1986, 36 (03) : 273 - 292
  • [29] Coupled bending-bending-torsion vibration of a pre-twisted beam with aerofoil cross-section by finite element method (vol 10, pg 223, 2003)
    Yardimoglu, B
    Inman, DJ
    SHOCK AND VIBRATION, 2003, 10 (5-6) : 387 - 387
  • [30] Dynamic stability of spinning beams with an unsymmetrical cross-section and distinct boundary conditions subjected to time-dependent spin speed
    Lee, HP
    Tan, TH
    Leng, GSB
    MECHANICS OF STRUCTURES AND MACHINES, 1997, 25 (02): : 179 - 200