Imperfection sensitivity of free vibration of symmetrically/anti-symmetrically laminated FRC beams in thermally pre-and post-buckling equilibrium states

被引:21
|
作者
Jin, Qiduo [1 ,2 ]
Ren, Yiru [1 ,2 ]
Peng, Fan [1 ,2 ]
Jiang, Hongyong [1 ,2 ]
机构
[1] Hunan Univ, State Key Lab Adv Design & Mfg Vehicle Body, Changsha 410082, Hunan, Peoples R China
[2] Hunan Univ, Coll Mech & Vehicle Engn, Changsha 410082, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
Free vibration; Pre-and post-buckled FRC beams; Zig-zag displacements; Imperfection sensitivity; Two-step perturbation; COMPOSITE BEAMS; CARBON NANOTUBE; NONLINEAR VIBRATION; RITZ-SOLUTION; BUCKLED BEAM; SHEAR; BEHAVIOR; PLATES; DEFLECTION; STABILITY;
D O I
10.1016/j.actaastro.2020.04.024
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Linear/nonlinear free vibration of imperfect symmetrically/anti-symmetrically laminated fibre-reinforced composite (FRC) beams in the pre-and post-buckling equilibrium states are studied. It is assumed that the initial defect has the same shape as the first-order buckling mode and the in-plane boundaries are immovable. A modified higher-order shear deformation zig-zag beam model is applied for refined modeling of the laminated beams. The Hamilton variational principle is utilized to obtain the governing equations of motion. The two-step perturbation technique is combined with the harmonic balance method to obtain the asymptotic analytic solutions. The results based on the zig-zag model and its degenerate equivalent single-layer models are compared and verified. Further, the sensitivity of vibration characteristics to the size of imperfections at different temperature rise is investigated. Numerical results suggest that there exists a load range near the critical buckling load of the perfect beams where the linear/nonlinear frequency is sensitive to the initial imperfections.
引用
收藏
页码:240 / 251
页数:12
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