期刊
ACTA ASTRONAUTICA
卷 173, 期 -, 页码 240-251出版社
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actaastro.2020.04.024
关键词
Free vibration; Pre-and post-buckled FRC beams; Zig-zag displacements; Imperfection sensitivity; Two-step perturbation
资金
- Foundation for Innovative Research Groups of the National Natural Science Foundation of China [51621004]
- National Natural Science Foundation of China [11402011]
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.
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