2017
DOI: 10.1016/j.cja.2016.12.027
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Analytical solution methods for eigenbuckling of symmetric cross-ply composite laminates

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Cited by 6 publications
(1 citation statement)
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“…It was concluded that for plate structures with the characteristic lengthto-thickness ratio greater than 20, the results from [119][120][121][122][124][125][126], [127,128] obtained from different plate theories under various boundary conditions agree well with the exact solutions. Lastly, based on the FSDPT, Xing and Xiang [123] proposed an analytical method for the buckling of symmetric cross-ply composite laminates, using the separation-of-variable method in conjunction with the SSA to enhance the computational efficiency and circumvent numerically illconditioned problems. The accuracy and effectiveness of the analytical model were validated by comparing the numerical results with the those in the literature [126,148].…”
Section: Laminated Platesmentioning
confidence: 99%
“…It was concluded that for plate structures with the characteristic lengthto-thickness ratio greater than 20, the results from [119][120][121][122][124][125][126], [127,128] obtained from different plate theories under various boundary conditions agree well with the exact solutions. Lastly, based on the FSDPT, Xing and Xiang [123] proposed an analytical method for the buckling of symmetric cross-ply composite laminates, using the separation-of-variable method in conjunction with the SSA to enhance the computational efficiency and circumvent numerically illconditioned problems. The accuracy and effectiveness of the analytical model were validated by comparing the numerical results with the those in the literature [126,148].…”
Section: Laminated Platesmentioning
confidence: 99%