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• W4200578627 endingPage "115074" @default.
• W4200578627 startingPage "115074" @default.
• W4200578627 abstract "In this paper, an enhanced higher order zigzag theory is developed for laminated composite plates. By satisfying inter-laminar stress continuity conditions and free surfaces conditions, the final displacement field of the present theory can be obtained from Cho’s the initial displacement field [27]. The displacement variables in the present theory are independent on the number of layer. In contrast to Cho’s higher order zigzag theory [27], only one transverse displacement variable is introduced into in-plane displacement field in the proposed theory. To assess the accuracy of this model, simply-supported laminated composite plates subjected to mechanical or thermal loading are analyzed respectively by using the Navier method. Numerical results show that the present model can accurately predict behaviors of laminated composite plates and are more suitable for multilayered plates in comparison with Cho’s higher order zigzag theory." @default.
• W4200578627 created "2021-12-31" @default.
• W4200578627 creator A5042973046 @default.
• W4200578627 creator A5044649484 @default.
• W4200578627 date "2022-02-01" @default.
• W4200578627 modified "2023-09-24" @default.
• W4200578627 title "An enhanced higher order zigzag theory for laminated composite plates under mechanical/thermal loading" @default.
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• W4200578627 doi "https://doi.org/10.1016/j.compstruct.2021.115074" @default.
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