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Laminated composite plates exhibit properties different from those of single-layer plate. In addition, the great difference in elastic properties between fiber and matrix materials leads to a high ratio of in-plane Young`s modulus to transverse shear modulus for laminated composite plates. It results in the fact that the classical theory of plates, based on neglecting transverse shear deformation, is invalid for laminated composite plates. Thus, to obtain the more exact behavior of laminated composite plates, considering a effects of shear deformation and geometrical nonlinear should be considered in the analysis of them. The finite difference technique is used to analyze laminated composite rectangular plates in geometrical nonlinear problem as well as linear problem. The algorithm in this study is the Newton-Raphson iteration method. From the numerical results, it is clarified that the effects of transverse shear deformation and coupling between stretching and bending due to variation of ply-angle are quite significant components for small ratio of side length to thickness.
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UCI(KEPA) : I410-ECN-0101-2018-053-003648908