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In recent years the development of high modulus, high strength and low density boron and graphite fibers bonded together has brought a renewed interest in structural elements fabricated of layers, each layer possessing different mechanical properties. Typically the application of these composite materials involves multiple layers of fibers, and the dimensions of the structural elements are such the each layer can be adequately modeled as an anisotropic layer. The great difference in elastic properties between fiber and matrix materials leads to a higher ratio of in-plane Young`s modulus to transverse shear modulus for laminated composite plates. Thus, to obtain the more accurate solutions to laminated composite plate problems, The effects of shear strain should be considered in analysis of them. The present study deals with the third-order shear deformation theory for simply supported cross-ply and antisymmetric angle-ply laminated composite plates by Navier solutions. The present third-order theory gives more exact solution than either the first-order theory or the classical theory. Theory and enact analysis of laminated composite plates proposed in this paper should be used in design of them.
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UCI(KEPA) : I410-ECN-0101-2018-053-003650117