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Plasticity Analysis of Laminated Composite Plates

Journal of Applied Mechanics, 1982
Elastic-plastic behavior of symmetric metal-matrix composite laminates is analyzed for the case of in-plane mechanical loading. The overall response of the laminate at each instant is derived from the elastic-plastic deformation of the individual fibrous layers, and from their mutual constraints.
Bahei-El-Din, Y. A., Dvorak, G. J.
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Dynamic Response of Laminated Composite Plates

AIAA Journal, 1975
HE classical method of separation of variables combined with the Mindlin-Goodman procedure1 is employed to analyze the dynamic response of an infinitely long simplysupported composite plate under a uniform dynamic pressure, P0, on the upper surface of the plate.
Sun, Chang-Tsan   +2 more
openaire   +1 more source

Edge Vibrations in Laminated Composite Plates

Journal of Applied Mechanics, 1985
Plane strain edge vibrations or end modes in laminated composite plates are investigated by means of finite elements. This method is capable of modeling the behavior of any laminate construction whose properties are completely anisotropic within the plane. Two eigenvalue problems involving nonsymmetric matrices are derived.
Dong, S. B., Huang, K. H.
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Edge Effects in Laminated Composite Plates

Journal of Applied Mechanics, 1982
The attenuation of self-equilibrated edge stress states into the interior of a laminated plate composed of an arbitrary number of bonded, elastic, anisotropic layers is investigated in the context of Saint-Venant’s principle using the exponential decay results of Toupin, Knowles, and Horgan.
Dong, S. B., Goetschel, D. B.
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Review on laminated composite plates

ASPS Conference Proceedings, 2022
A composite material is a combination of different material which can be assembled to provide required engineering properties like bending, buckling, stiffness etc. It can give better properties than those of individual components. A lamina is the building block of modern composite laminated structures. A lamina is also known as a ply, or a layer.
D. Dibyajyoti, B. Alfia
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On the Behaviour of Plates Laminated of Bimodulus Composite Materials

ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1982
AbstractAn excet and finite‐element analysis is used to predict the static bending and natural vibration response of rectangular plates laminated of composite material having different elastic properties depending upon whether the fiber‐direction strains are tensile or compressive. The analysis is based on a theory that accounts for anisotropy, bending‐
Reddy, J. N., Bert, C. W.
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