Results 301 to 310 of about 44,087 (354)

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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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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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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MITC finite elements for laminated composite plates

International Journal for Numerical Methods in Engineering, 2001
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
ALFANO G., AURICCHIO F., ROSATI, LUCIANO, SACCO E.   +3 more
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Analysis of composite laminated plates

Applied Mathematics and Mechanics, 1988
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Yeh, Kaiyuan, Deng, Liangbo
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Bending of Laminated Composite Plates

Applied Mechanics and Materials, 2015
In this work, there are presented overviews of theoretical and numerical models for defining the stress-strain state in the cross section of moderately thick and thick composite plates in case of bending. Layered composite plates are constructed by combination of layers of various materials and geometrical characteristics, wherein each of them has got ...
Marina Rakočević, Nikolay Vatin
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Optimum Design of Laminated Composite Plates Using Lamination Parameters

AIAA Journal, 1991
When laminated composite plates are symmetric and orthotropic, their in-plane and flexural stiffnesses become the functions of the lamination parameters that are the functions of their stacking sequences. We use the lamination parameters as fundamental design variables in designing laminates. The feasible region of the lamination parameters is obtained
MITSUNORI MIKI, YOSHIHIKO SUGIYAMA
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Buckling Behavior of Laminated Composite Plates

Journal of Reinforced Plastics and Composites, 2007
In this study, the influence of boundary conditions on the buckling load for rectangular plates of various cutout shape, length/thickness ratio, and ply orientation is examined. Boundary conditions consisting of clamped, pinned, and their combinations are considered.
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VARIABLE KINEMATIC MODELLING OF LAMINATED COMPOSITE PLATES

International Journal for Numerical Methods in Engineering, 1996
A displacement-based variable kinematic global-local finite element model is developed using hierarchical, multiple assumed displacement fields at two different levels: (1) at the element level, and (2) at the mesh level. The displacement field hierarchy contains both a conventional two-dimensional plate expansion and a full layerwise three-dimensional
Robbins, D. H. jun., Reddy, J. N.
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Composite Laminated Plates

2013
High-performance and lightweight characteristics of composite materials have motivated a wide range of applications of these materials in aeronautic and space vehicles and in naval, automotive and civil structures, among other fields [Bar2,BC,Mar,TH4,Ts,Wh].
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