Journal ArticleDOI
A high-order theory for the analysis of circular cylindrical composite sandwich shells with transversely compliant core subjected to external loads
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TLDR
In this article, a new model based on the high order sandwich panel theory is proposed to study the effect of external loads on the free vibration of circular cylindrical composite sandwich shells with transversely compliant core, including also the calculation of the buckling loads.About:
This article is published in Composite Structures.The article was published on 2012-06-01. It has received 42 citations till now. The article focuses on the topics: Sandwich panel & Displacement field.read more
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Review of current trends in research and applications of sandwich structures
TL;DR: A review of modern trends in theoretical developments, novel designs and modern applications of sandwich structures can be found in this paper, where the most recent literature published at the time of writing this review is considered, older sources are listed only on as-needed basis.
Journal ArticleDOI
A unified formulation for vibration analysis of composite laminated shells of revolution including shear deformation and rotary inertia
TL;DR: In this paper, a variational formulation for predicting the free, steady-state and transient vibrations of composite laminated shells of revolution subjected to various combinations of classical and non-classical boundary conditions is presented.
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A simple first-order shear deformation shell theory for vibration analysis of composite laminated open cylindrical shells with general boundary conditions
Qingshan Wang,Dong Shao,Bin Qin +2 more
TL;DR: In this article, a simple first-order shear deformation shell theory (S-FSDST) was proposed for free and transient vibration analysis of composite laminated open cylindrical shells with general boundary conditions.
Journal ArticleDOI
An efficient layerwise finite element for shallow composite and sandwich shells
M. Yaqoob Yasin,Santosh Kapuria +1 more
TL;DR: In this paper, a four-node quadrilateral element for laminated plates based on an efficient layerwise theory, called the Zigzag theory (ZIGT), was extended to laminated shallow shells and compared with the available 3D elasticity solutions as well as the 2D analytical and FE solutions for various singly and doubly-curved composite and sandwich shallow shells.
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Three-dimensional thermo-elasticity solution of sandwich cylindrical panel with functionally graded core
TL;DR: In this paper, a static analysis of a simply supported sandwich panel with functionally graded material (FGM) core subjected to thermo-mechanical mechanical load is carried out based on theory of elasticity.
References
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Book
Mechanics of Laminated Composite Plates and Shells : Theory and Analysis, Second Edition
TL;DR: The use of composite materials in engineering structures continues to increase dramatically, and there have been significant advances in modeling for general and composite materials and structures in particular as discussed by the authors. But the use of composites is not limited to the aerospace domain.
Book
Mechanics of laminated composite plates and shells : theory and analysis
TL;DR: In this article, the authors present an analysis of the properties of composite materials using the classical and first-order theories of Laminated Composite Plates and shells, as well as a detailed analysis of their properties.
Journal ArticleDOI
Historical review of Zig-Zag theories for multilayered plates and shells
TL;DR: A review of the Zig-Zag theories for multilayered structures can be found in this article, where the authors refer to these three theories by using the following three names: Lekhnitskii Multi-layered Theory, ~LMT!, Ambartsumian Multi-Layered Theory ~AMT!, and Reissner Multilayed Theory ~RMT.
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Laminated Composite Plate Theory With Improved In-Plane Responses
TL;DR: In this paper, a new laminated composite plate theory was developed based upon a new variational principle proposed by Reissner (1984), which was achieved by including a zigzag-shaped C 0 function to approximate the thickness variation of in-plane displacements.