Thermal buckling of hybrid angle-ply laminated composite plates with a hole

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Date

2005

Journal Title

Journal ISSN

Volume Title

Publisher

ELSEVIER SCI LTD

Access Rights

info:eu-repo/semantics/openAccess

Abstract

In this paper, thermal buckling analysis of symmetric and antisymmetric laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions is presented. The first-order shear deformation theory in conjunction with variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used for obtaining the thermal buckling temperatures of glass-epoxy/boron-epoxy hybrid laminates. The effects of hole size, layup sequences and boundary conditions on thermal buckling temperatures are investigated. The results are shown in graphical form for various boundary conditions. (c) 2005 Elsevier Ltd. All rights reserved.

Description

Keywords

hybrid composite plates, thermal buckling, finite element method

Journal or Series

COMPOSITES SCIENCE AND TECHNOLOGY

WoS Q Value

Q1

Scopus Q Value

Q1

Volume

65

Issue

11.12.2020

Citation