Thermal Buckling of Rectangular Laminated Plates with a Hole-Reference-Cited by-同舟云学术

Thermal Buckling of Rectangular Laminated Plates with a Hole

Published:2005-02 Issue:3 Volume:24 Page:259-272
ISSN:0731-6844
Container-title:Journal of Reinforced Plastics and Composites
language:en
Short-container-title:Journal of Reinforced Plastics and Composites

Author:

Avci Ahmet¹,Kaya Sami²,Daghan Behcet²

Affiliation:

1. Department of Mechanical Engineering, Selçuk University, Konya, Turkey,

2. Department of Mechanical Engineering, Selçuk University, Konya, Turkey

Abstract

Thermal buckling analysis of symmetric and antisymmetric laminated composite plates with clamped and simply supported edges, and containing a hole is presented in this paper. The first-order shear deformation theory in conjunction with the variational energy method is employed in mathematical formulation. The eight-node Lagrangian finite element technique is used to find thermal buckling temperatures of isotropic, glass-epoxy and boron-epoxy laminates. The effects of hole size, angle of ply orientation, lay-up sequences, and boundary conditions on thermal buckling temperatures are investigated. The result is shown in graphical forms for various boundary conditions.

Publisher

SAGE Publications

Subject

Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Link

http://journals.sagepub.com/doi/pdf/10.1177/1731684405043554

Reference18 articles.

1. Thermal buckling of cross-ply composite laminates

2. Thermal buckling of cross-ply composite laminates using a first-order shear deformation theory

3. Thermal buckling of rectangular plates

4. Thermal buckling of clamped symmetric laminated plates

5. Prabhu, M.R. and Dhanaraj, R. (1994). Thermal Buckling of Laminated Composite Plates, Computers & Structures, 1193-1204.

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