Thermal buckling of hybrid laminated composite plates with a hole

被引：17

作者：

Avci, A ^{[1
]}

Sahin, ÖS ^{[1
]}

Uyaner, M ^{[1
]}

机构：

[1] Selcuk Univ, Dept Mech Engn, TR-42075 Konya, Turkey

来源：

COMPOSITE STRUCTURES | 2005年 / 68卷 / 02期

关键词：

hybrid composite plates; thermal buckling; finite element method;

D O I：

10.1016/j.compstruct.2004.03.017

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Thermal buckling analysis of symmetric and antisymmetric cross-ply laminated hybrid composite plates with a hole subjected to a uniform temperature rise for different boundary conditions are presented in this paper. The first-order shear deformation theory in conjunction with variational energy method is employed in the mathematical formulation. The eight-node Lagrangian finite element technique is used for finding the thermal buckling temperatures of hybrid laminates. The effects of hole size, lay-up sequences and boundary conditions on the thermal buckling temperatures are investigated. The results are shown in graphical form for various conditions. (c) 2004 Published by Elsevier Ltd.

引用

页码：247 / 254

页数：8

共 20 条

[1] THERMAL BUCKLING OF CROSS-PLY COMPOSITE LAMINATES USING A 1ST-ORDER SHEAR DEFORMATION-THEORY [J].