Predicting the buckling load of anisotropic sandwich panels: an approach including shear deformation of the faces

被引：24

作者：

Hadi, BK ^{[1
]}

Matthews, FL ^{[1
]}

机构：

[1] Univ London Imperial Coll Sci Technol & Med, Ctr Composite Mat, London SW7 2BY, England

来源：

COMPOSITE STRUCTURES | 1998年 / 42卷 / 03期

关键词：

D O I：

10.1016/S0263-8223(98)00067-1

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This paper presents a method for calculating the critical buckling load of sandwich panels. Based on earlier 'zig-zag' models for through-thickness displacements, the transverse shear deformation of the faces is included, thus allowing the analysis of thick sandwich plates. Where possible, predictions have been compared with other workers. Also, the influence of face lay-up and plate aspect ratio are investigated. (C) 1998 Published by Elsevier Science Ltd. All rights reserved.

引用

页码：245 / 255

页数：11

共 19 条

[1]

Allen H.G., 1969, ANAL DESIGN STRUCTUR

[2] BUCKLING OF GENERALLY LAMINATED COMPOSITE PLATES [J].