BUCKLING AND POSTBUCKLING OF COMPOSITE STRUCTURES

被引：112

作者：

STEVENS, KA

RICCI, R

DAVIES, GAO

机构：

[1] Department of Aeronautics, Imperial College of Science, Technology and Medicine, London, SW7 2BY, Prince Consort Road

来源：

COMPOSITES | 1995年 / 26卷 / 03期

关键词：

I-STIFFENED PANEL; BUCKLING BEHAVIOR; FAILURE MECHANISM;

D O I：

10.1016/0010-4361(95)91382-F

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

The postbuckling behaviour of a flat, stiffened, carbon fibre composite compression panel has been studied, theoretically and experimentally. The panel had a collapse load in excess of three times the buckling load. An initial failure mechanism leading to eventual explosive collapse of the panel is identified and the damaging stress resultant is measured in the panel and predicted from a finite element analysis.

引用

页码：189 / 199

页数：11

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