Interactive local/Euler buckling of composite cylindrical shells

被引:14
作者
Weaver, PM [1 ]
Dickenson, R [1 ]
机构
[1] Univ Bristol, Dept Aerosp Engn, Bristol BS8 1TR, Avon, England
基金
英国工程与自然科学研究理事会;
关键词
buckling; cylindrical shell; composite; spiral;
D O I
10.1016/S0045-7949(03)00339-0
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
Long circular cylindrical shells may locally buckle at lower loads than those predicted by classical linear Donnell solutions due to long range interaction between Euler and local buckling. In fact, Euler buckling may be viewed as a special case of local buckling in which both the longitudinal and circumferential wave numbers are unity. This paper investigates this phenomenon for composite tubes as a function of lay-up. Tubes that are reinforced in predominantly the longitudinal or circumferential directions suffer the least knockdown of approximately 10% for tubes that are designed to buckle concurrently by Euler and local mechanisms. The greatest knockdown of approximately 35% occurs for isotropic laminates. The effect of material lay-up has been taken account of by forming a non-dimensional length parameter that is a function of both tube geometry and material properties. An interaction formula is proposed to help in design situations. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2767 / 2773
页数:7
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