BUCKLING OF THICK ORTHOTROPIC CYLINDRICAL-SHELLS UNDER EXTERNAL-PRESSURE

被引：62

作者：

KARDOMATEAS, GA

机构：

[1] School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA

来源：

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1993年 / 60卷 / 01期

关键词：

Shells; (structures);

D O I：

10.1115/1.2900745

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

An elasticity solution to the problem of buckling of orthotropic cylindrical shells subjected to external pressure is presented. In this context, the structure is considered a three-dimensional body. The results show that the shell theory predictions can produce nonconservative results on the critical load of composite shells with moderately thick construction. The solution provides a means of accurately assessing the limitations of shell theories in predicting stability loss.

引用

页码：195 / 202

页数：8

共 13 条

[1]

Ambartsumyan S. A., 1961, THEORY ANISOTROPIC S

[2]

ANASTASIADIS JS, 1990, THESIS GEORGIA I TEC

[3]

Brush D.O., 1975, BUCKLING BARS PLATES

[4] ACCURATE BUCKLING EQUATIONS FOR ARBITRARY AND CYLINDRICAL ELASTIC SHELLS [J].