Affiliation:
1. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0150
Abstract
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.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Cited by
72 articles.
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