Affiliation:
1. Grumman Aerospace Corporation, Bethpage, New York 11714
Abstract
By observing results of experimental program for testing static strength of composite laminates under combined by-pass tension and bolt load, a tension failure factor is proposed herein to determine the failure modes of the composites. Comparison with experimental results shows that the proposed tension failure factor is a reasonable indicator. Possible application for estimating failure loads by interpolation of available data is illustrated with a numerical example.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
11 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献