Affiliation:
1. Department of Civil, Mechanical and Environmental Engineering The George Washington University Washington, DC 20052
Abstract
A fatigue residual strength degradation model has been generalized to account for the effect of tension-compression fatigue loading. The model is verified experimentally by use of graphite/epoxy unnotched composite laminates. It is shown that the correlation between the experimental results and the theoretical predictions on both the residual strength degradation and fatigue life is very reasonable.
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Cited by
108 articles.
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