Effect of Load Sequence on the Statistical Fatigue of Composites
Author:
Affiliation:
1. The George Washington University, Washington, D. C.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50912
Reference18 articles.
1. Fatigue and Residual Strength Degradation for Graphite/Epoxy Composites Under Tension-Compression Cyclic Loadings
2. Residual Strength Degradation Model and Theory of Periodic Proof Tests for Graphite/Epoxy Laminates*
3. Statistical Fatigue of Graphite/Epoxy Angle-Ply Laminates in Shear1
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