Effect of Load Sequence on the Statistical Fatigue of Composites
- 1 December 1980
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (12), 1525-1531
- https://doi.org/10.2514/3.50912
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Effect of High Load on Statistical Fatigue of Unnotched Graphite/Epoxy Laminates*Journal of Composite Materials, 1980
- Statistical Fatigue of Graphite/Epoxy Angle-Ply Laminates in Shear1Journal of Composite Materials, 1978
- Fatigue and Residual Strength Degradation for Graphite/Epoxy Composites Under Tension-Compression Cyclic LoadingsJournal of Composite Materials, 1978
- Residual Strength Degradation Model and Theory of Periodic Proof Tests for Graphite/Epoxy Laminates*Journal of Composite Materials, 1977
- A Note on Determination of the Shear Stress-Strain Response of Unidirectional CompositesJournal of Composite Materials, 1973
- A Simple Procedure for Experimental Determination of the Longitudinal Shear Modulus of Unidirectional CompositesJournal of Composite Materials, 1972
- A New Theory to Predict Cumulative Fatigue Damage in Fiberglass Reinforced PlasticsPublished by ASTM International ,1972