A continuum model for predicting strain evolution in carbon fiber-reinforced composites subjected to cyclic loading
Author:
Funder
Aeronautics Research and Development Board
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
https://link.springer.com/content/pdf/10.1007/s12046-021-01728-8.pdf
Reference22 articles.
1. Epaarachchi J A and Clausen P D 2003 An empirical model for fatigue behavior prediction of glass fibre-reinforced plastic composites for various stress ratios and test frequencies. Composites Part A 34: 313–326
2. Reifsnider K L and Talug A 1980 Analysis of fatigue damage in composite laminates. Int. J. Fatigue 2: 3–11
3. Highsmith A L and Reifsnider K L 1982 Stiffness–reduction mechanisms in composite laminates. Damage in Composite Materials: Basic Mechanisms, Accumulation, Tolerance, and Characterization, ed. K. Reifsnider (West Conshohocken, PA: ASTM International) 103–117
4. Yang J N 1978 Fatigue and Residual Strength Degradation for Graphite/Epoxy Composites Under Tension-Compression Cyclic Loadings. J. Composite Materials 12: 19–39
5. Caprino G 1984 Residual Strength Prediction of Impacted CFRP Laminates. J. Composite Materials 18: 508–518
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