Progressive Fatigue Damage Modeling of Cross-ply Laminates, I: Modeling Strategy

被引:34
|
作者
Shokrieh, M. M. [1 ]
Taheri-Behrooz, F. [1 ]
机构
[1] Iran Univ Sci & Technol, Composites Res Lab, Dept Mech Engn, Tehran 1684613114, Iran
关键词
progressive fatigue damage modeling; carbon/epoxy; cross-ply composites; stiffness degradation; strength degradation; CARBON-FIBER COMPOSITES; LIFE PREDICTION; TRANSVERSE CRACKING; FAILURE CRITERION; RESIDUAL STRENGTH; UNIAXIAL FATIGUE; BEHAVIOR; STRESS;
D O I
10.1177/0021998309351604
中图分类号
TB33 [复合材料];
学科分类号
摘要
The main goal of this research is the fatigue simulation of cross-ply laminates under cyclic tension-tension loading conditions. For this purpose, a progressive fatigue damage model is developed based on two main assumptions. First, it is assumed that off-axis plies are responsible for stress redistribution into the laminate. Second, on-axis plies are responsible for strength reduction and control failure of the laminate. Developed model is capable of predicting the fatigue life and residual strength of cross-ply laminates with a limited experimental data and acceptable accuracy. The results of the model are compared with the experimental data provided in the second part of the present article.
引用
收藏
页码:1217 / 1231
页数:15
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