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Life prediction of a notched composite ring using progressive fatigue damage models

机译:渐进式疲劳损伤模型预测带缺口复合材料环的寿命

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摘要

In this paper, a progressive fatigue damage modeling technique is proposed based on Reifsnider's critical element concept. The static and fatigue behavior of the unidirectional E-glass/epoxy composite plies in the fiber and matrix direction is obtained experimentally. Considering suitable material property degradation models, a computer code is developed which integrating with the Abaqus software it is capable of predicting the fatigue life of a notched composite ring with different layup configuration under arbitrary states of stress. To evaluate the applicability of the model, a number of fatigue tests under different states of stress are conducted on the notched composite rings. It is proved that by having unidirectional properties of a composite, this model is capable of estimating the static strength of the notched rings with less than five percent deviation and putting forward a reliable prediction for fatigue life with less than twenty percent underestimation.
机译:本文基于Reifsnider的关键要素概念,提出了一种渐进式疲劳损伤建模技术。通过实验获得了单向电子玻璃/环氧树脂复合材料层在纤维和基体方向上的静态和疲劳行为。考虑合适的材料性能退化模型,开发了计算机代码,该代码与Abaqus软件集成在一起,能够预测在任意应力状态下具有不同铺层配置的带槽复合环的疲劳寿命。为了评估该模型的适用性,在带缺口的复合材料环上进行了许多在不同应力状态下的疲劳测试。实践证明,通过具有复合材料的单向特性,该模型能够估算出缺口环的静态强度,偏差小于5%,并提出了可靠的疲劳寿命预测值,该估算值被低估了不到20%。

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