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Fatigue behavior of the carbon/epoxy and the carbon/PEEK composites subjected to low-energy impact

机译:碳/环氧树脂和碳/ PEEK复合材料在低能量冲击下的疲劳行为

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Fatigue behaviors of carbon fiber reinforced thermosetting and thermoplastic composites with and without subjecting low-energy impact were investigated. The [0/45/90-45]_2s T300/976 carbon/epoxy and AS-4/PEEK laminates were used in this study. The impact response of these two laminates shows a linear force-deformation relationship in the initial penetration impact loading, which implies an elastic behavior of these two composites; the following zigzag peaks indicate fracture initiation and arrest. The fatigue tests were performed at various stress levels under tension-tension loadings with a fatigue frequency of 3 and stress ratio of 0.1. The median rank method and Weibull distribution were applied to predict the fatigue probabilities of the specimen under static and fatigue tests. The S-N curves for the undamaged and low-energy impact damaged laminates are compared.
机译:研究了碳纤维增强的热固性和热塑性复合材料在有无低能冲击下的疲劳行为。在这项研究中使用了[0/45 / 90-45] _2s T300 / 976碳/环氧树脂和AS-4 / PEEK层压板。这两个层压板的冲击响应在初始穿透冲击载荷中显示出线性力-变形关系,这暗示了这两个复合材料的弹性行为。以下锯齿形峰表示骨折的开始和停止。在不同的应力水平下,在疲劳频率为3且应力比为0.1的拉伸-拉伸载荷下进行疲劳测试。应用中位秩和威布尔分布预测静态和疲劳试验下的样品疲劳概率。比较了未损坏和低能量冲击损坏的层压板的S-N曲线。

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