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首页> 外文期刊>Composite Structures >Notch insensitivity in fatigue failure of chopped carbon fiber chip-reinforced composites using experimental and computational analysis
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Notch insensitivity in fatigue failure of chopped carbon fiber chip-reinforced composites using experimental and computational analysis

机译:使用实验和计算分析,切碎的碳纤维芯片增强复合材料疲劳失效的凹口不敏感

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摘要

This study focuses on the notch effect on the fatigue failure of chopped carbon fiber chip-reinforced sheet molding compound (SMC) composites by using both experimental and numerical methods. The S-N diagrams of notched specimens are first obtained experimentally, which exhibit large scatter and are shown to depend on the spatial distribution of local fiber orientations. After considering the effect of this spatial distribution by adopting a new fatigue damage parameter to normalize the results, we achieve a much better correlation in the normalized S-N diagram for all the notched specimens with different hole diameters. Next, compared with the fatigue results of smooth specimens without notches, we find that SMC composites under tension-tension fatigue loading exhibit notch-insensitivity, which renders this type of composites a better candidate in joints or similar applications. Meanwhile, the fatigue failure mechanisms of notched SMC composites are explored through a microstructure characterization procedure. On this basis, a computational micromechanics model considering the notch effect and an improved multi-scale progressive damage fatigue law, calibrated by coupon-level fatigue tests of smooth SMC composites under different loading conditions, are employed to predict the fatigue behavior of notched SMC composites. We show that detailed failure processes and fatigue life of notched SMC composites can be efficiently and adequately predicted by this computational framework.
机译:本研究专注于通过使用两种实验和数值方法对切碎的碳纤维芯片增强板成型化合物(SMC)复合材料疲劳失效的凹口效应。首先通过实验获得缺口样品的S-N图,其表现出大散射,并显示为局部纤维取向的空间分布。在考虑这种空间分布的效果之后采用新的疲劳损伤参数来规范化结果,我们在具有不同孔直径的所有缺口样本的标准化S-N图中获得了更好的相关性。接下来,与没有缺口的平滑样品的疲劳结果相比,我们发现在张紧张力疲劳负载下的SMC复合材料表现出凹口内不敏感性,这使得这种复合材料呈现在关节或类似应用中的更好候选物。同时,通过微结构表征程序探索缺口SMC复合材料的疲劳失效机制。在此基础上,考虑到凹口效应的计算微机械模型和改进的多尺度逐行损伤疲劳法,通过在不同负载条件下的平滑SMC复合材料的优惠级疲劳试验校准,用于预测缺口SMC复合材料的疲劳行为。我们表明,通过该计算框架可以有效和充分地预测缺口SMC复合材料的详细故障过程和疲劳寿命。

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