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Impact-Induced Delamination Suppression in Laminated Composites using through-thickness Stitching

机译:使用厚度拼接的层压复合材料的冲击诱导分层抑制

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This paper aims to investigate the effectiveness of using through-thickness stitching in suppressing impact-induced delamination growth in laminated composites. Low-velocity impact tests are conducted on unstitched and stitched specimens with varying stitch density and stitch thread thickness. Results show that stitching effectively bridges and arrests delamination crack, and reduces delamination growth up to 40%. It is also revealed that increasing stitch density is more effective (23% reduction) in minimising delamination area than increasing stitch thread thickness (8% reduction). A novel empirical-based Delamination Reduction Law (DRL) has been formulated to predict the delamination reduction in stitched composites due to impact loading. The DRL is further validated with numerous published literature results, which have demonstrated good consistency and excellent agreement with the prediction curve. The effectiveness of stitching in impact-induced delamination, which is primarily mode II and without stitch breakage, is compared and discussed with authors' previous work on mode I fracture delamination of stitched composites.
机译:本文旨在研究使用全厚度缝合来抑制层压复合材料中冲击诱导的脱层生长的有效性。低速冲击试验是在针迹密度和线迹粗细不同的未缝制和已缝制样品上进行的。结果表明,针迹有效地桥接和阻止了分层裂纹,并减少了高达40%的分层增长。还表明,增加针迹密度在最小化分层区域方面比增加针迹线厚度(减少8%)更有效(减少23%)。一种新的基于经验的分层减少法则(DRL)已经被制定出来,以预测由于冲击载荷导致的缝合复合材料的分层减少量。 DRL已通过大量已发表的文献结果进行了进一步验证,这些结果已显示出良好的一致性和与预测曲线的极佳一致性。与作者先前在缝制复合材料的模式I断裂分层方面的工作进行了比较,并讨论了缝线在冲击引起的分层中的有效性(主要是模式II,没有缝线断裂)。

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