损伤容限
材料科学
复合材料
抗冲击性
复合材料层合板
复合数
航空航天
艾氏冲击强度试验
环氧树脂
结构工程
工程类
极限抗拉强度
航空航天工程
作者
Hussein Dalfi,Khayale Jan,Zeshan Yousaf,Mazhar Hussain Peerzada
标识
DOI:10.1177/00219983231209718
摘要
As the use of composite laminates are unceasingly increasing more and more in many applications, the in-depth understanding about the impact response of composite laminates in certain areas like sport, aerospace and automotive has gained more attention of the designers and scientists over the last two decades. The authors have focused to review the impact properties of fibre reinforced composites particularly impact damage tolerance. Impact resistance, damage tolerance, composite failure and methods of assessing damage tolerance are presented. Furthermore, the approaches for improving damage tolerance such as fibre architectures resin system, and hybridisation using either yarn hybridisation or hybrid layers are discussed. In the end, a survey of modelling the impact damage of laminated composites is made by considering the inter-laminar and intra-laminar failures as key point for evaluating the response of laminates under impact loading.
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