Intralaminar hybrid configurations on the impact resistance of Carbon/ Kevlar plain-woven composite plates

被引:0
|
作者
Wu, Hang [1 ,3 ,4 ]
Zhao, Zhenqiang [1 ,3 ,4 ]
Bai, Yang [1 ,3 ,4 ]
Fang, Shilin [1 ,3 ,4 ]
Ma, Dayou [5 ]
Zhang, Chao [2 ,3 ]
机构
[1] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Sch Civil Aviat, Xian 710072, Peoples R China
[3] Joint Int Res Lab Impact Dynam & Its Engn Applicat, Xian 710072, Shaanxi, Peoples R China
[4] Natl Key Lab Strength & Struct Integr, Xian 710072, Peoples R China
[5] Politecn Milan, Dept Mech Engn, Via Masa 1, I-20156 Milan, Italy
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
Plain-woven composites; Intralaminar hybrid; High-velocity impact; Finite element model; LOW-VELOCITY IMPACT; FRACTURE-TOUGHNESS; DAMAGE MODEL; BEHAVIOR; HYBRIDIZATION; FAILURE; BASALT;
D O I
10.1016/j.tws.2024.112895
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Intralaminar hybridization with Kevlar is an effective approach to enhance the impact resistance of carbon fiber- reinforced composite plates. This study investigates the influence of different intralaminar hybrid configurations on the impact resistance of plain-woven composite plates. Carbon/Kevlar hybrid composite plates with various configurations were fabricated and subjected to high-velocity impact tests, accompanied by numerical simulations based on a multi-scale modeling framework considering elastoplasticity of Kevlar tension-compression asymmetry. The results reveal that integrating Kevlar fibers into carbon fiber plain-woven composite plates significantly improves impact resistance by shifting the dominant failure mode from brittle fracture of carbon fibers to the fiber pull-out of Kevlar bundles. Additionally, reducing the number of carbon/Kevlar interwoven regions further enhances the impact resistance of hybrid composite plates with the same Kevlar content.
引用
收藏
页数:12
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