A review on the multi-scale simulation of Z-pinned composite laminates

被引:23
作者
Cheng, Jisiyuan [1 ]
Xu, Yingjie [1 ,2 ,3 ]
Zhang, Weihong [1 ]
Liu, Weiwei [1 ]
机构
[1] Northwestern Polytech Univ, State IJR Ctr Aerosp Design & Addit Mfg, Xian 710072, Shaanxi, Peoples R China
[2] Northwestern Polytech Univ, Shaanxi Prov Key Lab Aeronaut & Aerosp Struct Tech, Xian 710072, Shaanxi, Peoples R China
[3] Northwestern Polytech Univ, POB 68, Xian 710072, Shaanxi, Peoples R China
关键词
Z-pin; Composite laminates; Multi-scale simulation; Finite Element; MODE-I DELAMINATION; INTERLAMINAR FRACTURE-TOUGHNESS; THROUGH-THICKNESS REINFORCEMENT; LOW-VELOCITY IMPACT; PROGRESSIVE FAILURE ANALYSIS; WOVEN FABRIC COMPOSITES; FINITE-ELEMENT-ANALYSIS; COHESIVE ZONE MODEL; RECTANGULAR Z-PINS; BRAIDED COMPOSITES;
D O I
10.1016/j.compstruct.2022.115834
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Z-pinned composite laminates have been increasingly applied to aircraft and other lightweight products. This paper reviews published multi-scale research into polymer composite laminates reinforced by z-pins. Basic knowledge of multi-scale strategy and z-pin reinforcements has been reviewed at first. Then the methodology and relevant research progress of micro-and macro-scale models are separately presented. Z-pin bridging micro mechanisms and microstructure can be characterized by micro-scale modelling. The effects of z-pinning on the mechanical performances of composite laminates can be analyzed by the macro-scale models. The traction separation laws can be derived from micro-scale models and further incorporated into macro-scale models, bridging two models together. Most finite element models show satisfactory agreement with experimental phenomena and analytical conclusions. Gaps in the multi-scale simulation of z-pinned composite laminates and future research opportunities are identified.
引用
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页数:26
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