Low-velocity impact behavior and residual tensile strength of CFRP laminates

被引:85
作者
Zhou, Jianwu [1 ]
Liao, Binbin [2 ]
Shi, Yaoyao [1 ]
Zuo, Yangjie [3 ]
Tuo, Hongliang [4 ]
Jia, Liyong [5 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Shaanxi, Peoples R China
[2] Zhejiang Univ, Inst Proc Equipment, Hangzhou 300027, Zhejiang, Peoples R China
[3] Sichuan Univ, Sch Aeronaut & Astronaut, Chengdu 610065, Sichuan, Peoples R China
[4] Northwestern Polytech Univ, Sch Aeronaut, Xian 710072, Shaanxi, Peoples R China
[5] First Aircraft Inst Aviat Ind Corp, Xian 710089, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
Impactor parameters; Layup patterns; Impact behaviors; Tensile strength; STACKING-SEQUENCE; DAMAGE; COMPOSITES; PREDICTION; OPTIMIZATION; STIFFNESS; DIAMETER; EPOXY; SHAPE;
D O I
10.1016/j.compositesb.2018.10.090
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper experimentally studies the low-velocity impact behaviors and residual tensile strength of carbon fiber reinforced plastics (CFRP) laminates. Firstly, the effects of four factors, i.e. impact angle, impactor diameter, the proportion of ply orientation and stacking sequence, on the impact responses of laminates are studied. The damage characteristics are evaluated by dent depth, delamination damage projection area (DDPA) and energy dissipation. Secondly, the tensile responses of the laminates after impact are investigated based on residual tensile strength (RTS). Finally, the correlations between the four damage evaluation criteria, i.e. dent depth, DDPA, energy dissipation and RTS, are sorted out. Experimental results demonstrate that the four factors have significant effects on the impact behaviors of laminates in different ways. The DDPA is negatively correlated with the dent depth of laminates, and the dent depth can be treated as an important reference for the RTS. Besides, a fracture phenomenon, i.e. a clear band of fiber fracture around the impact area after impact, has been observed and discussed.
引用
收藏
页码:300 / 313
页数:14
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