Experimental and Numerical Study of Adhesively Bonded CFRP Scarf-Lap Joints Subjected to Tensile Loads

被引:27
|
作者
Li, Jianfeng [1 ]
Yan, Ying [1 ]
Liang, Zudian [1 ]
Zhang, Taotao [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
来源
JOURNAL OF ADHESION | 2016年 / 92卷 / 01期
关键词
Composites; Epoxy; Finite element analysis; Scarf-lap joints; Stress distribution; STRESS-ANALYSIS; MODELS;
D O I
10.1080/00218464.2014.987343
中图分类号
TQ [化学工业];
学科分类号
0817 ;
摘要
The tensile performance of adhesively bonded CFRP scarf-lap joints was investigated experimentally and numerically. In this study, scarf angle and adherend thickness were chosen as design parameters. The lap shear strength is not directly proportional to scarf angle and adherend thickness for the brittle adhesive studied in the paper. The major failure mode includes cohesive shear failure and adherend delamination failure. The results present a stepped failure morphology along the bondline in the adhesive layer. A finite element model based on cohesive zone model was established to further investigate the stress distribution of scarf-lap joints with different lap parameters. The numerical results were compared with the experiment results, showing a good agreement, thus verifying the validity of the established numerical model.
引用
收藏
页码:1 / 17
页数:17
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