Failure load evaluation and prediction of hybrid composite double lap joints

被引:68
作者
Lee, Young-Hwan [2 ]
Lim, Do-Wan [1 ]
Choi, Jin-Ho [1 ]
Kweon, Jin-Hwe [1 ]
Yoon, Myung-Keun [3 ]
机构
[1] Gyeongsang Natl Univ, Sch Mech & Aerosp Engn, Res Ctr Aircraft Parts Technol, Jinju 660701, Gyeongnam, South Korea
[2] Hanyang Univ, Dept Mech Engn, Ansan 426791, Gyeonggi, South Korea
[3] S Dakota Sch Mines & Technol, Dept Mech Engn, Rapid City, SD 57701 USA
关键词
Hybrid composite joint; Damage zone theory; Failure Area Index (FAI); TO-ALUMINUM JOINTS; STIFFNESS BEHAVIOR; STRESS-ANALYSIS; FRACTURE; STRENGTH;
D O I
10.1016/j.compstruct.2010.05.002
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Hybrid joints are a combination of adhesive bonding and mechanical fastening and are known to combine the advantages of both joint types. In this paper, we evaluate and compare the strengths of mechanical joints, adhesive joints and hybrid composite joints. We manufactured and tested 10 hybrid joint specimens with different width-to-diameter (w/d) ratios, edge-to-diameter (e/d) ratios and adherend thicknesses. Additionally, the strengths of the hybrid joints were predicted using the Failure Area Index (FAI) method and the damage zone method, and we compared our theoretical predictions with our experimental results. From these data, we were able to predict hybrid joint strengths to within 23.0%. (C) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2916 / 2926
页数:11
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