Effect of manufacturing methods on the shear strength of composite single-lap bonded joints

被引：67
|
作者：
Song, Min-Gyu [1 ]
Kweon, Jin-Hwe [1 ]
Choi, Jin-Ho [1 ]
Byun, Jai-Hyun [2 ]
Song, Min-Hwan [3 ]
Shin, Sang-Joon [3 ]
Lee, Tae-Joo [3 ]
机构：
[1] Gyeongsang Natl Univ, Sch Mech & Aerosp Engn, Res Ctr Aircraft Parts Technol, Jinju 660701, Gyeongnam, South Korea
[2] Gyeongsang Natl Univ, Dept Ind & Syst Engn, Jinju 660701, Gyeongnam, South Korea
[3] Korea Aerosp Ind Ltd, Div Res & Dev, Sacheon 664802, Gyeongnam, South Korea
来源：
COMPOSITE STRUCTURES | 2010年 / 92卷 / 09期
基金：
新加坡国家研究基金会;
关键词：
Manufacturing method; Cocuring; Secondary bonding; Co-bonding; ADHESIVE JOINTS; LAMINATED COMPOSITES; FAILURE; PREDICTION; ADHERENDS; BEHAVIOR; MODE;
D O I：
10.1016/j.compstruct.2009.08.041
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The present paper experimentally addresses the effect of manufacturing methods on the strength of composite bonded joints. A total of 391 specimens, manufactured by four different fabrication methods, were tested. For each method, various overlap lengths, adherend thicknesses and lay-up patterns were examined. The failure strength was higher in thicker adherend joints and lower in specimens with larger overlap length. Results showed that the secondary bonded joints had higher strength than the co-bonded and adhesively cocured joints and yielded similar strength compared with the non-adhesive cocured case. Changes in the stacking sequence also affected the interlaminar stresses and failure loads. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码：2194 / 2202
页数：9
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