Failure prediction and strength improvement of uni-directional composite single lap bonded joints

被引:72
作者
Kim, Kwang-Soo
Yi, Yeong-Moo
Cho, Gwang-Rae
Kim, Chun-Gon
机构
[1] Korea Aerosp Res Inst, Dept Mat & Struct, Taejon 305333, South Korea
[2] Korea Adv Inst Sci & Technol, Dept Mech Engn, Div Aerosp Engn, Taejon 305701, South Korea
关键词
composite bonded joints; failure prediction; adhesive failure; single lap;
D O I
10.1016/j.compstruct.2007.02.005
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A methodology is presented for the failure prediction of the composite single lap bonded joints considering both the composite adherend and the bondline failures. An elastic-perfectly plastic model of the adhesive and a delamination failure criterion were used in the methodology. The failure predictions using the finite element analysis and the proposed methodology were performed. The failure prediction results such as failure mode and strength showed very good agreements with the test results for the joint specimens with various bonding methods and parameters. Based on the numerical investigation, the optimal joint strength condition was found and a new joint strength improvement technique was suggested. The suggested technique was verified to have a significant effect on the joint strength improvement. (c) 2007 Elsevier Ltd. All rights reserved.
引用
收藏
页码:513 / 520
页数:8
相关论文
共 16 条
[1]   QUADRATIC STRESS CRITERION FOR INITIATION OF DELAMINATION [J].
BREWER, JC ;
LAGACE, PA .
JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (12) :1141-1155
[2]   Failure of adhesive bonded composite lap shear joints with embedded precrack [J].
Cheuk, PT ;
Tong, LY .
COMPOSITES SCIENCE AND TECHNOLOGY, 2002, 62 (7-8) :1079-1095
[3]   A UNIFIED APPROACH FOR PREDICTING THE STRENGTH OF CRACKED AND NON-CRACKED ADHESIVE JOINTS [J].
CROCOMBE, AD ;
RICHARDSON, G ;
SMITH, PA .
JOURNAL OF ADHESION, 1995, 49 (3-4) :211-244
[4]  
*CYT ENG MAT INC, FM73 TOUGH EP FILM
[5]   Understanding and control of adhesive crack propagation in bonded joints between carbon fibre composite adherends II. Finite element analysis [J].
Guild, FJ ;
Potter, KD ;
Heinrich, J ;
Adams, RD ;
Wisnom, MR .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2001, 21 (06) :445-453
[6]  
HUANG H, 2000, P AM SOC COMPOS, V15, P599
[7]   STRENGTH AND FAILURE MODES OF BONDED SINGLE LAP JOINTS BETWEEN CROSS-PLY ADHERENDS [J].
KAIROUZ, KC ;
MATTHEWS, FL .
COMPOSITES, 1993, 24 (06) :475-484
[8]   Stress concentrations caused by bond cracks in single-lap adhesive composite joints [J].
Kayupov, M ;
Dzenis, YA .
COMPOSITE STRUCTURES, 2001, 54 (2-3) :215-220
[9]   The influence of adhesive bondline thickness imperfections on stresses in composite joints [J].
Kim, H .
JOURNAL OF ADHESION, 2003, 79 (07) :621-642
[10]   Investigation of optimal surface treatments for carbon/epoxy composite adhesive joints [J].
Kim, JK ;
Kim, HS ;
Lee, DG .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2003, 17 (03) :329-352