Crack equivalent concept applied to the fracture characterization of bonded joints under pure mode I loading

被引:239
作者
de Moura, M. F. S. F. [1 ]
Campilho, R. D. S. G. [1 ]
Goncalves, J. P. M. [2 ]
机构
[1] Univ Porto, Fac Engn, Dept Engn Mecan & Gestao Ind, P-4200465 Oporto, Portugal
[2] IBM Corp, Thomas J Watson Res Ctr, Dept Math Sci, Yorktown Hts, NY 10598 USA
关键词
adhesive joints; fracture toughness; finite element analysis (FEA); cohesive damage models;
D O I
10.1016/j.compscitech.2008.04.003
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this work, an accurate and suitable data reduction scheme is developed to measure the fracture energy of adhesive joints under pure mode I loading. The method is based on the crack equivalent concept and is applied to the double cantilever beam specimen. Using the proposed methodology it is not necessary to measure the crack length during propagation, which can introduce non-negligible errors on the fracture energy measurements. Moreover, it accounts for the fracture process zone effects which can be significant when ductile adhesives are used. The new method was compared to classical data reduction schemes and was validated numerically using a trapezoidal mixed-mode cohesive damage model. The fracture characterization in mode I using a developed trapezoidal cohesive damage model is performed by an inverse method. Excellent agreement between the numerical and experimental R-curves was achieved demonstrating the adequacy of the proposed method. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:2224 / 2230
页数:7
相关论文
共 16 条
[1]   The stress-elongation relation for an adhesive layer loaded in peel using equilibrium of energetic forces [J].
Andersson, T ;
Stigh, U .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2004, 41 (02) :413-434
[2]   Double cantilever beam testing of repaired carbon fibre composites [J].
Bader, MG ;
Hamerton, I ;
Hay, JN ;
Kemp, M ;
Winchester, S .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2000, 31 (06) :603-608
[3]   The use of a cohesive zone model to study the fracture of fibre composites and adhesively-bonded joints [J].
Blackman, BRK ;
Hadavinia, H ;
Kinloch, AJ ;
Williams, JG .
INTERNATIONAL JOURNAL OF FRACTURE, 2003, 119 (01) :25-46
[4]   Modelling single and double-lap repairs on composite materials [J].
Campilho, RDSG ;
de Moura, MFSF ;
Domingues, JJMS .
COMPOSITES SCIENCE AND TECHNOLOGY, 2005, 65 (13) :1948-1958
[5]   Numerical simulation of the ENF test for the mode-II fracture characterization of bonded joints [J].
De Moura, MFSF .
JOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, 2006, 20 (01) :37-52
[6]   Influence of intralaminar cracking on the apparent interlaminar mode I fracture toughness of cross-ply laminates [J].
de Moura, MFSF ;
Pereira, AB ;
de Morais, AB .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2004, 27 (09) :759-766
[7]   Mixed mode failure criteria for a glass/epoxy composite and an adhesively bonded composite/composite joint [J].
Ducept, F ;
Davies, P ;
Gamby, D .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2000, 20 (03) :233-244
[8]  
Kanninen MF., 1985, Advanced Fracture Mechanics
[9]  
Kinloch A. J., 1987, ADHES ADHES
[10]   Shear behaviour of adhesive layers [J].
Leffler, K. ;
Alfredsson, K. S. ;
Stigh, U. .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2007, 44 (02) :530-545