Predicting the effect of through-thickness compressive stress on delamination using interface elements

被引:89
作者
Li, Xiangqlan [1 ]
Hallett, Stephen R. [1 ]
Wisnom, Michael R. [1 ]
机构
[1] Univ Bristol, Adv Composite Ctr Innovat & Sci, Bristol BS8 1TR, Avon, England
关键词
mechanical properties; delamination; fracture; finite element analysis (FEA); interface elements;
D O I
10.1016/j.compositesa.2007.11.005
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The failure of interface elements is typically based on interactive mixed mode criteria for both initiation and propagation of damage. The effect of tensile through-thickness stress is normally taken into account in combination with interlaminar shear stress. When the through-thickness stress is compressive, however, its effect is usually ignored and the failure of interface elements is considered to be pure mode II. Experiments on single-lap, cut-ply and dropped-ply specimens however show that the compressive through-thickness stress can greatly increase the delamination failure stress and cannot be simply neglected. The influence of compressive stress on mode II damage evolution is investigated numerically based on the cut-ply and dropped-ply experiments. A new interfacial failure model with modified failure initiation and propagation criteria is proposed to take the effect of compression on matrix shear strength and mode II critical fracture energy, G(IIC), into account. The new model uses one independently determined parameter to relate the compression to the increase in interlaminar shear strength and G(IIC). With the new failure criterion applied, two types of cut-ply models and two types of dropped-ply models, using the same input parameter, all produce excellent correlation with experimental delamination stresses. As a validation case the single-lap model was run with the new criterion and the same input parameters and this also achieves very good correlation with the experimental failure stress. (c) 2007 Elsevier Ltd. All rights reserved.
引用
收藏
页码:218 / 230
页数:13
相关论文
共 35 条
[1]  
[Anonymous], 1967, J PROC
[2]  
BEER G, 1985, INT J NUMER METH ENG, V21, P585, DOI 10.1002/nme.1620210402
[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]   Simulating DCB, ENF and MMB experiments using shell elements and a cohesive zone model [J].
Borg, R ;
Nilsson, L ;
Simonsson, K .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (02) :269-278
[5]   QUADRATIC STRESS CRITERION FOR INITIATION OF DELAMINATION [J].
BREWER, JC ;
LAGACE, PA .
JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (12) :1141-1155
[6]   Fracture analysis of composite co-cured structural joints using decohesion elements [J].
Camanho, PP ;
Dávila, CG ;
Pinho, ST .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2004, 27 (09) :745-757
[7]  
Camanho PP, 2003, J COMPOS MATER, V37, P1415, DOI [10.1177/0021998303034505, 10.1177/002199803034505]
[8]   Delamination failure investigation for out-of-plane loading in laminates [J].
Christensen, RM ;
DeTeresa, SJ .
JOURNAL OF COMPOSITE MATERIALS, 2004, 38 (24) :2231-2238
[9]  
CUI W, 1994, J COMPOS TECH RES, V16, P329, DOI 10.1520/CTR10593J
[10]  
CZARNOCKI P, 2003, UAV NET M 7 PAR JUN