A study on the influence of cohesive zone interface element strength parameters on mixed mode behaviour

被引:77
作者
Harper, Paul W. [1 ]
Sun, Lu [2 ]
Hallett, Stephen R. [1 ]
机构
[1] Univ Bristol, Adv Composites Ctr Innovat & Sci, Bristol BS8 1TR, Avon, England
[2] Aviat Enterprises Ltd, Membury Airfield, Lambourn RG17 7TJ, Berks, England
关键词
Polymer-matrix composites (PMCs); Delamination; Fracture; Finite element analysis; PROGRESSIVE DELAMINATION; COMPOSITE; SIMULATION; FRACTURE; GROWTH; INITIATION; SPECIMENS; STRESS;
D O I
10.1016/j.compositesa.2011.12.016
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper presents a detailed study of the influence of maximum interfacial stress on interface element analyses for composites delamination. The development of the non-linear cohesive zone ahead of a crack tip is analysed with respect to length, stress distribution and mode ratio. The energy absorbed by interface elements is compared with the crack tip strain energy release rate from fracture mechanics analyses. These studies are performed initially on standard fracture toughness specimens, where mode-ratio is fixed by the applied displacement constraints. Results show close agreement with linear elastic fracture mechanics solutions. A simple ply drop specimen is then modelled, where the mode ratio is not constrained by the boundary conditions, and results are compared with the Virtual Crack Closure Technique. In this case maximum interfacial stress has a far greater influence on the numerical results, due to its significant influence on cohesive zone length, mode ratio and energy absorbed. (c) 2012 Elsevier Ltd. All rights reserved.
引用
收藏
页码:722 / 734
页数:13
相关论文
共 25 条
[1]   Finite element interface models for the delamination analysis of laminated composites: Mechanical and computational issues [J].
Alfano, G ;
Crisfield, MA .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 2001, 50 (07) :1701-1736
[2]  
[Anonymous], D5528012007E1 ASTM
[3]  
Asp LE, 2001, J COMPOS TECH RES, V23, P55, DOI 10.1520/CTR10914J
[4]   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
[5]   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
[6]   QUADRATIC STRESS CRITERION FOR INITIATION OF DELAMINATION [J].
BREWER, JC ;
LAGACE, PA .
JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (12) :1141-1155
[7]   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
[8]  
Camanho PP, 2003, J COMPOS MATER, V37, P1415, DOI 10.1177/002199803034505
[9]   Predicting progressive delamination of composite material specimens via interface elements [J].
Chen, J ;
Crisfield, M ;
Kinloch, AJ ;
Busso, EP ;
Matthews, FL ;
Qiu, Y .
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES, 1999, 6 (04) :301-317
[10]   In quest of virtual tests for structural composites [J].
Cox, Brian ;
Yang, Qingda .
SCIENCE, 2006, 314 (5802) :1102-1107