Delamination growth directionality and the subsequent migration processes - The key to damage tolerant design

被引:49
作者
Canturri, Carla [1 ]
Greenhalgh, Emile S. [1 ]
Pinho, Silvestre T. [1 ]
Ankersen, Jesper [1 ]
机构
[1] Imperial Coll London, Composites Ctr, London SW7 2AZ, England
关键词
Polymer-matrix composites (PMCs); Delamination; Fractography; Prepreg; DOUBLE-CANTILEVER BEAM; COMPOSITES; LAMINATE; CRITERIA; FRACTURE;
D O I
10.1016/j.compositesa.2013.07.004
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Delamination has been recognised as one of the most challenging hurdles in using laminated composites, and has been the focus of considerable research over the last three decades. The research reported in this paper investigated the influence of ply interface on the delamination propagation processes. Experimental evidence is presented which illustrates that delamination does not grow in a self-similar manner. Instead, delaminations were shown to propagate preferentially in the direction of one ply at the delaminating interface; which ply was dictated by the orientation of the principal delaminating stress at the ply interface. In conjunction with the experimental studies, an initial methodology for modelling delamination directionality is presented. The results of this study have considerable implications for tailoring stacking sequences to promote delamination migration and thus enhance damage tolerance. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:79 / 87
页数:9
相关论文
共 19 条
[1]   The effect of weave pattern and crack propagation direction on mode I delamination resistance of woven glass and carbon composites [J].
Alif, N ;
Carlsson, LA ;
Boogh, L .
COMPOSITES PART B-ENGINEERING, 1998, 29 (05) :603-611
[2]   Dependence of fracture toughness of composite laminates on interface ply orientations and delamination growth direction [J].
Andersons, J ;
König, M .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (13-14) :2139-2152
[3]   Prediction of size effects in notched laminates using continuum damage mechanics [J].
Camanho, P. P. ;
Maimi, P. ;
Davila, C. G. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2007, 67 (13) :2715-2727
[4]  
Canturri C, 2011, ICCM 18 JEJ ISL AUG
[5]  
Davidson BD, 1995, J COMPOS MAT, V29
[6]   Fractographic observations on delamination growth and the subsequent migration through the laminate [J].
Greenhalgh, Emile S. ;
Rogers, Charlotte ;
Robinson, Paul .
COMPOSITES SCIENCE AND TECHNOLOGY, 2009, 69 (14) :2345-2351
[7]  
Greenhalgh ES, 2009, WOODHEAD PUBL MATER, P1
[8]   FAILURE CRITERIA FOR UNIDIRECTIONAL FIBER COMPOSITES [J].
HASHIN, Z .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1980, 47 (02) :329-334
[9]  
Hikosaka Y, 2011, P ICCM 18 JEJ ISL AU
[10]   DAMAGE MECHANISM CHARACTERIZATION IN COMPOSITE DAMAGE TOLERANCE INVESTIGATIONS [J].
HULL, D ;
SHI, YB .
COMPOSITE STRUCTURES, 1993, 23 (02) :99-120