ANALYSIS OF STITCHED LAMINATED ENF SPECIMENS FOR INTERLAMINAR MODE-II FRACTURE-TOUGHNESS

被引:56
作者
JAIN, LK [1 ]
MAI, YW [1 ]
机构
[1] UNIV SYDNEY,DEPT MECH & MECHATR ENGN,CTR ADV MAT TECHNOL,SYDNEY,NSW 2006,AUSTRALIA
关键词
D O I
10.1007/BF00013069
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Two simple micromechanics based models are proposed to predict the effect of through-thickness reinforcement (stitching) on the improvement of delamination crack growth resistance in end-notched flexure (ENF) specimens. In the first model, it is assumed that stitches stretch elastically and then rupture when the load carried approaches the failure load. In the second model, it is assumed that stitches are discontinuous and that the stitch thread-matrix interface is completely frictional. Approximate closed form solutions for energy release rates are obtained, and the effects of stitch density, matrix-stitch thread interfacial shear stress, stitch thread diameter, volume fraction of stitches, critical energy release rate and Young's modulus are then examined. A simple design study for sizing the ENF specimen to minimise geometric nonlinear response is presented. The influences of interlaminar shear deformation and friction between the crack surfaces on the strain energy release rate are examined.
引用
收藏
页码:219 / 244
页数:26
相关论文
共 34 条
[1]   MODE-I DELAMINATION OF A 3-DIMENSIONAL FABRIC COMPOSITE [J].
BYUN, JH ;
GILLESPIE, JW ;
CHOU, TW .
JOURNAL OF COMPOSITE MATERIALS, 1990, 24 (05) :497-518
[2]   ON THE ANALYSIS AND DESIGN OF THE END NOTCHED FLEXURE (ENF) SPECIMEN FOR MODE-II TESTING [J].
CARLSSON, LA ;
GILLESPIE, JW ;
PIPES, RB .
JOURNAL OF COMPOSITE MATERIALS, 1986, 20 (06) :594-604
[3]   MODELING LAMINATED COMPOSITE STRUCTURES AS ASSEMBLAGE OF SUBLAMINATES [J].
CHATTERJEE, SN ;
RAMNATH, V .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1988, 24 (05) :439-458
[4]   MIXED-MODE DELAMINATION FRACTURE IN LAMINATED COMPOSITES [J].
CHATTERJEE, SN ;
DICK, WA ;
PIPES, RB .
COMPOSITES SCIENCE AND TECHNOLOGY, 1986, 25 (01) :49-67
[5]   ANALYSIS OF TEST SPECIMENS FOR INTERLAMINAR MODE-II FRACTURE-TOUGHNESS .1. ELASTIC LAMINATES [J].
CHATTERJEE, SN .
JOURNAL OF COMPOSITE MATERIALS, 1991, 25 (05) :470-493
[6]  
CHATTERJEE SN, 1984, ASTM STP, V836, P161
[7]  
de Charentenay F., 1982, ASTM STP, V836, P84
[8]  
DEVITT DF, 1980, J COMPOS MATER, V14, P270
[9]   ON THE IMPACT PERFORMANCE OF CARBON-FIBER LAMINATES WITH EPOXY AND PEEK MATRICES [J].
DOREY, G ;
BISHOP, SM ;
CURTIS, PT .
COMPOSITES SCIENCE AND TECHNOLOGY, 1985, 23 (03) :221-237
[10]  
DOW MB, 1989, 21ST INT SAMPE TECHN, P295