ANALYSIS OF TEST SPECIMENS FOR INTERLAMINAR MODE-II FRACTURE-TOUGHNESS .1. ELASTIC LAMINATES

被引:32
作者
CHATTERJEE, SN
机构
[1] Materials Sciences Corporation, Blue Bell, PA 19422
关键词
DELAMINATION FRACTURE; COMPOSITE LAMINATES; MODE-II TOUGHNESS; THICK BEAM; END-NOTCHED FLEXURE;
D O I
10.1177/002199839102500501
中图分类号
TB33 [复合材料];
学科分类号
摘要
Results from approximate and exact stress analyses are reported for elastic stress and displacement fields in two interlaminar mode II fracture toughness specimens. End-notched flexure tests for laminates and unidirectional composites are studied in detail. Based on approximate closed form solutions for energy release rates procedures are suggested for fitting compliance versus delamination length data. Such procedures should be followed when through the thickness shear moduli of the layers are small as compared to axial moduli.
引用
收藏
页码:470 / 493
页数:24
相关论文
共 31 条
[1]  
[Anonymous], 1958, FRACTURE
[2]  
BENTHEM JP, 1973, METHODS ANAL SOLUTIO
[3]  
BRADLEY WL, 1982, AFOSRTR82 US AIR FOR
[4]  
Carlsson L. A., 1986, Journal of Reinforced Plastics and Composites, V5, P170, DOI 10.1177/073168448600500302
[5]   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
[7]   MODELING LAMINATED COMPOSITE STRUCTURES AS ASSEMBLAGE OF SUBLAMINATES [J].
CHATTERJEE, SN ;
RAMNATH, V .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1988, 24 (05) :439-458
[8]   MIXED-MODE DELAMINATION FRACTURE IN LAMINATED COMPOSITES [J].
CHATTERJEE, SN ;
DICK, WA ;
PIPES, RB .
COMPOSITES SCIENCE AND TECHNOLOGY, 1986, 25 (01) :49-67
[9]  
CHATTERJEE SN, 1979, MODERN DEV COMPOSITE, P1
[10]  
CHATTERJEE SN, 1982, NADC8103460 NAV AIR, P92