MODELING AND IDENTIFICATION OF THE MECHANICAL-BEHAVIOR OF COMPOSITE LAMINATES IN COMPRESSION

被引:56
作者
ALLIX, O
LADEVEZE, P
VITTECOQ, E
机构
[1] UNIV PARIS 06,ENS CACHAN,MECAN & TECHNOL LAB,CNRS,61 AVE PRESIDENT WILSON,F-94235 CACHAN,FRANCE
[2] UNIV EVRY VAL ESSONE,IUT,GMP,F-91000 EVRY,FRANCE
[3] USTL,ENSAM,EC LILLE,LAB MECAN LILLE,CNRS,URA D1441,F-59651 VILLENEUVE DASCQ,FRANCE
关键词
CARBON EPOXY LAMINATES; COMPRESSION BEHAVIOR; 4-POINT BENDING TEST; MECHANICAL MODELING; LEE-HARRIS MICROMECHANICAL MODEL;
D O I
10.1016/0266-3538(94)90154-6
中图分类号
TB33 [复合材料];
学科分类号
摘要
It is shown that mechanical compression behaviour in the fibre direction for laminated carbon/epoxy structure can be predicted with an elastic non-linear model. For that purpose, a specific bending test has been developed. A model for any stacking sequence is proposed and verified in several tension, compression and bending tests. Finally, a possible explanation using the model proposed by Lee and Harris is developed.
引用
收藏
页码:35 / 42
页数:8
相关论文
共 24 条
[1]  
Adsit N., 1983, P S COMPR TEST HOM M, P175
[2]   A THERMOMECHANICAL CONSTITUTIVE THEORY FOR ELASTIC COMPOSITES WITH DISTRIBUTED DAMAGE .1. THEORETICAL DEVELOPMENT [J].
ALLEN, DH ;
HARRIS, CE ;
GROVES, SE .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1987, 23 (09) :1301-1318
[3]   INTERLAMINAR INTERFACE MODELING FOR THE PREDICTION OF DELAMINATION [J].
ALLIX, O ;
LADEVEZE, P .
COMPOSITE STRUCTURES, 1992, 22 (04) :235-242
[4]  
ALLIX O, 1988, COMPTES RENDUS JNC6, P11
[5]  
ALLIX O, 1992, COMPT REND HUIT JOUR, P763
[6]  
ALLIX O, 1990, YIELDING DAMAGE FAIL, V5, P551
[7]  
GANSDSIREVINCON I, 1992, COMPTES RENDUS HUITI, P41
[8]  
GRANDIDIER JC, 1990, CR ACAD SCI II, V310, P1
[9]   DAMAGE MODELING OF THE ELEMENTARY PLY FOR LAMINATED COMPOSITES [J].
LADEVEZE, P ;
LEDANTEC, E .
COMPOSITES SCIENCE AND TECHNOLOGY, 1992, 43 (03) :257-267
[10]  
LADEVEZE P, 1992, 3RD P INT C COMP P 2, P1369