A 3-D FINITE-DIFFERENCE SOLUTION FOR ORTHOTROPIC LAMINATED COMPOSITES USING CURVILINEAR COORDINATES

被引：5
作者：
ALTUS, E
BARYOSEPH, P
机构：
来源：
COMPUTERS & STRUCTURES | 1983年 / 17卷 / 04期
关键词：
D O I：
10.1016/0045-7949(83)90051-2
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
引用
收藏
页码：573 / 577
页数：5
相关论文
共 16 条
[1]  
ALTUS E, 1980, J COMPOS MATER, V14, P21
[2]   A 3-D FRACTURE-MECHANICS APPROACH TO THE STRENGTH OF COMPOSITE-MATERIALS [J].
ALTUS, E ;
ROTEM, A .
ENGINEERING FRACTURE MECHANICS, 1981, 14 (03) :637-&
[3]   CALCULATION OF INTERLAMINAR STRESS-CONCENTRATION IN COMPOSITE LAMINATES [J].
BARYOSEPH, P ;
PIAN, THH .
JOURNAL OF COMPOSITE MATERIALS, 1981, 15 (MAY) :225-239
[4]  
BARYOSEPH P, 1983, COMPUT METH APPL MEC
[5]   FLEXIBLE FINITE-DIFFERENCE STENCILS FROM ISOPARAMETRIC FINITE-ELEMENTS [J].
FREY, WH .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1977, 11 (11) :1653-1665
[6]  
KASSIR MK, 1975, MECHANICS FRACTURE, V2
[7]   STRESS-ANALYSIS OF HOLES IN ANGLE-PLY LAMINATES - AN EFFICIENT ASSUMED STRESS SPECIAL-HOLE-ELEMENT APPROACH AND A SIMPLE ESTIMATION METHOD [J].
NISHIOKA, T ;
ATLURI, SN .
COMPUTERS & STRUCTURES, 1982, 15 (02) :135-147
[8]   INTERLAMINAR STRESS SINGULARITIES AT A STRAIGHT FREE EDGE IN COMPOSITE LAMINATES [J].
RAJU, IS ;
CREWS, JH .
COMPUTERS & STRUCTURES, 1981, 14 (1-2) :21-28
[9]  
RYBICKI EF, 1973, AFMLTR73100 BATTL CO
[10]  
SAVIN GN, 1970, NASA TTF607
12