ASSUMED STRESS FINITE-ELEMENT ANALYSIS OF THROUGH-CRACKS IN ANGLE-PLY LAMINATES

被引：13
作者：
NISHIOKA, T
ATLURI, SN
机构：
来源：
AIAA JOURNAL | 1980年 / 18卷 / 09期
关键词：
D O I：
10.2514/3.50862
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：1125 / 1132
页数：8
相关论文
共 11 条
[1]  
[Anonymous], ADV COMPUTER METHODS
[2]   TRACTION BOUNDARY-CONDITIONS IN HYBRID-STRESS FINITE-ELEMENT MODEL [J].
ATLURI, SN ;
RHEE, HC .
AIAA JOURNAL, 1978, 16 (05) :529-531
[3]  
HILTON PD, 1975, FRACTURE MECHANICS C, P3
[4]   FINITE ELEMENT SOLUTIONS FOR LAMINATED THICK PLATES [J].
MAU, ST ;
TONG, P ;
PIAN, THH .
JOURNAL OF COMPOSITE MATERIALS, 1972, 6 (APR) :304-&
[5]  
NISHIOKA T, UNPUBLISHED
[6]  
PANGANO NJ, 1970, J COMPOSITE MATERIAL, V4, P20
[7]   DERIVATION OF ELEMENT STIFFNESS MATRICES BY ASSUMED STRESS DISTRIBUTIONS [J].
PIAN, THH .
AIAA JOURNAL, 1964, 2 (07) :1333-1336
[8]  
PIAN THH, 1972, ADV APPLIED MECHANIC, V12, P2
[9]  
SIH GC, 1968, FRACTURE, V2, P68
[10]   MULTILAYER HYBRID-STRESS FINITE-ELEMENT ANALYSIS OF A THROUGH-THICKNESS EDGE CRACK IN A +/-45DEGREES LAMINATE [J].
WANG, SS ;
MANDELL, JF ;
MCGARRY, FJ .
ENGINEERING FRACTURE MECHANICS, 1977, 9 (01) :217-238
12