USE OF CURVILINEAR FIBER FORMAT IN COMPOSITE STRUCTURE DESIGN

被引:222
作者
HYER, MW [1 ]
CHARETTE, RF [1 ]
机构
[1] DAVID W TAYLOR NAVAL SHIP RES & DEV CTR,DIV SUBMARINE STRUCT,BETHESDA,MD 20084
关键词
11;
D O I
10.2514/3.10697
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:1011 / 1015
页数:5
相关论文
共 11 条
[1]  
Cooper, 1972, THESIS WASHINGTON U
[2]  
EVANS DO, 1989, 34 INT SAMPE S EXH M, P1822
[3]   ALLEVIATION OF STRESS-CONCENTRATION WITH ANALOG REINFORCEMENT [J].
HELLER, RA ;
CHIBA, T .
EXPERIMENTAL MECHANICS, 1973, 13 (12) :519-525
[4]   EFFECT OF BOLT LOAD PROPORTIONING ON THE CAPACITY OF MULTIPLE-BOLT COMPOSITE JOINTS [J].
HYER, MW ;
CHASTAIN, PA .
JOURNAL OF AIRCRAFT, 1988, 25 (02) :184-189
[5]  
HYER MW, 1988, VPIE888 VIRG POL I S
[6]  
HYER MW, 1987, TR875 U MAR DEP MECH
[7]  
KATZ Y, 1989, 4 TECHN C COMP MAT B, P62
[8]  
KNOBLACH GM, 1989, SAMPE J, V25, P9
[9]   IMPORTANCE OF ANISOTROPY ON BUCKLING OF COMPRESSION-LOADED SYMMETRICAL COMPOSITE PLATES [J].
NEMETH, MP .
AIAA JOURNAL, 1986, 24 (11) :1831-1835
[10]  
Tsai Stephen W., 1987, COMPOSITES DESIGN, VThird