CONDITIONS FOR LAMINATED PLATES TO REMAIN FLAT UNDER INPLANE LOADING

被引:123
作者
LEISSA, AW
机构
关键词
D O I
10.1016/0263-8223(86)90022-X
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
引用
收藏
页码:261 / 270
页数:10
相关论文
共 8 条
[1]  
Ashton JE, 1970, THEORY LAMINATED PLA
[2]  
Ashton JE, 1969, PRIMER COMPOSITE MAT
[3]  
Chia C. Y., 1980, NONLINEAR ANAL PLATE
[4]   BUCKLING AND POST-BUCKLING BEHAVIOR OF COMPOSITE PLATES UNDER BIAXIAL LOADING [J].
HARRIS, GZ .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 1975, 17 (03) :187-202
[5]  
JONES RM, 1975, MECHANICS COMPOSITE
[6]  
Leissa A. W., 1985, AFWALTR853069 FLIGHT
[7]  
Lekhnitskii SG, 1968, ANISOTROPIC PLATES
[8]   POST-BUCKLING BEHAVIOR OF SIMPLY-SUPPORTED CROSS-PLY RECTANGULAR-PLATES [J].
PRABHAKARA, MK .
AERONAUTICAL QUARTERLY, 1976, 27 (NOV) :309-316