POST-BUCKLING BEHAVIOUR OF SIMPLY-SUPPORTED SQUARE PLATES

被引:41
作者
WALKER, AC
机构
来源
AERONAUTICAL QUARTERLY | 1969年 / 20卷
关键词
D O I
10.1017/S0001925900005035
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:203 / &
相关论文
共 20 条
[1]  
BIJLAARD PP, 1952, TN2640 NACA
[2]  
COAN JM, 1951, J APPL MECH-T ASME, V18, P143
[3]   THE CRIPPLING STRENGTH OF COMPRESSION ELEMENTS [J].
GERARD, G .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (01) :37-52
[4]  
HEIMERL GJ, 1949, TN1817 NACA
[5]  
HEMP WS, 1945, RM2178 ARC
[6]  
HU PC, 1946, TN1124 NACA
[7]  
LEVY S, 1942, TR737 NACA
[8]   THE ULTIMATE STRENGTH OF ALUMINUM-ALLOY FORMED STRUCTURAL SHAPES IN COMPRESSION [J].
NEEDHAM, RA .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (04) :217-229
[9]  
NISHINO F, 1964, THESIS LEHIGH U
[10]  
PERRY SH, 1966, THESIS U LONDON