Stability analysis of a cylindrical shell with a cut under axial compression and external pressure

被引:0
|
作者
Evdokimov, E. V. [1 ]
Safronov, V. S. [1 ]
Turkin, I. K. [1 ]
机构
[1] Moscow Aviat Inst State Univ Aerosp Technol, Moscow 125993, Russia
关键词
Cylindrical Shell; Critical Load; Axial Compression; Displacement Function; Total Potential Energy;
D O I
10.3103/S002565440701013X
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
引用
收藏
页码:104 / 119
页数:16
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