Stability of a cylindrical shell under axial compression

被引：0
|
作者：
Bakhtieva L.U. [1 ]
Tazyukov F.K. [1 ]
机构：
[1] Kazan (Volga Region) Federal University, ul. Kremlevskaya 18, Kazan
来源：
Russ. Aeronaut. | / 1卷 / 106-111期
关键词：
buckling load; deflection; shell; stability;
D O I：
10.3103/S1068799815010171
中图分类号：
学科分类号：
摘要：
A new approach to solving the task of stability for a circular cylindrical shell under axial compression is presented, taking into account the dynamic buckling. The modification of the algorithm for solving the known problem by the Ritz method is also proposed that allows investigating the effect of geometrical factors on the buckling load. © 2015, Allerton Press, Inc.
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页码：106 / 111
页数：5
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