Exact solution for buckling of axially-compressed cylindrical panels with frames attached to the circular edges

被引：3

作者：

Soares, P. T. M. L. ^{[1
]}

Santana, R. C. ^{[2
]}

Lucena Neto, E. ^{[2
]}

Monteiro, F. A. C. ^{[2
]}

Souza Neto, A. F. ^{[2
]}

Queiroz, P. I. B. ^{[2
]}

机构：

[1] Ctr Estudos & Projetos Engn Aeronaut, BR-01552000 Sao Paulo, SP, Brazil

[2] Inst Tecnol Aeronaut, BR-12228900 Sao Jose Dos Campos, SP, Brazil

来源：

LATIN AMERICAN JOURNAL OF SOLIDS AND STRUCTURES | 2020年 / 17卷 / 08期

关键词：

Cylindrical panel; Buckling; Exact solution; Frame;

D O I：

10.1590/1679-78255903

中图分类号：

TU [建筑科学];

学科分类号：

0813 ;

摘要：

This paper presents an exact solution for the boundary-value problem which describes the linear buckling of axially-compressed cylindrical panels with frames attached to the circular edges. The boundary conditions differ from the classical simply supported ones, often assumed for design purposes, in the sense that the torsion resisted by the frames are also taken into account. The quality of the results reported herein may be valuable benchmark data.

引用

页码：1 / 21

页数：21

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