BUCKLING OF QUASISINUSOIDALLY CORRUGATED PLATES IN SHEAR

被引：1

作者：

TODA, S ^{[1
]}

SANBONGI, S ^{[1
]}

机构：

[1] NATL AEROSP LAB, STRUCT LAB, TOKYO, JAPAN

来源：

AIAA JOURNAL | 1986年 / 24卷 / 01期

关键词：

STRUCTURAL ANALYSIS;

D O I：

10.2514/3.8230

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper determines the buckling stress of quasisinusoidally corrugated plates in shear. Governing equations are obtained by the variations of potential energy, which is evaluated by assuming the buckling deflection components in the form of a Fourier series. An approximate but closed-form solution is then derived to determine the governing parameters of the problem. The present analytical results are compared favorably with both finite element methods and experimental results.

引用

页码：138 / 143

页数：6

共 8 条

[1]

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[2]

LIBOVE C, 1977, STABILITY STRUCTURES, P453

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PEREL, D ;

LIBOVE, C .

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1978, 45 (03) :579-582

[4]

SANBONGI S, 1983, TR759 NAT AER LAB RE

[5]

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[6]

TIMOSHENKO S, 1961, THEORY ELASTIC STABI, P379

[7] BUCKLING OF SINUSOIDALLY CORRUGATED PLATES UNDER AXIAL-COMPRESSION [J].

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AIAA JOURNAL, 1983, 21 (08) :1211-1213

[8]

1971, HDB STRUCTURAL STABI

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