The Influence of Body Forces on the Stability of a Reinforced Rectangular Plate

IF 1.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE Aeronautical Journal Pub Date : 1955-06-01 DOI:10.1017/S0368393100118747
C. L. Amba Rao
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引用次数: 1

Abstract

Reinforced rectangular plates find frequent application in the field of aeroplane structures, ship structures and allied fields. The stability of a structural element, if its critical load in compression is rather low, is normally influenced by its own weight. Usually the ratio of the body forces of the stiffened plate to the critical load is a considerable amount and the influence of the body forces of the plate and the ribs on the critical load of the stiffened plate is discussed here. In this note (following Timoshenko), the extensional deformation of the middle surface during buckling is neglected, which greatly simplifies the analysis. Although it leads to an under-estimation of the critical load (of the order of 10 per cent at most) it is not likely to influence the general conclusions. Strain energy method of analysis is used.
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体力对加筋矩形板稳定性的影响
矩形加筋板在飞机结构、船舶结构及相关领域中有着广泛的应用。如果一个结构单元的临界压缩载荷很低,它的稳定性通常会受到其自重的影响。通常加筋板的体力与临界荷载之比是相当大的,这里讨论了板和肋的体力对加筋板临界荷载的影响。在本文(继Timoshenko之后)中,忽略了屈曲过程中中表面的拉伸变形,这大大简化了分析。虽然它导致对临界负荷的低估(最多为10%),但不太可能影响一般结论。采用应变能法进行分析。
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来源期刊
Aeronautical Journal
Aeronautical Journal 工程技术-工程:宇航
CiteScore
3.70
自引率
14.30%
发文量
86
审稿时长
6-12 weeks
期刊介绍: The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.
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