Hostname: page-component-586b7cd67f-t7czq Total loading time: 0 Render date: 2024-11-24T17:47:42.645Z Has data issue: false hasContentIssue false
  • English
  • Français

Buckling of a Long Flat Panel with a Series of Equidistant Longitudinal Supports in Combined Longitudinal Compression and Shear

Published online by Cambridge University Press:  07 June 2016

W. H. Wittrick  and
P. L. V. Curzon
W. H. Wittrick
Affiliation:
Department of Civil Engineering, University of Birmingham
P. L. V. Curzon
Affiliation:
Department of Civil Engineering, University of Birmingham
Get access

Summary

The main purpose of this paper is to illustrate the use of the stability functions for long plates in combined compression and shear defined in a previous paper by the authors. The panel is supported on its two edges and on a series of N intermediate simple supports. Each of the two edges is either clamped or simply-supported and numerical results are given for each of the three possible combinations, with varying numbers of supports. In all cases it is found that a simple parabolic interaction formula between shear and compression is extremely accurate. Also simple approximate formulae are given for calculating the wavelength of the buckle and the lead of the nodal lines for any combination of compression, shear, edge conditions and number of supports.

Type
Research Article
Information
Aeronautical Quarterly , Volume 20 , Issue 1 , February 1969 , pp. 17 - 24
Copyright
Copyright © Royal Aeronautical Society. 1969

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Wittrick, W. H. and Curzon, P. L. V. Stability functions for the local buckling of thin flat-walled structures with the walls in combined shear and compression. Aeronautical Quarterly, Vol. XIX, p. 327, November 1968.Google Scholar
2. Wittrick, W. H. and Curzon, P. L. V. Nodal lines for long plates in combined shear and compression with sinusoidal edge rotations. Aeronautical Quarterly, Vol. XX, p. 1, February 1969. (In this issue.)Google Scholar

A correction has been issued for this article:

Errata