Hostname: page-component-78c5997874-4rdpn Total loading time: 0 Render date: 2024-11-05T10:42:56.571Z Has data issue: false hasContentIssue false
  • English
  • Français

The Buckling of a Rectangular Plate under Combined Biaxial Compression, Bending and Shear

Published online by Cambridge University Press:  07 June 2016

K. I. McKenzie
K. I. McKenzie*
Affiliation:
Aeronautical Research Laboratories, Melbourne
Get access

Summary

An analysis is presented of the buckling of a rectangular plate under combined biaxial compression, bending and shear. The sides of the plate to which bending is applied are simply-supported, the other two sides being supported by arbitrary edge members. The solution is expressed in a form suited to automatic computation and some sample results are given.

Type
Research Article
Information
Aeronautical Quarterly , Volume 15 , Issue 3 , August 1964 , pp. 239 - 246
Copyright
Copyright © Royal Aeronautical Society 1964 

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. Gerard, G. and Becker, H. Handbook of Structural Stability. Part I, Buckling of Flat Plates. N.A.C.A. T.N. 3781, 1954.Google Scholar
2. Wittrick, W. H. Buckling of an Infinite Simply-Supported Strip under Combined Longitudinal Compression, Transverse Compression, Bending and Shear. Aeronautical Research Laboratories Unpublished Report, No. S.M.234.Google Scholar
3. Kantorovich, L. V. and Krylov, V. I. Approximate Methods of Higher Analysis, Chapter IV. Noordhoff, The Hague, 1958.Google Scholar
4. Stein, M. and Neff, J. Buckling Stresses of Simply-Supported Rectangular Hat Plates in Shear. N.A.C.A. T.N. 1222, 1947.Google Scholar