Hostname: page-component-586b7cd67f-dsjbd Total loading time: 0 Render date: 2024-11-24T18:40:15.902Z Has data issue: false hasContentIssue false

Discontinuities in Bent Plates

Published online by Cambridge University Press:  07 June 2016

R. G. Redwood*
Affiliation:
Department of Civil Engineering and Applied Mechanics, McGill University
Get access

Summary

A method of deriving the finite-difference equations to be applied at or near flexural discontinuities in plates subjected to bending is suggested. Such equations are presented for the case when a plate consists of two regions of different flexural rigidities, the boundary between the regions being formed by straight lines meeting at right angles.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1965

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. Wood, R. H. Plastic and Elastic Design of Slabs and Plates, Chap. VIII. Thames and Hudson, London, 1961.Google Scholar
2. Allen, D. N. De G. and Severn, R. T. The Stresses in Foundation Rafts. II. Proceedings of the Institution of Civil Engineers, Vol. 20, p. 293, October 1961.CrossRefGoogle Scholar
3. Livesley, R. K. and Birchall, P. C. Analysis of a Loaded Cantilever Plate by Finite Difference Methods. R.A.E. Tech. Note, M.S. 26, June 1956.Google Scholar
4. Redwood, R. G. The Bending of a Plate Loaded Through a Rigid Rectangular Inclusion. The International Journal of Mechanical Sciences, Vol. 7, p. 421, June 1965.CrossRefGoogle Scholar
5. Salvadori, M. G. Stresses at a Re-Entrant Corner of a Plate. Proceedings of the American Society of Civil Engineers, ST Div., Vol. 87, p. 91, October 1961.Google Scholar
6. Williams, D. A General Method (Depending on the Aid of a Digital Computer) for Deriving the Structural Influence Coefficients of Aeroplane Wings. A.R.C. R. & M. 3048, 1959.Google Scholar