Hostname: page-component-f554764f5-fr72s Total loading time: 0 Render date: 2025-04-08T17:46:04.985Z Has data issue: false hasContentIssue false
  • English
  • Français

Some Identities on Structural Flexibility after Buckling

Published online by Cambridge University Press:  07 June 2016

E. H. Mansfield
E. H. Mansfield*
Affiliation:
Royal Aircraft Establishment
Get access

Summary

This paper gives some identities concerning the flexibility of certain elastic structures, including flat plates, at the onset of buckling and subsequently. The identities have a useful application in determining the flexibility and the rate of change of flexibility with load for structures in which the mode in the buckled state changes continuously with load.

Type
Research Article
Information
Aeronautical Quarterly , Volume 9 , Issue 3 , August 1958 , pp. 300 - 304
Copyright
Copyright © Royal Aeronautical Society. 1958

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.)

Article purchase

Temporarily unavailable

References

1. Mansfield, E. H. On the Post-Buckling Behaviour of Stiffened Plane Sheet under Shear. R. & M. 3073, July 1958.Google Scholar
2. Williams, D. The Use of the Principle of Minimum Potential Energy in Problems of Static Equilibrium. R. & M. 1827. January 1938.Google Scholar
3. Love, A. E. H. The Mathematical Theory of Elasticity. Cambridge University Press, 1892. Reprinted by Dover Publications, New York, 1944.Google Scholar