Hostname: page-component-77c89778f8-m8s7h Total loading time: 0 Render date: 2024-07-24T10:22:40.041Z Has data issue: false hasContentIssue false
  • English
  • Français

The Bending of Symmetrically Loaded Circular Plates of Variable Thickness under Uniform Compression

Published online by Cambridge University Press:  07 June 2016

R. S. Dhaliwal
R. S. Dhaliwal*
Affiliation:
University of Calgary, Alberta, Canada
Get access

Summary

The solution has been obtained for the problem of a uniformly compressed and symmetrically loaded circular ring plate of linearly varying thickness. Four particular cases have been discussed and numerical values of the maximum deflection have been obtained for various sizes of the hole of the ring.

Type
Research Article
Information
Aeronautical Quarterly , Volume 19 , Issue 1 , February 1968 , pp. 59 - 70
Copyright
Copyright © Royal Aeronautical Society. 1968

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. Holzer, H. Zeitschrift für Turbinenwesen, Vol. 15, p. 21, 1918.Google Scholar
2. Pichler, O. Die Biegung kreissymmetrischer Platten von veränderlicher Dicke (Dissertation, Stuttgart), Berlin, 1928.Google Scholar
3. Olsson, R. G. Biegung dreisförmiger Platten von radial veränderlicher Steiflgkeit. Ingenieur-Archiv, Vol. 8, 81, 1937.Google Scholar
4. Conway, H. D. The bending of symmetrically loaded circular plates of variable thickness. Journal of Applied Mechanics, Vol. 15, p. 1, 1948.Google Scholar
5. Conway, H. D. Axially symmetrical plates with linearly varying thickness. Journal of Applied Mechanics, Vol. 18, p. 140, 1951.CrossRefGoogle Scholar
6. Timoshenko, S. Theory of Plates and Shells. McGraw-Hill, New York, 1940.Google Scholar