Hostname: page-component-78c5997874-t5tsf Total loading time: 0 Render date: 2024-11-06T07:45:21.376Z Has data issue: false hasContentIssue false

Stresses in Shock Absorbers

Published online by Cambridge University Press:  28 July 2016

N. J. Durant*
Affiliation:
Rotol/British Messier Ltd.

Extract

This investigation is concerned with the stresses in a hollow circular cylinder of constant wall thickness, and closed by flexible plates, also of constant thickness. The cylinder is subjected to the combined action of an internal pressure and an axial force, both of which are statically applied. Although the particular case envisaged is that of a shock absorber, there are other engineering elements to which the analysis is applicable. Any closed circular cylinder of constant wall thickness subjected to an internal pressure is within the category. In a paper, Dr. D. M. A. Leggett investigated the case of an oleopneumatic shock absorber with rigid end plates, and what follows is an extension of his paper. As would be expected, the flexibility of the end plates causes a reduction in the flexural stress.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1956

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. Leggett, D. M. A. (1951). A note on the Stressing of Oleo-Pneumatic Shock Absorbers. The Aeronautical Quarterly, September 1951.Google Scholar
2. Timoshenko, S. (1936). Theory of Elastic Stability. Chap. IX, McGraw-Hill, 1936.Google Scholar
3. Love, A. E. H. (1927). The Mathematical Theory of Elasticity. Fourth Edition. £314 (a). Cambridge University Press, 1927.Google Scholar