Hostname: page-component-cd9895bd7-8ctnn Total loading time: 0 Render date: 2024-12-25T05:31:25.010Z Has data issue: false hasContentIssue false

Stresses Due to Internal Hydrostatic Pressure in Thin-Walled Vessels of Stream-Line Form

Published online by Cambridge University Press:  28 July 2016

Extract

Tanks in the form of a surface of revolution are sometimes employed for carrying fuel. The purpose of this paper is to show how the stresses, due to the internal hydrostatic pressure, in a shell of this kind can be calculated when the equation of the generating curve is given. The acceleration imposed on the shell and its contents will be assumed to be at right angles to the axis of revolution, hence shear as well as direct stresses are set up. It will be supposed that no longitudinal bulkheads are fitted, and the shell will be taken as very thin so that the bending stresses in it are negligible. No attempt will be made to examine the stress distribution in the neighbourhood of a relatively rigid supporting ring; as shown by Timoshenko these ‘ end effects ’ are appreciable only in the immediate vicinity of the support. Nor will the stability be considered of those portions of the shell which are subjected to compression. Thus attention will be confined to what are commonly described as the membrane stresses.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1944

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 Timoshenko, Theory of Plates and Shells, McGraw-Hill, New York and London, 1940, chaps. XI and XII.

2 Loc. cit., p. 373.

3 Loc. cit., p. 365.

4 Cox, , J. of Roy. Aero. Soc., Vol. 33 (1929), p. 800 Google Scholar.