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Thermal Stresses in Disks of Constant Thickness

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 May 1957

75

Abstract

TURBINE disks are subject to stresses due to two causes; the inertia effects of rotation, and the radial variation of temperature across the disk. Elastic stresses due to each of these effects may be determined separately and superposed to obtain the resultant stress distribution.

Citation

Norbury, J.F. (1957), "Thermal Stresses in Disks of Constant Thickness", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 5, pp. 132-137. https://doi.org/10.1108/eb032823

Publisher

:

MCB UP Ltd

Copyright © 1957, MCB UP Limited

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