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Asymmetrical Bending of Tapered Disks: The Solution of a Problem in Disk Bending Occurring in Connexion with Gas Turbines

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1950

20

Abstract

THE problem considered is that of a tapered bored disk, built‐in at the inner edge and twisted about a diameter, the outer edge remaining plane and circular. The outer edge may be regarded as:

Citation

Gradwell, C.F. (1950), "Asymmetrical Bending of Tapered Disks: The Solution of a Problem in Disk Bending Occurring in Connexion with Gas Turbines", Aircraft Engineering and Aerospace Technology, Vol. 22 No. 7, pp. 209-212. https://doi.org/10.1108/eb031926

Publisher

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MCB UP Ltd

Copyright © 1950, MCB UP Limited

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