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Volume 22, Issue 7
1 July 1950
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 22, Issue 7
Review Article| July 01 1950

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

C.F. Gradwell, M.A.
C.F. Gradwell, M.A.
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Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1950
Aircraft Engineering (1950) 22 (7): 209–212.
https://doi.org/10.1108/eb031926

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:

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1950
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