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Turbine Stresses in Aero‐Engines: A paper read before the Society for Experimental Stress Analysis of Cambridge, Mass., U.S.A., on November 30, 1951

D.A. Drew, B.Sc, A.M.I.M.E., A.M.I.E.E. (Chief of Vibration Department, Kolls‐Royce Ltd.)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 May 1952

Abstract

AS a member of a Rolls‐Royce team of engineers I have been engaged upon the study of the cause of turbine blade failure on the test‐bed and in flight, but I should like to mention here that the views expressed in this paper are entirely my own and do not necessarily represent the views or the policy of Rolls‐Royce Limited. I have not hesitated to put forward some views, although the data are not available at this stage to provide rigid proofs that the views are correct. I hope that in doing this I may add to the interest of the discussion that will follow this paper.

Citation

Drew, D.A. (1952), "Turbine Stresses in Aero‐Engines: A paper read before the Society for Experimental Stress Analysis of Cambridge, Mass., U.S.A., on November 30, 1951", Aircraft Engineering and Aerospace Technology, Vol. 24 No. 5, pp. 138-141. https://doi.org/10.1108/eb032158

Publisher

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MCB UP Ltd

Copyright © 1952, MCB UP Limited