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.
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 ; 24 , 5 ; 138-141
1952-05-01
4 pages
Article (Journal)
Electronic Resource
English
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