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The Relative Merits of Centrifugal and Axial Compressors for Aircraft Gas Turbines

Published online by Cambridge University Press:  28 July 2016

E. S. Moult  and
H. Pearson
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Extract

The suitability of a piece of mechanism for a given job depended both on the nature of the job and on the solution offered. In aviation they had to consider performance, time of development, cost in production and serviceability in its widest sense. It was proposed to review these different aspects as they applied to the compressors for aircraft gas turbines.

Type
Research Article
Information
The Aeronautical Journal , Volume 55 , Issue 483 , March 1951 , pp. 129 - 152
Copyright
Copyright © Royal Aeronautical Society 1951

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References

page 147 note * Reproduced from “ Design and Development of Centrifugal Compressors for Aircraft Gas Turbines,” L. J. Cheshire, Proceedings of the Institution of Mech. E., 1945, Volume 153.