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Pressure Ratios for Aero‐Engines: A Note on the Factors Limiting the Choice of Pressure Ratio

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 December 1953

48

Abstract

IT is usually supposed that the designer of a gas turbine engine has considerable freedom in choosing the pressures, temperatures and other features. Indeed this apparent flexibility has been claimed as an inherent advantage of the gas turbine, which enables it to be tailor‐made for any prescribed duty.

Citation

Stephenson, J.M. (1953), "Pressure Ratios for Aero‐Engines: A Note on the Factors Limiting the Choice of Pressure Ratio", Aircraft Engineering and Aerospace Technology, Vol. 25 No. 12, pp. 371-371. https://doi.org/10.1108/eb032365

Publisher

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MCB UP Ltd

Copyright © 1953, MCB UP Limited

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