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
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
:MCB UP Ltd
Copyright © 1953, MCB UP Limited