Air Cooling of Turbine Blades and Vanes: An account of the history and development of gas turbine cooling
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 August 1967
Abstract
THE demand of the aircraft designer has been, and presumably always will be, for his engines to operate better in three basic respects. To give more thrust, to have less weight, and to require less fuel.
Citation
Halls, G.A. (1967), "Air Cooling of Turbine Blades and Vanes: An account of the history and development of gas turbine cooling", Aircraft Engineering and Aerospace Technology, Vol. 39 No. 8, pp. 4-14. https://doi.org/10.1108/eb034284
Publisher
:MCB UP Ltd
Copyright © 1967, MCB UP Limited