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Research Papers

Turbine Cooling

[+] Author and Article Information
Jack B. Esgar

Structures Branch, Lewis Flight Propulsion Laboratory, National Advisory Committee for Aeronautics, Cleveland, Ohio

J. Eng. Power 81(3), 226-233 (Jul 01, 1959) (8 pages) doi:10.1115/1.4008052 History: Received June 03, 1958; Published July 01, 1959; Online February 20, 2019

Abstract

Turbine cooling, originally developed because of a shortage of heat-resistant alloys, is of interest for certain applications to permit operation of gas-turbine engines above uncooled temperatures. Specific power output would be increased, and in some cases specific fuel consumption decreased, depending on the engine type. Progress is reported on developments since 1952.

Copyright © 1959 by ASME
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