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.
Air Cooling of Turbine Blades and Vanes
An account of the history and development of gas turbine cooling
Aircraft Engineering and Aerospace Technology ; 39 , 8 ; 4-14
01.08.1967
11 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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