Thermal Performance Evaluation in Gas Turbine Aero Engines Accessory Gearbox
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منابع مشابه
Performance Evaluation of Simple Aero Gas Turbine Cycle with Transpiration Cooling of Gas Turbine Blades
Aero gas turbine engines have been using mainly film cooling and convection cooling techniques. For operating at high gas temperature amongst different cooling options the transpiration cooling technique has emerged as the most promising technique to improve the gas turbine cycle performance by allowing higher turbine inlet temperatures. This paper investigates the advantages of transpiration c...
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ژورنال
عنوان ژورنال: International Journal of Turbomachinery, Propulsion and Power
سال: 2020
ISSN: 2504-186X
DOI: 10.3390/ijtpp5030021