Porous Ceramic Coating for Transpiration Cooling of Gas Turbine Blade
نویسندگان
چکیده
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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ii ACKNOWLEDGEMENTS Behind every success, there is inspiration or support of at least one person. In my case, it was a group of people including my mentor, my family, and my friends. First of all, I would like to thank Dr. Srinath Ekkad for his guidance, wisdom, and financial support. I do not think many advisors would go to the lab to help his student running an experiment. Whenever I had any ...
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ژورنال
عنوان ژورنال: Journal of Thermal Spray Technology
سال: 2013
ISSN: 1059-9630,1544-1016
DOI: 10.1007/s11666-013-9883-1