Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions

Higher turbine inlet temperatures (TIT) are required for higher overall efficiency of gas turbine engines. Due to the constant push towards achieving high TIT, the heat load on high pressure turbine components has been increasing with time. Gas turbine airfoils are equipped with several sophisticate...

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Bibliographic Details
Main Author: Singh, Prashant
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2017
Subjects:
Online Access:http://hdl.handle.net/10919/78358