The Influence of Pressure Ratio on Film Cooling Performance of a Turbine Blade

The relationship between the plenum to freestream total pressure ratio on film cooling performance is experimentally investigated. Measurements of both the heat transfer coefficient and the adiabatic effectiveness were made on the suction side of the center blade in a linear transonic cascade. Entr...

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Bibliographic Details
Main Author: Bubb, James Vernon
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/34023
http://scholar.lib.vt.edu/theses/available/etd-071599-164531/