Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor

Cooling combustor chambers for gas turbine engines is challenging because of the complex flow fields inherent to this engine component. This complexity, in part, arises from the interaction of high momentum dilution jets required to mix the fuel with effusion film cooling jets that are intended to...

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Bibliographic Details
Main Author: Scrittore, Joseph
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/28171
http://scholar.lib.vt.edu/theses/available/etd-06302008-152132/