Optimisation techniques for combustor wall cooling

In a drive to increase the thermal efficiency of modern gas turbine engines, the turbine entry temperature (TET) has been steadily increasing over time to the point where the hot gasses contained within the combustion chamber have temperatures well in excess of the melting point of the materials use...

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Bibliographic Details
Main Author: Jason Krawciw
Format: Default Thesis
Published: 2017
Subjects:
Other engineering not elsewhere classified
Film cooling
Effusion cooling
Pressure sensitive paint
Infrared thermography
CFD
Engineering not elsewhere classified
Online Access:https://hdl.handle.net/2134/25030
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https://hdl.handle.net/2134/25030

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