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Thesis

Unsteady phenomena and realistic geometry effects at the combustor-turbine interface of a large gas turbine

Abstract:

Gas turbines in combined cycle are the cleanest and most efficient form of large-scale thermal power generation, and their use is expected to increase in the future. The most arduous conditions within a turbine are faced by the first stage nozzle guide vanes (NGV). These are located immediately after the combustion chamber and face the highest thermal loads, as well a a complex flow field influenced by combustor conditions. For this thesis, experiments and computational methods are develop...

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Division:
MPLS
Department:
Engineering Science
Oxford college:
Worcester College
Role:
Author

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Role:
Supervisor
Type of award:
DPhil
Level of award:
Doctoral
Awarding institution:
University of Oxford

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