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Thesis

Combustor and turbine aerothermal interactions in gas turbines with can combustors

Abstract:

As the research into the improvement of gas turbine performance progresses, the combustor- turbine interface becomes of increasing importance. In new engine designs components come closer together and the study of the combustor and turbine interactions can prove to be valuable for the improvement of the aerothermal performance of the vane.

This thesis presents an experimental and numerical investigation of the aerodynamic and heat transfer aspect of the interactions between the comb...

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Department:
University of Oxford

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

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