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Thesis

The development of a heat transfer measurement technique for application to rotating turbine blades

Abstract:

The successful design of a long-lived and efficient gas turbine engine requires a good knowledge of the thermal and aerodynamic performances of the components of the turbine. Of particular importance, is the heat transfer rate from the hot gases to the cooled turbine blades, since this limits the maximum turbine entry temperatures which can be obtained.

Much gas turbine research is concentrated on experimental modelling and measurements to assist in the development of improved theo...

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Institution:
University of Oxford
Division:
MPLS
Role:
Author

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Role:
Supervisor
Role:
Supervisor
Publication date:
1985
Type of award:
DPhil
Level of award:
Doctoral
Awarding institution:
University of Oxford
Source identifiers:
603840276
Language:
English
Subjects:
UUID:
uuid:36bbf5b6-8978-4aae-920e-06ce0b96194e
Local pid:
td:603840276
Deposit date:
2014-07-22

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