Thesis
High pressure nozzle guide vane cooling system flow characteristics
- Abstract:
-
The continuous demand from the airlines for reduced jet engine fuel consumption results in increasingly challenging high pressure turbine nozzle guide vane (NGV) working conditions. The capability to reproduce representative boundary conditions in a rig at the combustor-turbine interaction plane is a key feature when testing NGVs in an engine-representative environment. A large scale linear cascade rig to investigate NGV leading edge cooling systems has been designed with particular at...
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Authors
Contributors
+ Ireland, P
- Institution:
- University of Oxford
- Division:
- MPLS
- Department:
- Engineering Science
- Role:
- Supervisor
- Type of award:
- DPhil
- Level of award:
- Doctoral
- Awarding institution:
- University of Oxford
- Language:
-
English
- UUID:
-
uuid:b8826eb5-f4ad-4fe8-8730-9134fd9fd183
- Deposit date:
-
2018-09-28
Terms of use
- Copyright holder:
- Cresci, I
- Copyright date:
- 2016
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