Thesis
Turbine blade mid-chord internal cooling
- Abstract:
-
Modern gas turbine engines operate at temperatures well above the melting point of the metal components. This has driven manufactures to develop sophisticated cooling methods which minimise the use of coolant to maximise engine efficiency by enabling further increases in operating temperature. This thesis investigates the cooling performance of engine representative mid-chord internal cooling passages for turbine blades. The work forms part of a larger E.C. FP7 project ERICKA (Engine Repre...
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Authors
Contributors
+ Gilispie, D
- Division:
- MPLS
- Department:
- Engineering Science
- Role:
- Supervisor
+ McGilvray, M
- Division:
- MPLS
- Department:
- Engineering Science
- Role:
- Supervisor
+ Engineering and Physical Sciences Research Council
More from this funder
- Funding agency for:
- Ryley, J
- Grant:
- 09000077
- Publication date:
- 2014
- DOI:
- Type of award:
- DPhil
- Level of award:
- Doctoral
- Awarding institution:
- Oxford University, UK
- Language:
-
English
- Keywords:
- Subjects:
- UUID:
-
uuid:14469a51-517c-400c-b477-4fb432c8b648
- Local pid:
-
ora:9160
- Deposit date:
-
2014-10-22
- ARK identifier:
Terms of use
- Copyright holder:
- Joshua Ryley
- Copyright date:
- 2014
- Notes:
- This thesis is not currently available in ORA.
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