Thesis
Internal cooling for HP turbine blades
- Abstract:
-
Modern gas turbine engines run at extremely high temperatures which require the high pressure turbine blades to be extensively cooled in order to reach life requirements. This must be done using the minimum amount of coolant in order to reduce the negative impacts on the cycle efficiency. In the design process the cooling configuration and stress distribution must be carefully considered before verification of the design is conducted. Improvements to all three of these blade design areas a...
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Funding
Engineering and Physical Sciences Research Council
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European Union
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Rolls Royce
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Bibliographic Details
- Type of award:
- DPhil
- Level of award:
- Doctoral
- Awarding institution:
- University of Oxford
Item Description
- Language:
- English
- Keywords:
- Subjects:
- UUID:
-
uuid:832038c9-e934-413d-bbb5-336ab4775055
- Deposit date:
- 2018-02-14
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Terms of use
- Copyright holder:
- Pearce, R
- Copyright date:
- 2016
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