Preliminary investigation into the effects of a compressor rim purge flow on OGV/pre-diffuser and combustion system aerodynamics
As aero gas turbine designs strive for ever greater efficiencies the trend is for engine overall pressure ratios to rise. Although this provides greater thermal efficiency it means that cycle temperatures also increase. Traditionally turbines have been the focus of cooling schemes to enable them to...
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| Main Authors: | , , |
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| Format: | Default Conference proceeding |
| Published: |
2017
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| Subjects: | |
| Online Access: | https://hdl.handle.net/2134/26863 |
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