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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Bibliographic Details
Main Authors: Duncan Walker, Bharat R. Koli, Peter Beecroft
Format: Default Conference proceeding
Published: 2017
Subjects:
Online Access:https://hdl.handle.net/2134/26863
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