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Effect of Aggressive Inlet Swirl on Heat Transfer and Aerodynamics in an Unshrouded Transonic HP Turbine

Abstract:

Swirling flows are now widely being used in modern gas turbine combustors to improve the combustion characteristics, flame stability, and reduce emissions. Residual swirl at the combustor exit will affect the performance of the downstream high-pressure (HP) turbine. In order to perform a detailed investigation of the effect of swirl on a full-scale HP turbine stage, a combustor swirl simulator has been designed and commissioned in the Oxford Turbine Research Facility (OTRF), previously locate...

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Publication status:
Published

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Publisher copy:
10.1115/1.4004876

Authors


Qureshi, I More by this author
Beretta, A More by this author
More by this author
Institution:
University of Oxford
Department:
Oxford
Journal:
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
Volume:
134
Issue:
6
Pages:
061023-061023
Publication date:
2012-11-05
DOI:
EISSN:
1528-8900
ISSN:
0889-504X
URN:
uuid:bc19bd99-a3ac-40e1-bff5-c117314faf0b
Source identifiers:
351474
Local pid:
pubs:351474

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