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A comparison of experimental and computational heat transfer results for a leading edge impingement system

Abstract:

Leading edge impingement systems are increasingly being used for high pressure turbine blades in gas turbine engines, in regions where very high heat loads are encountered. The flow structure in such systems can be very complex and high resolution experimental data is required for engine-realistic systems to enable code validation and optimal design. This paper presents spatially resolved heat transfer distributions for an engine-realistic impingement system for multiple different hole geomet...

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Publication status:
Published
Peer review status:
Peer reviewed
Version:
Publisher's version

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Publisher copy:
10.3390/ijtpp3040023

Authors


More by this author
Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
More by this author
Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
Oxford college:
St Catherines College
Telisinghe, J More by this author
Rolls-Royce plc More from this funder
Publisher:
MDPI Publisher's website
Journal:
International Journal of Turbomachinery, Propulsion and Power Journal website
Volume:
3
Issue:
4
Pages:
23
Publication date:
2018-11-16
Acceptance date:
2018-11-12
DOI:
ISSN:
2504-186X
Pubs id:
pubs:946035
URN:
uri:a8add0ac-c8d5-41d7-baf3-a464de77a204
UUID:
uuid:a8add0ac-c8d5-41d7-baf3-a464de77a204
Local pid:
pubs:946035

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