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Heat transfer in the core compressor under ice crystal icing conditions

Abstract:

It has been recognised in recent years that high altitude atmospheric ice crystals pose a threat to aircraft engines. Instances of damage, surge and shutdown have been recorded at altitudes significantly greater than those associated with supercooled water icing. It is believed that solid ice particles can accrete inside the core compressor, although the exact mechanism by which this occurs remains poorly understood. Development of analytical and empirical models of the ice crystal icing phe...

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Publication status:
Published
Peer review status:
Peer reviewed

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Publisher copy:
10.1115/GT2017-63077

Authors


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Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
Oxford college:
St Catherine's College
Role:
Author
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Rolls-Royce Plc More from this funder
Publisher:
American Society of Mechanical Engineers Publisher's website
Journal:
Proceedings of the ASME Turbo Expo Journal website
Volume:
2D-2017: Turbomachinery
Article number:
GT2017-63077
Host title:
Proceedings of the ASME Turbo Expo: Turbomachinery Technical Conference and Exposition
Publication date:
2017-06-26
Acceptance date:
2017-01-23
DOI:
Source identifiers:
731019
ISBN:
9780791850817
Pubs id:
pubs:731019
UUID:
uuid:6d94db28-fa04-45b8-910e-d570a1ff07f6
Local pid:
pubs:731019
Deposit date:
2018-11-26

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