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Understanding thermal unsteadiness in engine representative flows and improved methodologies for derived heat transfer calculations using thin-film gauges

Abstract:
The Oxford Turbine Research Facility (OTRF) is a high-speed rotating transient test facility, that allows unsteady aerodynamic and heat transfer measurements at engine representative conditions. In addition, a variety of inlet temperature profiles can be simulated in the rig including radial distortion, circumferential distortion, and swirl. However, the engine representative flows cause complications in the processing of heat transfer data. The unsteadiness in temperature data was found to significantly rise as temperature distortions were introduced in the NGV inlet profile, to model a lean burn combustor exit. Using the NGV inlet temperature profile survey data, the thermal unsteadiness has been quantified and compared with a Uniform inlet. The experiments with a radially varying NGV inlet temperature profile showed up to nine times higher thermal unsteadiness, compared to the Uniform inlet. The second part of the paper is a continuation of the work presented in a previous paper by Singh et al. [1] and describes improved methodologies for derived heat transfer calculations using thinfilm gauges. In addition, the uncertainty associated with the derived heat transfer parameters, such as the heat transfer coefficient and adiabatic wall temperature has been quantified. The refined processing techniques have been demonstrated on casing heat transfer measurements, acquired in the OTRF with two inlet temperature profiles.
Publication status:
Published
Peer review status:
Peer reviewed

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Publisher copy:
10.1115/gt2023-101625

Authors

More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
ORCID:
0000-0003-0265-9207
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Oxford college:
Exeter College
Role:
Author
ORCID:
0000-0003-4812-6182
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
Department:
Engineering Science
Oxford college:
St Anne's College
Role:
Author


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Funder identifier:
https://ror.org/04h08p482


Publisher:
ASME International
Host title:
Proceedings of ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition (GT2023)
Article number:
GT2023-101625
Series:
Turbo Expo Proceedings
Series number:
13B
Publication date:
2023-09-28
Acceptance date:
2023-02-03
Event title:
ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition (GT2023)
Event location:
Boston, Massachusetts, USA
Event website:
https://event.asme.org/Turbo-Expo-(1)
Event start date:
2023-06-26
Event end date:
2023-06-30
DOI:
ISBN:
9780791887097


Language:
English
Pubs id:
1573845
UUID:
uuid_47144bbb-1576-45a1-8ccb-d64eb8abeaa1
Local pid:
pubs:1573845
Deposit date:
2026-01-06
ARK identifier:

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