Conference item
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
Actions
Access Document
- Publisher copy:
- 10.1115/gt2023-101625
Authors
- 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:
Terms of use
- Copyright holder:
- ASME
- Copyright date:
- 2023
- Rights statement:
- © 2023 by ASME
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