- Abstract:
-
This paper presents an experimental and numerical investigation of the aero-thermal performance of an uncooled winglet tip, under transonic conditions. Spatially-resolved heat transfer data, including winglet tip surface and near tip side walls, are obtained using the transient infrared thermography technique within the Oxford High Speed Linear Cascade test facility. CFD predictions are also conducted using the Rolls-Royce HYDRA suite. Most of the spatial heat transfer variations on the tip s...
Expand abstract - Publication status:
- Published
- Publisher copy:
- 10.1115/GT2010-22794
-
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- Volume:
- 4
- Issue:
- PARTS A AND B
- Pages:
- 357-367
- Publication date:
- 2010-01-01
- DOI:
- URN:
-
uuid:5acbc319-be2e-45b9-8863-bfa78d0111bc
- Source identifiers:
-
146763
- Local pid:
- pubs:146763
- ISBN:
- 978-0-7918-4399-4
- Copyright date:
- 2010
Conference
AERO-THERMAL PERFORMANCE OF A WINGLET AT ENGINE REPRESENTATIVE MACH AND REYNOLDS NUMBERS
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