Heat/mass transfer characteristics in the near-tip region on a turbine blade surface under combustor-level high inlet turbulence
- Authors
- Kwon, Hyun Goo; Lee, Sang Woo
- Issue Date
- Mar-2007
- Publisher
- KOREAN SOC MECHANICAL ENGINEERS
- Keywords
- gas turbine; turbine rotor blade; heat transfer; tip clearance gap; high inlet turbulence
- Citation
- JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, v.21, no.3, pp 486 - 494
- Pages
- 9
- Journal Title
- JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY
- Volume
- 21
- Number
- 3
- Start Page
- 486
- End Page
- 494
- URI
- https://scholarworks.bwise.kr/kumoh/handle/2020.sw.kumoh/21959
- DOI
- 10.1007/BF02916310
- ISSN
- 1738-494X
1976-3824
- Abstract
- Heat/mass transfer characteristics on the near-tip blade surface under combustor-level high inlet turbulence have been investigated within a high-turning turbine rotor passage by using the naphthalene sublimation technique. The inlet turbulence intensity and length scale are 14.7% and 80 turn, respectively. The tip gap-to-chord ratio is changed to be h/c = 0.74, 1.47, and 2.94 percents. Increasing h/c results not only in higher heat/mass transfer in the pressure-side tip region but also in more convective transport on the pressure surface even far away from the tip edge. Severe heat/mass transfer is always observed in the suction-side tip-leakage flow region which can be divided into two distinct high transport regions. There is a local maximum of heat/mass transfer along the trailing-edge centerline. This arises from the interaction of a tip-leakage vortex with a trailing-edge vortex shedding. Comparisons of the present data for h/c = 2.94 percents with the previous low turbulence one show that there is a large discrepancy of heat/mass transfer in the pressure-side near-tip area, which diminishes with departing from the tip edge. The suction-side heat/mass transfer in the tip-leakage flow region is less influenced by the high inlet turbulence than that at the mid-span. The leading-edge heat/mass transfer under the high inlet turbulence is always higher than that in the low turbulence case, while there is no big difference in the trailing-edge heat/mass transfer between the two cases.
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Collections - Department of Mechanical Engineering > 1. Journal Articles
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