Local Mass and Heat Transfer on a Turbine Blade Tip

Local Mass and Heat Transfer on a Turbine Blade Tip

Local mass and heat transfer measurements on a simulated high-pressure turbine blade-tip surface are conducted in a linear cascade with a nonmoving tip endwall, using a naphthalene sublimation technique. The effects of tip clearance (0.86–6.90% of chord) are investigated at various exit Reynolds num...

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Bibliographic Details
Main Authors: P. Jin, R. J. Goldstein
Format: Article
Language:English
Published: Hindawi Limited 2003-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/S1023621X03000083
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spelling doaj-2a39d804760b4294b26a48d336b710b62020-11-25T00:11:37ZengHindawi LimitedInternational Journal of Rotating Machinery1023-621X2003-01-0192819510.1155/S1023621X03000083Local Mass and Heat Transfer on a Turbine Blade TipP. Jin0R. J. Goldstein1Heat Transfer Laboratory, Department of Mechanical Engineering, University of Minnesota, Minneapolis, Minnesota, USAHeat Transfer Laboratory, Department of Mechanical Engineering, University of Minnesota, Minneapolis, Minnesota, USALocal mass and heat transfer measurements on a simulated high-pressure turbine blade-tip surface are conducted in a linear cascade with a nonmoving tip endwall, using a naphthalene sublimation technique. The effects of tip clearance (0.86–6.90% of chord) are investigated at various exit Reynolds numbers (4–7 × 105) and turbulence intensities (0.2 and 12.0%).http://dx.doi.org/10.1155/S1023621X03000083
collection DOAJ
language English
format Article
sources DOAJ
author P. Jin
R. J. Goldstein
spellingShingle P. Jin
R. J. Goldstein
Local Mass and Heat Transfer on a Turbine Blade Tip
International Journal of Rotating Machinery
author_facet P. Jin
R. J. Goldstein
author_sort P. Jin
title Local Mass and Heat Transfer on a Turbine Blade Tip
title_short Local Mass and Heat Transfer on a Turbine Blade Tip
title_full Local Mass and Heat Transfer on a Turbine Blade Tip
title_fullStr Local Mass and Heat Transfer on a Turbine Blade Tip
title_full_unstemmed Local Mass and Heat Transfer on a Turbine Blade Tip
title_sort local mass and heat transfer on a turbine blade tip
publisher Hindawi Limited
series International Journal of Rotating Machinery
issn 1023-621X
publishDate 2003-01-01
description Local mass and heat transfer measurements on a simulated high-pressure turbine blade-tip surface are conducted in a linear cascade with a nonmoving tip endwall, using a naphthalene sublimation technique. The effects of tip clearance (0.86–6.90% of chord) are investigated at various exit Reynolds numbers (4–7 × 105) and turbulence intensities (0.2 and 12.0%).
url http://dx.doi.org/10.1155/S1023621X03000083
work_keys_str_mv AT pjin localmassandheattransferonaturbinebladetip
AT rjgoldstein localmassandheattransferonaturbinebladetip
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