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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| Format: | Article |
| Language: | English |
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Wiley
2003-01-01
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| Series: | International Journal of Rotating Machinery |
| Online Access: | http://dx.doi.org/10.1155/S1023621X03000083 |
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| _version_ | 1832552486348521472 |
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| author | P. Jin R. J. Goldstein |
| author_facet | P. Jin R. J. Goldstein |
| author_sort | P. Jin |
| collection | DOAJ |
| 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%). |
| format | Article |
| id | doaj-art-2a39d804760b4294b26a48d336b710b6 |
| institution | Kabale University |
| issn | 1023-621X |
| language | English |
| publishDate | 2003-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Rotating Machinery |
| spelling | doaj-art-2a39d804760b4294b26a48d336b710b62025-02-03T05:58:27ZengWileyInternational 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 |
| spellingShingle | P. Jin R. J. Goldstein Local Mass and Heat Transfer on a Turbine Blade Tip International Journal of Rotating Machinery |
| title | 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_short | Local Mass and Heat Transfer on a Turbine Blade Tip |
| title_sort | local mass and heat transfer on a turbine blade tip |
| url | http://dx.doi.org/10.1155/S1023621X03000083 |
| work_keys_str_mv | AT pjin localmassandheattransferonaturbinebladetip AT rjgoldstein localmassandheattransferonaturbinebladetip |