Mass Transfer over a Film-Cooled Turbine Blade
A naphthalene sublimation technique was employed to study the mass transfer distributions over a turbine blade surface with secondary flows ejected in the spanwise direction through three rows of equally-spaced injection holes located in the leading edge region. The mass transfer measurements were c...
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| Format: | Article |
| Language: | English |
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Wiley
1996-01-01
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| Series: | International Journal of Rotating Machinery |
| Subjects: | |
| Online Access: | http://dx.doi.org/10.1155/S1023621X96000103 |
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| _version_ | 1832553180187066368 |
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| author | Ping-Hei Chen Jr-Ming Miao |
| author_facet | Ping-Hei Chen Jr-Ming Miao |
| author_sort | Ping-Hei Chen |
| collection | DOAJ |
| description | A naphthalene sublimation technique was employed to study the mass transfer distributions over a turbine blade surface with secondary flows ejected in the spanwise direction through three rows of equally-spaced injection holes located in the leading
edge region. The mass transfer measurements were conducted in a range of blowing ratios from 0.6 to 1.2 at two different mainstream turbulence levels (0.4% and 6.0%) while keeping the exit Reynolds number, Re2, at a constant value of 397,000. |
| format | Article |
| id | doaj-art-3437f77c7e0b4ecea6791702483046a0 |
| institution | Kabale University |
| issn | 1023-621X |
| language | English |
| publishDate | 1996-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Rotating Machinery |
| spelling | doaj-art-3437f77c7e0b4ecea6791702483046a02025-02-03T05:55:18ZengWileyInternational Journal of Rotating Machinery1023-621X1996-01-012422123610.1155/S1023621X96000103Mass Transfer over a Film-Cooled Turbine BladePing-Hei Chen0Jr-Ming Miao1Department of Mechanical Engineering, National Taiwan University, Taipei 10764, TaiwanDepartment of Mechanical Engineering, National Taiwan University, Taipei 10764, TaiwanA naphthalene sublimation technique was employed to study the mass transfer distributions over a turbine blade surface with secondary flows ejected in the spanwise direction through three rows of equally-spaced injection holes located in the leading edge region. The mass transfer measurements were conducted in a range of blowing ratios from 0.6 to 1.2 at two different mainstream turbulence levels (0.4% and 6.0%) while keeping the exit Reynolds number, Re2, at a constant value of 397,000.http://dx.doi.org/10.1155/S1023621X96000103turbine bladefilm coolingturbulence levelmass transfer. |
| spellingShingle | Ping-Hei Chen Jr-Ming Miao Mass Transfer over a Film-Cooled Turbine Blade International Journal of Rotating Machinery turbine blade film cooling turbulence level mass transfer. |
| title | Mass Transfer over a Film-Cooled Turbine Blade |
| title_full | Mass Transfer over a Film-Cooled Turbine Blade |
| title_fullStr | Mass Transfer over a Film-Cooled Turbine Blade |
| title_full_unstemmed | Mass Transfer over a Film-Cooled Turbine Blade |
| title_short | Mass Transfer over a Film-Cooled Turbine Blade |
| title_sort | mass transfer over a film cooled turbine blade |
| topic | turbine blade film cooling turbulence level mass transfer. |
| url | http://dx.doi.org/10.1155/S1023621X96000103 |
| work_keys_str_mv | AT pingheichen masstransferoverafilmcooledturbineblade AT jrmingmiao masstransferoverafilmcooledturbineblade |