Effect of Jet Pulsing on Film Cooling—Part I: Effectiveness and Flow-Field Temperature ResultsSource: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002::page 232DOI: 10.1115/1.2437231Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Pulsed film cooling was studied experimentally to determine its effect on film-cooling effectiveness. The film-cooling jets were pulsed using solenoid valves in the supply air line. Cases with a single row of cylindrical film-cooling holes inclined at 35 deg to the surface of a flat plate were considered at blowing ratios of 0.25, 0.5, 1.0, and 1.5 for a variety of pulsing frequencies and duty cycles. Temperature measurements were made using an infrared camera, thermocouples, and cold-wire anemometry. Hot-wire anemometry was used for velocity measurements. The local film-cooling effectiveness was calculated based on the measured temperatures, and the results were compared to baseline cases with continuous blowing. Phase-locked flow temperature fields were determined from cold-wire surveys. Pulsing at high frequencies helped to improve film-cooling effectiveness in some cases by reducing overall jet liftoff. At lower frequencies, pulsing tended to have the opposite effect. With the present geometry and a steady mainflow, pulsing did not provide an overall benefit. The highest overall effectiveness was achieved with continuous jets and a blowing ratio of 0.5. The present results may prove useful for understanding film-cooling behavior in engines, where mainflow unsteadiness causes film-cooling jet pulsation.
keyword(s): Flow (Dynamics) , Temperature , Cooling , Cycles , Frequency , Jets AND Valves ,
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| contributor author | Sarah M. Coulthard | |
| contributor author | Ralph J. Volino | |
| contributor author | Karen A. Flack | |
| date accessioned | 2017-05-09T00:26:10Z | |
| date available | 2017-05-09T00:26:10Z | |
| date copyright | April, 2007 | |
| date issued | 2007 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28736#232_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/137031 | |
| description abstract | Pulsed film cooling was studied experimentally to determine its effect on film-cooling effectiveness. The film-cooling jets were pulsed using solenoid valves in the supply air line. Cases with a single row of cylindrical film-cooling holes inclined at 35 deg to the surface of a flat plate were considered at blowing ratios of 0.25, 0.5, 1.0, and 1.5 for a variety of pulsing frequencies and duty cycles. Temperature measurements were made using an infrared camera, thermocouples, and cold-wire anemometry. Hot-wire anemometry was used for velocity measurements. The local film-cooling effectiveness was calculated based on the measured temperatures, and the results were compared to baseline cases with continuous blowing. Phase-locked flow temperature fields were determined from cold-wire surveys. Pulsing at high frequencies helped to improve film-cooling effectiveness in some cases by reducing overall jet liftoff. At lower frequencies, pulsing tended to have the opposite effect. With the present geometry and a steady mainflow, pulsing did not provide an overall benefit. The highest overall effectiveness was achieved with continuous jets and a blowing ratio of 0.5. The present results may prove useful for understanding film-cooling behavior in engines, where mainflow unsteadiness causes film-cooling jet pulsation. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of Jet Pulsing on Film Cooling—Part I: Effectiveness and Flow-Field Temperature Results | |
| type | Journal Paper | |
| journal volume | 129 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2437231 | |
| journal fristpage | 232 | |
| journal lastpage | 246 | |
| identifier eissn | 1528-8900 | |
| keywords | Flow (Dynamics) | |
| keywords | Temperature | |
| keywords | Cooling | |
| keywords | Cycles | |
| keywords | Frequency | |
| keywords | Jets AND Valves | |
| tree | Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002 | |
| contenttype | Fulltext |