Effect of Unheated Starting Lengths on Film Cooling ExperimentsSource: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003::page 579DOI: 10.1115/1.2184355Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The effect of an unheated starting length upstream of a row of film cooling holes was studied experimentally to determine its effect on heat transfer coefficients downstream of the holes. Cases with a single row of cylindrical film cooling holes inclined at 35deg to the surface of a flat plate were considered at blowing ratios of 0.25, 0.5, 1.0, and 1.5. For each case, experiments were conducted to determine the film-cooling effectiveness and the Stanton number distributions in cases with the surface upstream of the holes heated and unheated. Measurements were made using an infrared camera, thermocouples, and hot and cold-wire anemometry. Ratios were computed of the Stanton number with film cooling (Stf) to corresponding Stanton numbers in cases without film cooling (Sto), but the same surface heating conditions. Contours of these ratios were qualitatively the same regardless of the upstream heating conditions, but the ratios were larger for the cases with a heating starting length. Differences were most pronounced just downstream of the holes and for the lower blowing rate cases. Even 12 diameters downstream of the holes, the Stanton number ratios were 10–15% higher with a heated starting length. At higher blowing rates the differences between the heated and unheated starting length cases were not significant. The differences in Stanton number distributions are related to jet flow structures, which vary with blowing rate.
keyword(s): Cooling AND Jets ,
|
Collections
Show full item record
| contributor author | Sarah M. Coulthard | |
| contributor author | Ralph J. Volino | |
| contributor author | Karen A. Flack | |
| date accessioned | 2017-05-09T00:21:57Z | |
| date available | 2017-05-09T00:21:57Z | |
| date copyright | July, 2006 | |
| date issued | 2006 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28730#579_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/134837 | |
| description abstract | The effect of an unheated starting length upstream of a row of film cooling holes was studied experimentally to determine its effect on heat transfer coefficients downstream of the holes. Cases with a single row of cylindrical film cooling holes inclined at 35deg to the surface of a flat plate were considered at blowing ratios of 0.25, 0.5, 1.0, and 1.5. For each case, experiments were conducted to determine the film-cooling effectiveness and the Stanton number distributions in cases with the surface upstream of the holes heated and unheated. Measurements were made using an infrared camera, thermocouples, and hot and cold-wire anemometry. Ratios were computed of the Stanton number with film cooling (Stf) to corresponding Stanton numbers in cases without film cooling (Sto), but the same surface heating conditions. Contours of these ratios were qualitatively the same regardless of the upstream heating conditions, but the ratios were larger for the cases with a heating starting length. Differences were most pronounced just downstream of the holes and for the lower blowing rate cases. Even 12 diameters downstream of the holes, the Stanton number ratios were 10–15% higher with a heated starting length. At higher blowing rates the differences between the heated and unheated starting length cases were not significant. The differences in Stanton number distributions are related to jet flow structures, which vary with blowing rate. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of Unheated Starting Lengths on Film Cooling Experiments | |
| type | Journal Paper | |
| journal volume | 128 | |
| journal issue | 3 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2184355 | |
| journal fristpage | 579 | |
| journal lastpage | 588 | |
| identifier eissn | 1528-8900 | |
| keywords | Cooling AND Jets | |
| tree | Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 003 | |
| contenttype | Fulltext |