The Influence of Large-Scale High-Intensity Turbulence on Vane Heat TransferSource: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001::page 23Author:F. E. Ames
DOI: 10.1115/1.2841007Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental research program was undertaken to examine the influence of large-scale high-intensity turbulence on vane heat transfer. The experiment was conducted in a four-vane linear cascade at exit Reynolds numbers of 500,000 and 800,000 based on chord length. Heat transfer measurements were made for four inlet turbulence conditions including a low turbulence case (Tu ≅ 1 percent), a grid turbulence case (Tu ≅ 7.5 percent), and two levels of large-scale turbulence generated with a mock combustor at two upstream locations (Tu ≅ 12 percent and 8 percent). The heat transfer data demonstrated that the length scale, Lu, has a significant effect on stagnation region and pressure surface heat transfer.
keyword(s): Turbulence , Heat transfer , Measurement , Pressure , Reynolds number , Cascades (Fluid dynamics) , Combustion chambers AND Chords (Trusses) ,
|
Collections
Show full item record
| contributor author | F. E. Ames | |
| date accessioned | 2017-05-08T23:55:12Z | |
| date available | 2017-05-08T23:55:12Z | |
| date copyright | January, 1997 | |
| date issued | 1997 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28657#23_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/119654 | |
| description abstract | An experimental research program was undertaken to examine the influence of large-scale high-intensity turbulence on vane heat transfer. The experiment was conducted in a four-vane linear cascade at exit Reynolds numbers of 500,000 and 800,000 based on chord length. Heat transfer measurements were made for four inlet turbulence conditions including a low turbulence case (Tu ≅ 1 percent), a grid turbulence case (Tu ≅ 7.5 percent), and two levels of large-scale turbulence generated with a mock combustor at two upstream locations (Tu ≅ 12 percent and 8 percent). The heat transfer data demonstrated that the length scale, Lu, has a significant effect on stagnation region and pressure surface heat transfer. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Influence of Large-Scale High-Intensity Turbulence on Vane Heat Transfer | |
| type | Journal Paper | |
| journal volume | 119 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2841007 | |
| journal fristpage | 23 | |
| journal lastpage | 30 | |
| identifier eissn | 1528-8900 | |
| keywords | Turbulence | |
| keywords | Heat transfer | |
| keywords | Measurement | |
| keywords | Pressure | |
| keywords | Reynolds number | |
| keywords | Cascades (Fluid dynamics) | |
| keywords | Combustion chambers AND Chords (Trusses) | |
| tree | Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001 | |
| contenttype | Fulltext |