| contributor author | Scot K. Waye | |
| contributor author | David G. Bogard | |
| 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#202_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/137028 | |
| description abstract | Film cooling adiabatic effectiveness for axial and compound angle holes on the suction side of a simulated turbine vane was investigated to determine the relative performance of these configurations. The effect of the surface curvature was also evaluated by comparing to previous curvature studies and flat plate film cooling results. Experiments were conducted for varying coolant density ratio, mainstream turbulence levels, and hole spacing. Results from these measurements showed that for mild curvature, 2r∕d≈160, flat plate results are sufficient to predict the cooling effectiveness. Furthermore, the compound angle injection improves adiabatic effectiveness for higher blowing ratios, similar to previous studies using flat plate facilities. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | High-Resolution Film Cooling Effectiveness Comparison of Axial and Compound Angle Holes on the Suction Side of a Turbine Vane | |
| type | Journal Paper | |
| journal volume | 129 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2448016 | |
| journal fristpage | 202 | |
| journal lastpage | 211 | |
| identifier eissn | 1528-8900 | |
| keywords | Cooling | |
| keywords | Turbulence | |
| keywords | Suction | |
| keywords | Coolants | |
| keywords | Turbines | |
| keywords | Flat plates | |
| keywords | Density AND Resolution (Optics) | |
| tree | Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002 | |
| contenttype | Fulltext | |
