| contributor author | G. Medic | |
| contributor author | P. A. Durbin | |
| date accessioned | 2017-05-09T00:08:58Z | |
| date available | 2017-05-09T00:08:58Z | |
| date copyright | April, 2002 | |
| date issued | 2002 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28695#193_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/127633 | |
| description abstract | Computations of flow and heat transfer for a film-cooled high pressure gas turbine rotor blade geometry are presented with an assessment of several turbulence models. Details of flow and temperature field predictions in the vicinity of cooling holes are examined. It is demonstrated that good predictions can be obtained when spurious turbulence energy production by the turbulence model is prevented. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Toward Improved Film Cooling Prediction | |
| type | Journal Paper | |
| journal volume | 124 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.1458021 | |
| journal fristpage | 193 | |
| journal lastpage | 199 | |
| identifier eissn | 1528-8900 | |
| keywords | Cooling | |
| keywords | Turbulence | |
| keywords | Flow (Dynamics) | |
| keywords | Heat transfer | |
| keywords | Suction AND Blades | |
| tree | Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 002 | |
| contenttype | Fulltext | |
