| contributor author | R. E. Mayle | |
| contributor author | K. Dullenkopf | |
| date accessioned | 2017-05-08T23:34:08Z | |
| date available | 2017-05-08T23:34:08Z | |
| date copyright | April, 1990 | |
| date issued | 1990 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28601#188_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/107758 | |
| description abstract | A theory for transition from laminar to turbulent flow as the result of unsteady, periodic passing of turbulent wakes in the free stream is developed using Emmons’ transition model. Comparisons made to flat plate boundary layer measurements and airfoil heat transfer measurements confirm the theory. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Theory for Wake-Induced Transition | |
| type | Journal Paper | |
| journal volume | 112 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2927632 | |
| journal fristpage | 188 | |
| journal lastpage | 195 | |
| identifier eissn | 1528-8900 | |
| keywords | Heat transfer | |
| keywords | Measurement | |
| keywords | Turbulence | |
| keywords | Wakes | |
| keywords | Wake turbulence | |
| keywords | Boundary layers | |
| keywords | Flat plates AND Airfoils | |
| tree | Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002 | |
| contenttype | Fulltext | |
