| contributor author | A. J. Hanford | |
| contributor author | D. E. Wilson | |
| date accessioned | 2017-05-08T23:45:53Z | |
| date available | 2017-05-08T23:45:53Z | |
| date copyright | January, 1994 | |
| date issued | 1994 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28634#46_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/114585 | |
| description abstract | A phenomenological model is proposed that relates the effect of free-stream turbulence to the increase in stagnation point heat transfer. The model requires both turbulence intensity and energy spectra as inputs to the unsteady velocity at the edge of the boundary layer. The form of the edge velocity contains both a pulsation of the incoming flow and an oscillation of the streamlines. The incompressible unsteady and time-averaged boundary layer response is determined by solving the momentum and energy equations. The model allows for arbitrary two-dimensional geometry; however, results are given only for a circular cylinder. The time-averaged Nusselt number is determined theoretically and compared to existing experimental data. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Effect of a Turbulent Wake on the Stagnation Point: Part II—Heat Transfer Results | |
| type | Journal Paper | |
| journal volume | 116 | |
| journal issue | 1 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2928277 | |
| journal fristpage | 46 | |
| journal lastpage | 56 | |
| identifier eissn | 1528-8900 | |
| keywords | Wake turbulence | |
| keywords | Heat transfer | |
| keywords | Turbulence | |
| keywords | Boundary layers | |
| keywords | Circular cylinders | |
| keywords | Equations | |
| keywords | Geometry | |
| keywords | Oscillations | |
| keywords | Momentum | |
| keywords | Flow (Dynamics) AND Spectra (Spectroscopy) | |
| tree | Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001 | |
| contenttype | Fulltext | |