Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part I—Measurement of Wake-Affected Heat Transfer and Wake-Induced Transition ModelSource: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002::page 327Author:K. Funazaki
DOI: 10.1115/1.2836643Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Measurements of wake-affected heat transfer distributions on a flat plate are made by use of a wake generator that consists of a rotating disk and several types of circular cylinder. The main purpose of this study is to construct a wake-induced transition model in terms of an intermittency factor, considering the evolution of the wake-induced turbulent region, a so-called turbulent patch in a distance–time diagram. A comparison between the proposed transition model and the measured heat transfer data reveals that the transition model yields good agreement with the measured data of all test conditions in this study.
keyword(s): Heat transfer , Wakes , Boundary layers , Flat plates , Turbulence , Generators , Rotating Disks , Circular cylinders AND Measurement ,
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| contributor author | K. Funazaki | |
| date accessioned | 2017-05-08T23:51:58Z | |
| date available | 2017-05-08T23:51:58Z | |
| date copyright | April, 1996 | |
| date issued | 1996 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28651#327_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/117869 | |
| description abstract | Measurements of wake-affected heat transfer distributions on a flat plate are made by use of a wake generator that consists of a rotating disk and several types of circular cylinder. The main purpose of this study is to construct a wake-induced transition model in terms of an intermittency factor, considering the evolution of the wake-induced turbulent region, a so-called turbulent patch in a distance–time diagram. A comparison between the proposed transition model and the measured heat transfer data reveals that the transition model yields good agreement with the measured data of all test conditions in this study. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part I—Measurement of Wake-Affected Heat Transfer and Wake-Induced Transition Model | |
| type | Journal Paper | |
| journal volume | 118 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2836643 | |
| journal fristpage | 327 | |
| journal lastpage | 336 | |
| identifier eissn | 1528-8900 | |
| keywords | Heat transfer | |
| keywords | Wakes | |
| keywords | Boundary layers | |
| keywords | Flat plates | |
| keywords | Turbulence | |
| keywords | Generators | |
| keywords | Rotating Disks | |
| keywords | Circular cylinders AND Measurement | |
| tree | Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002 | |
| contenttype | Fulltext |