Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and DiscussionSource: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002::page 337Author:K. Funazaki
DOI: 10.1115/1.2836644Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As the second part of the study, detailed hot-wire anemometry measurements of wake-affected boundary layers on the flat plate are made. These measurements are organized in order, first, to check the standpoint of the modeling of the wake-induced transition proposed in Part I, and second, to observe wake–boundary layer interaction in detail from a viewpoint of direct and indirect effect of the wake passage upon turbulent spot generation within the boundary layer, as described by Walker (1993). The validity of the presumed state of the wake-affected boundary layer in the distance–time domain, which constitutes the basis of the transition model, is confirmed to great extent. However, it is also found that the criterion for the onset of the wake-induced transition adopted in Part I should be reconsidered. Some successful attempts are therefore made to specify the transition onset.
keyword(s): Measurement , Wakes , Boundary layers , Flat plates , Modeling , Turbulence AND Wire ,
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| contributor author | K. Funazaki | |
| date accessioned | 2017-05-08T23:51:59Z | |
| date available | 2017-05-08T23:51:59Z | |
| date copyright | April, 1996 | |
| date issued | 1996 | |
| identifier issn | 0889-504X | |
| identifier other | JOTUEI-28651#337_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/117870 | |
| description abstract | As the second part of the study, detailed hot-wire anemometry measurements of wake-affected boundary layers on the flat plate are made. These measurements are organized in order, first, to check the standpoint of the modeling of the wake-induced transition proposed in Part I, and second, to observe wake–boundary layer interaction in detail from a viewpoint of direct and indirect effect of the wake passage upon turbulent spot generation within the boundary layer, as described by Walker (1993). The validity of the presumed state of the wake-affected boundary layer in the distance–time domain, which constitutes the basis of the transition model, is confirmed to great extent. However, it is also found that the criterion for the onset of the wake-induced transition adopted in Part I should be reconsidered. Some successful attempts are therefore made to specify the transition onset. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion | |
| type | Journal Paper | |
| journal volume | 118 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.2836644 | |
| journal fristpage | 337 | |
| journal lastpage | 344 | |
| identifier eissn | 1528-8900 | |
| keywords | Measurement | |
| keywords | Wakes | |
| keywords | Boundary layers | |
| keywords | Flat plates | |
| keywords | Modeling | |
| keywords | Turbulence AND Wire | |
| tree | Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002 | |
| contenttype | Fulltext |