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    Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002::page 337
    Author:
    K. Funazaki
    DOI: 10.1115/1.2836644
    Publisher: 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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      Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion

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    https://yetl.yabesh.ir/yetl1/handle/yetl/117870
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    contributor authorK. Funazaki
    date accessioned2017-05-08T23:51:59Z
    date available2017-05-08T23:51:59Z
    date copyrightApril, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28651#337_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117870
    description abstractAs 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.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUnsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part II—Measurements of Unsteady Boundary Layers and Discussion
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2836644
    journal fristpage337
    journal lastpage344
    identifier eissn1528-8900
    keywordsMeasurement
    keywordsWakes
    keywordsBoundary layers
    keywordsFlat plates
    keywordsModeling
    keywordsTurbulence AND Wire
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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