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    Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part I—Measurement of Wake-Affected Heat Transfer and Wake-Induced Transition Model

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002::page 327
    Author:
    K. Funazaki
    DOI: 10.1115/1.2836643
    Publisher: 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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      Unsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part I—Measurement of Wake-Affected Heat Transfer and Wake-Induced Transition Model

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    http://yetl.yabesh.ir/yetl1/handle/yetl/117869
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    contributor authorK. Funazaki
    date accessioned2017-05-08T23:51:58Z
    date available2017-05-08T23:51:58Z
    date copyrightApril, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28651#327_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117869
    description abstractMeasurements 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.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUnsteady Boundary Layers on a Flat Plate Disturbed by Periodic Wakes: Part I—Measurement of Wake-Affected Heat Transfer and Wake-Induced Transition Model
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2836643
    journal fristpage327
    journal lastpage336
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsWakes
    keywordsBoundary layers
    keywordsFlat plates
    keywordsTurbulence
    keywordsGenerators
    keywordsRotating Disks
    keywordsCircular cylinders AND Measurement
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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