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    Heat Transfer on a Flat Surface Under a Region of Turbulent Separation

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 001::page 57
    Author:
    R. B. Rivir
    ,
    J. P. Johnston
    ,
    J. K. Eaton
    DOI: 10.1115/1.2928278
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fluid dynamics and heat transfer measurements were performed for a separation bubble formed on a smooth, flat, constant-heat-flux plate. The separation was induced by an adverse pressure gradient created by deflection of the opposite wall of the wind tunnel. The heat transfer rate was found to decline monotonically approaching the separation point and reach a broad minimum approximately 60 percent below zero-pressure-gradient levels. The heat transfer rate increased rapidly approaching reattachment with a peak occurring slightly downstream of the mean reattachment point. The opposite wall shape was varied to reduce the applied adverse pressure gradient. The heat transfer results were similar as long as the pressure gradient was sufficient to cause full separation of the boundary layer.
    keyword(s): Heat transfer , Separation (Technology) , Turbulence , Pressure gradient , Shapes , Wind tunnels , Bubbles , Boundary layers , Deflection , Gradients , Measurement , Pressure , Fluid dynamics AND Heat ,
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      Heat Transfer on a Flat Surface Under a Region of Turbulent Separation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/114586
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    contributor authorR. B. Rivir
    contributor authorJ. P. Johnston
    contributor authorJ. K. Eaton
    date accessioned2017-05-08T23:45:54Z
    date available2017-05-08T23:45:54Z
    date copyrightJanuary, 1994
    date issued1994
    identifier issn0889-504X
    identifier otherJOTUEI-28634#57_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114586
    description abstractFluid dynamics and heat transfer measurements were performed for a separation bubble formed on a smooth, flat, constant-heat-flux plate. The separation was induced by an adverse pressure gradient created by deflection of the opposite wall of the wind tunnel. The heat transfer rate was found to decline monotonically approaching the separation point and reach a broad minimum approximately 60 percent below zero-pressure-gradient levels. The heat transfer rate increased rapidly approaching reattachment with a peak occurring slightly downstream of the mean reattachment point. The opposite wall shape was varied to reduce the applied adverse pressure gradient. The heat transfer results were similar as long as the pressure gradient was sufficient to cause full separation of the boundary layer.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer on a Flat Surface Under a Region of Turbulent Separation
    typeJournal Paper
    journal volume116
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2928278
    journal fristpage57
    journal lastpage62
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsSeparation (Technology)
    keywordsTurbulence
    keywordsPressure gradient
    keywordsShapes
    keywordsWind tunnels
    keywordsBubbles
    keywordsBoundary layers
    keywordsDeflection
    keywordsGradients
    keywordsMeasurement
    keywordsPressure
    keywordsFluid dynamics AND Heat
    treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 001
    contenttypeFulltext
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