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    Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001::page 54
    Author:
    K. Rued
    ,
    S. Wittig
    DOI: 10.1115/1.3239697
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer and boundary layer measurements were derived from flows over a cooled flat plate with various free-stream turbulence intensities (Tu = 1.6–11 percent), favorable pressure gradients (k = νe /ue 2 •due /dx = 0÷6•10−6 ) and cooling intensities (Tw /Te = 1.0–0.53). Special interest is directed towards the effects of the dominant parameters, including the influence on laminar to turbulent boundary layer transition. It is shown, that free-stream turbulence and pressure gradients are of primary importance. The increase of heat transfer due to wall cooling can be explained primarily by property variations as transition, and the influence of free-stream parameters are not affected.
    keyword(s): Turbulence , Boundary layers , Heat transfer , Pressure gradient , Cooling , Measurement , Flow (Dynamics) , Boundary layer turbulence AND Flat plates ,
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      Free-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/99869
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorK. Rued
    contributor authorS. Wittig
    date accessioned2017-05-08T23:20:14Z
    date available2017-05-08T23:20:14Z
    date copyrightJanuary, 1985
    date issued1985
    identifier issn1528-8919
    identifier otherJETPEZ-26614#54_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99869
    description abstractHeat transfer and boundary layer measurements were derived from flows over a cooled flat plate with various free-stream turbulence intensities (Tu = 1.6–11 percent), favorable pressure gradients (k = νe /ue 2 •due /dx = 0÷6•10−6 ) and cooling intensities (Tw /Te = 1.0–0.53). Special interest is directed towards the effects of the dominant parameters, including the influence on laminar to turbulent boundary layer transition. It is shown, that free-stream turbulence and pressure gradients are of primary importance. The increase of heat transfer due to wall cooling can be explained primarily by property variations as transition, and the influence of free-stream parameters are not affected.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFree-Stream Turbulence and Pressure Gradient Effects on Heat Transfer and Boundary Layer Development on Highly Cooled Surfaces
    typeJournal Paper
    journal volume107
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239697
    journal fristpage54
    journal lastpage59
    identifier eissn0742-4795
    keywordsTurbulence
    keywordsBoundary layers
    keywordsHeat transfer
    keywordsPressure gradient
    keywordsCooling
    keywordsMeasurement
    keywordsFlow (Dynamics)
    keywordsBoundary layer turbulence AND Flat plates
    treeJournal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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