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    Separate Effects of Mach Number and Reynolds Number on Jet Array Impingement Heat Transfer

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002::page 269
    Author:
    Jongmyung Park
    ,
    Phil Ligrani
    ,
    Mike Fox
    ,
    Hee-Koo Moon
    ,
    Matt Goodro
    DOI: 10.1115/1.2437774
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Limited available data suggest a substantial impact of Mach number on the heat transfer from an array of jets impinging on a surface at fixed Reynolds number. Many jet array heat transfer correlations currently in use are based on tests in which the jet Reynolds number was varied by varying the jet Mach number. Hence, this data may be inaccurate for high Mach numbers. Results from the present study are new and innovative because they separate the effects of jet Reynolds number and jet Mach number for the purposes of validating and improving correlations that are currently in use. The present study provides new data on the separate effects of Reynolds number and Mach number for an array of impinging jets in the form of discharge coefficients, local and spatially averaged Nusselt numbers, and local and spatially averaged recovery factors. The data are unique because data are given for impingement jet Mach numbers as high as 0.60 and impingement jet Reynolds numbers as high as 60,000, and because the effects of Reynolds number and Mach number are separated by providing data at constant Reynolds number because the Mach number is varied, and data at constant Mach number because the Reynolds number is varied. As such, the present data are given for experimental conditions not previously examined, which are outside the range of applicability of current correlations.
    keyword(s): Flow (Dynamics) , Mach number , Temperature , Heat transfer , Reynolds number , Jets , Discharge coefficient , Pressure AND Measurement ,
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      Separate Effects of Mach Number and Reynolds Number on Jet Array Impingement Heat Transfer

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    contributor authorJongmyung Park
    contributor authorPhil Ligrani
    contributor authorMike Fox
    contributor authorHee-Koo Moon
    contributor authorMatt Goodro
    date accessioned2017-05-09T00:26:11Z
    date available2017-05-09T00:26:11Z
    date copyrightApril, 2007
    date issued2007
    identifier issn0889-504X
    identifier otherJOTUEI-28736#269_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137035
    description abstractLimited available data suggest a substantial impact of Mach number on the heat transfer from an array of jets impinging on a surface at fixed Reynolds number. Many jet array heat transfer correlations currently in use are based on tests in which the jet Reynolds number was varied by varying the jet Mach number. Hence, this data may be inaccurate for high Mach numbers. Results from the present study are new and innovative because they separate the effects of jet Reynolds number and jet Mach number for the purposes of validating and improving correlations that are currently in use. The present study provides new data on the separate effects of Reynolds number and Mach number for an array of impinging jets in the form of discharge coefficients, local and spatially averaged Nusselt numbers, and local and spatially averaged recovery factors. The data are unique because data are given for impingement jet Mach numbers as high as 0.60 and impingement jet Reynolds numbers as high as 60,000, and because the effects of Reynolds number and Mach number are separated by providing data at constant Reynolds number because the Mach number is varied, and data at constant Mach number because the Reynolds number is varied. As such, the present data are given for experimental conditions not previously examined, which are outside the range of applicability of current correlations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSeparate Effects of Mach Number and Reynolds Number on Jet Array Impingement Heat Transfer
    typeJournal Paper
    journal volume129
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2437774
    journal fristpage269
    journal lastpage280
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsMach number
    keywordsTemperature
    keywordsHeat transfer
    keywordsReynolds number
    keywordsJets
    keywordsDischarge coefficient
    keywordsPressure AND Measurement
    treeJournal of Turbomachinery:;2007:;volume( 129 ):;issue: 002
    contenttypeFulltext
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