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    Effect of Reynolds Number, Hole Patterns, and Hole Inclination on Cooling Performance of an Impinging Jet Array—Part I: Convective Heat Transfer Results and Optimization

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 004::page 41002
    Author:
    Li, Weihong
    ,
    Li, Xueying
    ,
    Yang, Li
    ,
    Ren, Jing
    ,
    Jiang, Hongde
    ,
    Ligrani, Phillip
    DOI: 10.1115/1.4035045
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study comprehensively illustrates the effect of Reynolds number, hole spacing, jet-to-target distance, and hole inclination on the convective heat transfer performance of an impinging jet array. Spatially resolved target surface heat transfer coefficient distributions are measured using transient liquid crystal (TLC) measurement techniques, over a range of Reynolds numbers from 5000 to 25,000. Considered are effects of streamwise and spanwise jet-to-jet spacing (X/D, Y/D: 4–8) and jet-to-target plate distance (Z/D: 0.75–3). Overall, a test matrix of 36 different configurations is employed. In addition, the effect of hole inclination (θ: 0–40 deg) on the heat transfer coefficient is investigated. Optimal hole spacing arrangements and impingement distance are pointed out to maximize the area-averaged Nusselt number and minimize the amount of cooling air. Also included is a new correlation, based on that of Florschuetz et al., to predict row-averaged Nusselt number. The new correlation is capable to cover low Z/D ∼ 0.75 and presents better prediction of row-averaged Nusselt number, which proves to be an effective impingement design tool.
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      Effect of Reynolds Number, Hole Patterns, and Hole Inclination on Cooling Performance of an Impinging Jet Array—Part I: Convective Heat Transfer Results and Optimization

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4236044
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    contributor authorLi, Weihong
    contributor authorLi, Xueying
    contributor authorYang, Li
    contributor authorRen, Jing
    contributor authorJiang, Hongde
    contributor authorLigrani, Phillip
    date accessioned2017-11-25T07:19:50Z
    date available2017-11-25T07:19:50Z
    date copyright2017/4/1
    date issued2017
    identifier issn0889-504X
    identifier otherturbo_139_04_041002.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236044
    description abstractThis study comprehensively illustrates the effect of Reynolds number, hole spacing, jet-to-target distance, and hole inclination on the convective heat transfer performance of an impinging jet array. Spatially resolved target surface heat transfer coefficient distributions are measured using transient liquid crystal (TLC) measurement techniques, over a range of Reynolds numbers from 5000 to 25,000. Considered are effects of streamwise and spanwise jet-to-jet spacing (X/D, Y/D: 4–8) and jet-to-target plate distance (Z/D: 0.75–3). Overall, a test matrix of 36 different configurations is employed. In addition, the effect of hole inclination (θ: 0–40 deg) on the heat transfer coefficient is investigated. Optimal hole spacing arrangements and impingement distance are pointed out to maximize the area-averaged Nusselt number and minimize the amount of cooling air. Also included is a new correlation, based on that of Florschuetz et al., to predict row-averaged Nusselt number. The new correlation is capable to cover low Z/D ∼ 0.75 and presents better prediction of row-averaged Nusselt number, which proves to be an effective impingement design tool.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Reynolds Number, Hole Patterns, and Hole Inclination on Cooling Performance of an Impinging Jet Array—Part I: Convective Heat Transfer Results and Optimization
    typeJournal Paper
    journal volume139
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4035045
    journal fristpage41002
    journal lastpage041002-11
    treeJournal of Turbomachinery:;2017:;volume( 139 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian