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    Effect of Target Wall Curvature on Heat Transfer and Pressure Loss From Jet Array Impingement

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 005::page 51004
    Author:
    Harrington, John
    ,
    Hossain, Jahed
    ,
    Wang, Wenping
    ,
    Kapat, Jayanta
    ,
    Maurer, Michael
    ,
    Thorpe, Steven
    DOI: 10.1115/1.4035160
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments to investigate the effect of target wall curvature on heat transfer and pressure loss from jet array impingement are performed. A jet plate configuration is studied with constant hole diameters and spacings. The geometry of the jet plate has streamwise jet spacings of 5.79 jet diameters, spanwise jet spacings of 4.49 jet diameters, and a jet-to-target plate distance of 3 jet diameters. For the curved case, the radius of the target plate is r/D = 31.57. A flat target wall setup with identical geometric spacing is also tested for direct comparison. Jet spacings were chosen such that validation and comparison can be made with open literature. For all configurations, spent air is drawn out in a single direction, which is tangential to the target plate curvature. Average jet Reynolds numbers ranging from 55,000 to 125,000 are tested. A steady-state measurement technique utilizing temperature-sensitive paint (TSP) is used on the target surface to obtain Nusselt number distributions. Pressure taps placed on the sidewall of the channel are used to evaluate the flow distribution in the impingement channel. Alongside the experimental work, CFD was performed utilizing the v2 − f turbulence model to better understand the relationship between the flow field and the heat transfer on the target surface. The main target of the current study is to quantify the impact of target wall radius and the decay of heat transfer after the impingement section, and to check the open literature correlations. It was found that the target wall curvature did not cause any significant changes in either the flow distribution or the heat transfer level. Comparisons with established correlations show similar level but different trends in heat transfer, potentially caused by differences in L/D. CFD results were able to show agreement in streamwise pitch-averaged Nusselt number levels with experimental results for the curved target plate at higher Re numbers.
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      Effect of Target Wall Curvature on Heat Transfer and Pressure Loss From Jet Array Impingement

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    contributor authorHarrington, John
    contributor authorHossain, Jahed
    contributor authorWang, Wenping
    contributor authorKapat, Jayanta
    contributor authorMaurer, Michael
    contributor authorThorpe, Steven
    date accessioned2017-11-25T07:19:51Z
    date available2017-11-25T07:19:51Z
    date copyright2017/24/1
    date issued2017
    identifier issn0889-504X
    identifier otherturbo_139_05_051004.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236056
    description abstractExperiments to investigate the effect of target wall curvature on heat transfer and pressure loss from jet array impingement are performed. A jet plate configuration is studied with constant hole diameters and spacings. The geometry of the jet plate has streamwise jet spacings of 5.79 jet diameters, spanwise jet spacings of 4.49 jet diameters, and a jet-to-target plate distance of 3 jet diameters. For the curved case, the radius of the target plate is r/D = 31.57. A flat target wall setup with identical geometric spacing is also tested for direct comparison. Jet spacings were chosen such that validation and comparison can be made with open literature. For all configurations, spent air is drawn out in a single direction, which is tangential to the target plate curvature. Average jet Reynolds numbers ranging from 55,000 to 125,000 are tested. A steady-state measurement technique utilizing temperature-sensitive paint (TSP) is used on the target surface to obtain Nusselt number distributions. Pressure taps placed on the sidewall of the channel are used to evaluate the flow distribution in the impingement channel. Alongside the experimental work, CFD was performed utilizing the v2 − f turbulence model to better understand the relationship between the flow field and the heat transfer on the target surface. The main target of the current study is to quantify the impact of target wall radius and the decay of heat transfer after the impingement section, and to check the open literature correlations. It was found that the target wall curvature did not cause any significant changes in either the flow distribution or the heat transfer level. Comparisons with established correlations show similar level but different trends in heat transfer, potentially caused by differences in L/D. CFD results were able to show agreement in streamwise pitch-averaged Nusselt number levels with experimental results for the curved target plate at higher Re numbers.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Target Wall Curvature on Heat Transfer and Pressure Loss From Jet Array Impingement
    typeJournal Paper
    journal volume139
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4035160
    journal fristpage51004
    journal lastpage051004-13
    treeJournal of Turbomachinery:;2017:;volume( 139 ):;issue: 005
    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
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