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    Effects of Jet To Target Plate Distance and Reynolds Number on Jet Array Impingement Heat Transfer

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 005::page 51013
    Author:
    Lee, Junsik
    ,
    Ren, Zhong
    ,
    Haegele, Jacob
    ,
    Potts, Geoffrey
    ,
    Sik Jin, Jae
    ,
    Ligrani, Phil
    ,
    Fox, Michael D.
    ,
    Moon, Hee
    DOI: 10.1115/1.4025228
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Data which illustrate the effects of jettotarget plate distance and Reynolds number on the heat transfer from an array of jets impinging on a flat plate are presented. Considered are Reynolds numbers Rej ranging from 8200 to 52,000 with isentropic jet Mach numbers of approximately 0.1 to 0.2. Jettotarget plate distances Z of 1.5D, 3.0D, 5.0D, and 8.0D are employed, where D is the impingement hole diameter. Streamwise and spanwise hole spacings are 8D. Local and spatiallyaveraged Nusselt numbers show strong dependence on the impingement jet Reynolds number for all situations examined. Experimental results also illustrate the dependence of local Nusselt numbers on normalized jettotarget plate distance, especially for smaller values of this quantity. The observed variations are partially due to accumulating crossflows produced as the jets advect downstream, as well as the interactions of the vortex structures, which initially form around the jets and then impact and interact as they advect away from stagnation points along the impingement target surface. The highest spatiallyaveraged Nusselt numbers are present for Z/D = 3.0 for Rej of 8200, 20,900, and 30,000. When Rej = 52,000, spatiallyaveraged Nusselt numbers increase as Z/D decreases, with the highest value present at Z/D = 1.5.
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      Effects of Jet To Target Plate Distance and Reynolds Number on Jet Array Impingement Heat Transfer

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    contributor authorLee, Junsik
    contributor authorRen, Zhong
    contributor authorHaegele, Jacob
    contributor authorPotts, Geoffrey
    contributor authorSik Jin, Jae
    contributor authorLigrani, Phil
    contributor authorFox, Michael D.
    contributor authorMoon, Hee
    date accessioned2017-05-09T01:13:35Z
    date available2017-05-09T01:13:35Z
    date issued2014
    identifier issn0889-504X
    identifier otherturbo_136_05_051013.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156595
    description abstractData which illustrate the effects of jettotarget plate distance and Reynolds number on the heat transfer from an array of jets impinging on a flat plate are presented. Considered are Reynolds numbers Rej ranging from 8200 to 52,000 with isentropic jet Mach numbers of approximately 0.1 to 0.2. Jettotarget plate distances Z of 1.5D, 3.0D, 5.0D, and 8.0D are employed, where D is the impingement hole diameter. Streamwise and spanwise hole spacings are 8D. Local and spatiallyaveraged Nusselt numbers show strong dependence on the impingement jet Reynolds number for all situations examined. Experimental results also illustrate the dependence of local Nusselt numbers on normalized jettotarget plate distance, especially for smaller values of this quantity. The observed variations are partially due to accumulating crossflows produced as the jets advect downstream, as well as the interactions of the vortex structures, which initially form around the jets and then impact and interact as they advect away from stagnation points along the impingement target surface. The highest spatiallyaveraged Nusselt numbers are present for Z/D = 3.0 for Rej of 8200, 20,900, and 30,000. When Rej = 52,000, spatiallyaveraged Nusselt numbers increase as Z/D decreases, with the highest value present at Z/D = 1.5.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Jet To Target Plate Distance and Reynolds Number on Jet Array Impingement Heat Transfer
    typeJournal Paper
    journal volume136
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4025228
    journal fristpage51013
    journal lastpage51013
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2014:;volume( 136 ):;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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