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    Free-Stream Turbulence From a Circular Wall Jet on a Flat Plate Heat Transfer and Boundary Layer Flow

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 001::page 78
    Author:
    R. MacMullin
    ,
    R. Rivir
    ,
    W. Elrod
    DOI: 10.1115/1.3262240
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of the longitudinal turbulence intensity parameter of free-stream turbulence (FST) on heat transfer were studied using the aggressive flow characteristics of a circular tangential wall jet over a constant heat flux surface. Profile measurements of velocity, temperature, integral length scale, and spectra were obtained at downstream locations (2 to 20 x /D ) and turbulence intensities (7 to 18 percent). The results indicated that the Stanton number (St) and friction factor (C f ) increased with increasing turbulence intensity. The Reynolds analogy factor (2St/C f ) increased up to turbulence intensities of 12 percent, then became constant, and decreased after 15 percent. This factor was also found to be dependent on the Reynolds number (Rex ) and plate configuration. The influence of length scale, as found by previous researchers, was inconclusive at the conditions tested.
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      Free-Stream Turbulence From a Circular Wall Jet on a Flat Plate Heat Transfer and Boundary Layer Flow

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    http://yetl.yabesh.ir/yetl1/handle/yetl/106199
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    contributor authorR. MacMullin
    contributor authorR. Rivir
    contributor authorW. Elrod
    date accessioned2017-05-08T23:31:23Z
    date available2017-05-08T23:31:23Z
    date copyrightJanuary, 1989
    date issued1989
    identifier issn0889-504X
    identifier otherJOTUEI-28594#78_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106199
    description abstractThe effects of the longitudinal turbulence intensity parameter of free-stream turbulence (FST) on heat transfer were studied using the aggressive flow characteristics of a circular tangential wall jet over a constant heat flux surface. Profile measurements of velocity, temperature, integral length scale, and spectra were obtained at downstream locations (2 to 20 x /D ) and turbulence intensities (7 to 18 percent). The results indicated that the Stanton number (St) and friction factor (C f ) increased with increasing turbulence intensity. The Reynolds analogy factor (2St/C f ) increased up to turbulence intensities of 12 percent, then became constant, and decreased after 15 percent. This factor was also found to be dependent on the Reynolds number (Rex ) and plate configuration. The influence of length scale, as found by previous researchers, was inconclusive at the conditions tested.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFree-Stream Turbulence From a Circular Wall Jet on a Flat Plate Heat Transfer and Boundary Layer Flow
    typeJournal Paper
    journal volume111
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262240
    journal fristpage78
    journal lastpage86
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1989:;volume( 111 ):;issue: 001
    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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