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    Heat Transfer Enhancement in Narrow Diverging Channels

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 004::page 41017
    Author:
    Lamont, Justin
    ,
    Ramesh, Sridharan
    ,
    Ekkad, Srinath V.
    ,
    Tolpadi, Anil
    ,
    Kaminski, Christopher
    ,
    Salamah, Samir
    DOI: 10.1115/1.4007740
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed heat transfer coefficient distributions have been obtained for narrow diverging channels with and without enhancement features. The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presented at a representative Reynolds number of 28,000. Pressure drop measurements for the overall channel are also presented to evaluate the heat transfer enhancement geometry with respect to the pumping power requirements. The test models were studied for wall heat transfer coefficient measurements using the transient liquid crystal technique. The model wall inner surfaces were sprayed with thermochromic liquid crystals and a transient test was used to obtain the local heat transfer coefficients from the measured color change. An analysis of the results shows that the choice of designs is limited by the available pressure drop, even if the design provides significantly higher heat transfer coefficients. Dimpled surfaces provide appreciably high heat transfer coefficients and a reasonable pressure drop, whereas ribbed ducts provide significantly higher heat transfer coefficients and a higher overall pressure drop.
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      Heat Transfer Enhancement in Narrow Diverging Channels

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    http://yetl.yabesh.ir/yetl1/handle/yetl/153472
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    • Journal of Turbomachinery

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    contributor authorLamont, Justin
    contributor authorRamesh, Sridharan
    contributor authorEkkad, Srinath V.
    contributor authorTolpadi, Anil
    contributor authorKaminski, Christopher
    contributor authorSalamah, Samir
    date accessioned2017-05-09T01:03:43Z
    date available2017-05-09T01:03:43Z
    date issued2013
    identifier issn0889-504X
    identifier otherturb_135_4_041017.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153472
    description abstractDetailed heat transfer coefficient distributions have been obtained for narrow diverging channels with and without enhancement features. The cooling configurations considered include rib turbulators and concavities (or dimples) on the main heat transfer surfaces. All of the measurements are presented at a representative Reynolds number of 28,000. Pressure drop measurements for the overall channel are also presented to evaluate the heat transfer enhancement geometry with respect to the pumping power requirements. The test models were studied for wall heat transfer coefficient measurements using the transient liquid crystal technique. The model wall inner surfaces were sprayed with thermochromic liquid crystals and a transient test was used to obtain the local heat transfer coefficients from the measured color change. An analysis of the results shows that the choice of designs is limited by the available pressure drop, even if the design provides significantly higher heat transfer coefficients. Dimpled surfaces provide appreciably high heat transfer coefficients and a reasonable pressure drop, whereas ribbed ducts provide significantly higher heat transfer coefficients and a higher overall pressure drop.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Enhancement in Narrow Diverging Channels
    typeJournal Paper
    journal volume135
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4007740
    journal fristpage41017
    journal lastpage41017
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2013:;volume( 135 ):;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
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