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    Local Heat/Mass Transfer Measurement on the Effusion Plate in Impingement/Effusion Cooling Systems

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 003::page 601
    Author:
    Hyung Hee Cho
    ,
    Dong Ho Rhee
    DOI: 10.1115/1.1344904
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study is conducted to investigate the local heat/mass transfer characteristics for flow through perforated plates. A naphthalene sublimation method is employed to determine the local heat/mass transfer coefficients on the effusion plate. Two parallel perforated plates are arranged in two different configurations: staggered and shifted in one direction. The experiments are conducted for hole pitch-to-diameter ratios of 6.0, for gap distance between the perforated plates of 0.33 to 10 hole diameters, and for Reynolds numbers of 5000 to 12,000. The result shows that the high transfer region is formed at stagnation region and at the midline of the adjacent impinging jets due to secondary vortices and flow acceleration to the effusion hole. For flows through the perforated plates, the mass transfer rates on the surface of the effusion plate are about six to ten times higher than for effusion cooling alone (single perforated plate). In general, higher heat/mass transfer is obtained with smaller gap distance between two perforated plates.
    keyword(s): Flow (Dynamics) , Heat , Mass transfer , Jets , Vortices , Plates (structures) , Reynolds number , Cooling AND Cooling systems ,
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      Local Heat/Mass Transfer Measurement on the Effusion Plate in Impingement/Effusion Cooling Systems

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/126035
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    • Journal of Turbomachinery

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    contributor authorHyung Hee Cho
    contributor authorDong Ho Rhee
    date accessioned2017-05-09T00:06:16Z
    date available2017-05-09T00:06:16Z
    date copyrightJuly, 2001
    date issued2001
    identifier issn0889-504X
    identifier otherJOTUEI-28689#601_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126035
    description abstractThe present study is conducted to investigate the local heat/mass transfer characteristics for flow through perforated plates. A naphthalene sublimation method is employed to determine the local heat/mass transfer coefficients on the effusion plate. Two parallel perforated plates are arranged in two different configurations: staggered and shifted in one direction. The experiments are conducted for hole pitch-to-diameter ratios of 6.0, for gap distance between the perforated plates of 0.33 to 10 hole diameters, and for Reynolds numbers of 5000 to 12,000. The result shows that the high transfer region is formed at stagnation region and at the midline of the adjacent impinging jets due to secondary vortices and flow acceleration to the effusion hole. For flows through the perforated plates, the mass transfer rates on the surface of the effusion plate are about six to ten times higher than for effusion cooling alone (single perforated plate). In general, higher heat/mass transfer is obtained with smaller gap distance between two perforated plates.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLocal Heat/Mass Transfer Measurement on the Effusion Plate in Impingement/Effusion Cooling Systems
    typeJournal Paper
    journal volume123
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1344904
    journal fristpage601
    journal lastpage608
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsHeat
    keywordsMass transfer
    keywordsJets
    keywordsVortices
    keywordsPlates (structures)
    keywordsReynolds number
    keywordsCooling AND Cooling systems
    treeJournal of Turbomachinery:;2001:;volume( 123 ):;issue: 003
    contenttypeFulltext
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