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    Impingement Heat Transfer Within Arrays of Circular Jets: Part II—Effects of Crossflow in the Presence of Roughness Elements

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004::page 594
    Author:
    T. A. Trabold
    ,
    N. T. Obot
    DOI: 10.1115/1.3262153
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was carried out to determine the effects of jet-induced crossflow on impingement heat transfer from rough surfaces. The jets impinged on surfaces having repeated square ribs, with transverse flow of the spent air. Two crossflow schemes were tested: discharge of the spent air through two opposite sides (intermediate crossflow) and through one side (complete or maximum crossflow) of the rectangular impingement surface. The rib height was fixed at 0.813 mm, while the pitch-to-height ratio (p /e) was varied between 6 and 10. The study covered standoff spacing and jet Reynolds number in the range 2 to 16 jet hole diameters and 1300 to 21,000, respectively. Three nozzle plates, having 48, 90, and 180 square-edged holes, were tested. For the maximum crossflow scheme, the presence of roughness results in small upstream reductions in heat transfer coefficient, with marked improvement in the downstream section; indicating that roughness elements can be used to compensate for the degradation that is usually associated with impingement on smooth surfaces.
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      Impingement Heat Transfer Within Arrays of Circular Jets: Part II—Effects of Crossflow in the Presence of Roughness Elements

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    http://yetl.yabesh.ir/yetl1/handle/yetl/103204
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    contributor authorT. A. Trabold
    contributor authorN. T. Obot
    date accessioned2017-05-08T23:26:00Z
    date available2017-05-08T23:26:00Z
    date copyrightOctober, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28586#594_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103204
    description abstractAn experimental investigation was carried out to determine the effects of jet-induced crossflow on impingement heat transfer from rough surfaces. The jets impinged on surfaces having repeated square ribs, with transverse flow of the spent air. Two crossflow schemes were tested: discharge of the spent air through two opposite sides (intermediate crossflow) and through one side (complete or maximum crossflow) of the rectangular impingement surface. The rib height was fixed at 0.813 mm, while the pitch-to-height ratio (p /e) was varied between 6 and 10. The study covered standoff spacing and jet Reynolds number in the range 2 to 16 jet hole diameters and 1300 to 21,000, respectively. Three nozzle plates, having 48, 90, and 180 square-edged holes, were tested. For the maximum crossflow scheme, the presence of roughness results in small upstream reductions in heat transfer coefficient, with marked improvement in the downstream section; indicating that roughness elements can be used to compensate for the degradation that is usually associated with impingement on smooth surfaces.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImpingement Heat Transfer Within Arrays of Circular Jets: Part II—Effects of Crossflow in the Presence of Roughness Elements
    typeJournal Paper
    journal volume109
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262153
    journal fristpage594
    journal lastpage601
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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