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    Effects of Rib Arrangements on Pressure Drop and Heat Transfer in a Rib-Roughened Channel With a Sharp 180 deg Turn

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003::page 610
    Author:
    S. Mochizuki
    ,
    A. Murata
    ,
    M. Fukunaga
    DOI: 10.1115/1.2841165
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this study was to investigate, through experiments, the combined effects of a sharp 180 deg turn and rib patterns on the pressure drop performance and distributions of the local heat transfer coefficient in an entire two-pass rib-roughened channel with a 180 deg turn. The rib pitch-to-equivalent diameter ratio P/de was 1.0, the rib-height-to-equivalent diameter ratio e/de was 0.09, and the rib angle relative to the main flow direction was varied from 30 ∼ 90 deg with an interval of 15 deg. Experiments were conducted for Reynolds numbers in the range 4000 ∼ 30,000. It was disclosed that, due to the interactions between the bend-induced secondary flow and the rib-induced secondary flow, the combination of rib patterns in the channel before and after the turn causes considerable differences in the pressure drop and heat transfer performance of the entire channel.
    keyword(s): Heat transfer , Channels (Hydraulic engineering) , Pressure drop , Flow (Dynamics) , Heat transfer coefficients AND Reynolds number ,
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      Effects of Rib Arrangements on Pressure Drop and Heat Transfer in a Rib-Roughened Channel With a Sharp 180 deg Turn

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119614
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    • Journal of Turbomachinery

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    contributor authorS. Mochizuki
    contributor authorA. Murata
    contributor authorM. Fukunaga
    date accessioned2017-05-08T23:55:07Z
    date available2017-05-08T23:55:07Z
    date copyrightJuly, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28661#610_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119614
    description abstractThe objective of this study was to investigate, through experiments, the combined effects of a sharp 180 deg turn and rib patterns on the pressure drop performance and distributions of the local heat transfer coefficient in an entire two-pass rib-roughened channel with a 180 deg turn. The rib pitch-to-equivalent diameter ratio P/de was 1.0, the rib-height-to-equivalent diameter ratio e/de was 0.09, and the rib angle relative to the main flow direction was varied from 30 ∼ 90 deg with an interval of 15 deg. Experiments were conducted for Reynolds numbers in the range 4000 ∼ 30,000. It was disclosed that, due to the interactions between the bend-induced secondary flow and the rib-induced secondary flow, the combination of rib patterns in the channel before and after the turn causes considerable differences in the pressure drop and heat transfer performance of the entire channel.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Rib Arrangements on Pressure Drop and Heat Transfer in a Rib-Roughened Channel With a Sharp 180 deg Turn
    typeJournal Paper
    journal volume119
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841165
    journal fristpage610
    journal lastpage616
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsChannels (Hydraulic engineering)
    keywordsPressure drop
    keywordsFlow (Dynamics)
    keywordsHeat transfer coefficients AND Reynolds number
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 003
    contenttypeFulltext
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