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    Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 1–Average Results

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001::page 97
    Author:
    S. Acharya
    ,
    V. Eliades
    ,
    D. E. Nikitopoulos
    DOI: 10.1115/1.1331539
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of ribs with different cross-stream profiles are investigated through detailed, surface mass (heat) transfer distributions along four active walls of a square duct containing a sharp 180 deg bend. The duct simulates two passes of an internal coolant channel in a gas turbine engine with ribs mounted on two opposite walls. Mass (heat) transfer measurements, taken using the naphthalene sublimation technique, are presented for a Reynolds number of 30,000, and rotation number of 0.3. Comparisons are made with conventional ribs having a rectangular cross section. It is shown that the use of certain profiled ribs provides considerable heat transfer enhancements over conventional ribs with the same blockage ratio in the duct. These enhancements are attributed to the generation of longitudinal vorticity (or secondary flows) by the profiled ribs in the channel.
    keyword(s): Heat transfer , Channels (Hydraulic engineering) , Flow (Dynamics) , Coolants , Ducts , Mass transfer , Heat , Measurement AND Reynolds number ,
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      Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 1–Average Results

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/126085
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    • Journal of Turbomachinery

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    contributor authorS. Acharya
    contributor authorV. Eliades
    contributor authorD. E. Nikitopoulos
    date accessioned2017-05-09T00:06:20Z
    date available2017-05-09T00:06:20Z
    date copyrightJanuary, 2001
    date issued2001
    identifier issn0889-504X
    identifier otherJOTUEI-28686#97_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126085
    description abstractThe effects of ribs with different cross-stream profiles are investigated through detailed, surface mass (heat) transfer distributions along four active walls of a square duct containing a sharp 180 deg bend. The duct simulates two passes of an internal coolant channel in a gas turbine engine with ribs mounted on two opposite walls. Mass (heat) transfer measurements, taken using the naphthalene sublimation technique, are presented for a Reynolds number of 30,000, and rotation number of 0.3. Comparisons are made with conventional ribs having a rectangular cross section. It is shown that the use of certain profiled ribs provides considerable heat transfer enhancements over conventional ribs with the same blockage ratio in the duct. These enhancements are attributed to the generation of longitudinal vorticity (or secondary flows) by the profiled ribs in the channel.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 1–Average Results
    typeJournal Paper
    journal volume123
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1331539
    journal fristpage97
    journal lastpage106
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsChannels (Hydraulic engineering)
    keywordsFlow (Dynamics)
    keywordsCoolants
    keywordsDucts
    keywordsMass transfer
    keywordsHeat
    keywordsMeasurement AND Reynolds number
    treeJournal of Turbomachinery:;2001:;volume( 123 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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