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    Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 2—Detailed Measurements

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001::page 107
    Author:
    D. E. Nikitopoulos
    ,
    V. Eliades
    ,
    S. Acharya
    DOI: 10.1115/1.1331538
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed heat/mass transfer distributions are presented inside a two-pass rotating ribbed coolant channel for two profiled-rib configurations. Several profiled-rib configurations have been studied (Acharya et al., 2000), and it was found that the best performance was achieved by saw-tooth ribs, and a pyramid–valley rib combination. The profiled ribs were placed directly opposite to each other on the leading and trailing surfaces. Smooth side walls were used in all the experiments. Heat transfer measurements were compared with straight ribs of equal blockage ratio. The measurements were made in a two-pass rotating facility using the naphthalene sublimation mass transfer technique, which provides highly resolved surface distributions. The results presented are for a Reynolds number of 30,000, two rotation numbers (0 and 0.3), and include average heat/mass transfer over the entire inter-rib module as well as detailed heat/mass transfer contours for two profiled-rib cases. Significant enhancement of up to 25 percent in heat/mass transfer was obtained with the pyramid–valley and saw-tooth shaped ribs under rotating conditions.
    keyword(s): Mass transfer , Heat transfer , Channels (Hydraulic engineering) , Measurement , Rotation , Flow (Dynamics) , Coolants , Ducts , Reynolds number , Surface acoustic waves AND Heat ,
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      Heat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 2—Detailed Measurements

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    http://yetl.yabesh.ir/yetl1/handle/yetl/126086
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    • Journal of Turbomachinery

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    contributor authorD. E. Nikitopoulos
    contributor authorV. Eliades
    contributor authorS. Acharya
    date accessioned2017-05-09T00:06:20Z
    date available2017-05-09T00:06:20Z
    date copyrightJanuary, 2001
    date issued2001
    identifier issn0889-504X
    identifier otherJOTUEI-28686#107_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126086
    description abstractDetailed heat/mass transfer distributions are presented inside a two-pass rotating ribbed coolant channel for two profiled-rib configurations. Several profiled-rib configurations have been studied (Acharya et al., 2000), and it was found that the best performance was achieved by saw-tooth ribs, and a pyramid–valley rib combination. The profiled ribs were placed directly opposite to each other on the leading and trailing surfaces. Smooth side walls were used in all the experiments. Heat transfer measurements were compared with straight ribs of equal blockage ratio. The measurements were made in a two-pass rotating facility using the naphthalene sublimation mass transfer technique, which provides highly resolved surface distributions. The results presented are for a Reynolds number of 30,000, two rotation numbers (0 and 0.3), and include average heat/mass transfer over the entire inter-rib module as well as detailed heat/mass transfer contours for two profiled-rib cases. Significant enhancement of up to 25 percent in heat/mass transfer was obtained with the pyramid–valley and saw-tooth shaped ribs under rotating conditions.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer Enhancements in Rotating Two-Pass Coolant Channels With Profiled Ribs: Part 2—Detailed Measurements
    typeJournal Paper
    journal volume123
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1331538
    journal fristpage107
    journal lastpage114
    identifier eissn1528-8900
    keywordsMass transfer
    keywordsHeat transfer
    keywordsChannels (Hydraulic engineering)
    keywordsMeasurement
    keywordsRotation
    keywordsFlow (Dynamics)
    keywordsCoolants
    keywordsDucts
    keywordsReynolds number
    keywordsSurface acoustic waves AND Heat
    treeJournal of Turbomachinery:;2001:;volume( 123 ):;issue: 001
    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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