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    Forced Convection Heat Transfer in Channels With Rib Turbulators Inclined at 45 deg

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 002::page 21012
    Author:
    Giovanni Tanda
    ,
    Roberto Abram
    DOI: 10.1115/1.2987241
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Local and average Nusselt numbers and friction factors are presented for rectangular channels with an aspect ratio of 5 and angled rib turbulators inclined at 45 deg with parallel orientations on one and two surfaces of the channel. The convective fluid was air, and the Reynolds number varied from 9000 to 35,500. The ratio of rib height to hydraulic diameter was 0.09, with the rib pitch-to-height ratio equal to 13.33 or 6.66. Experiments were based on the use of heating foils (for the attainment of uniform heat flux condition) and of the steady-state liquid crystal thermography (for the identification of isotherm lines and the reconstruction of local heat transfer coefficient). Local results showed quasiperiodic profiles of Nusselt number in the streamwise direction, whose features were strongly affected by the value of rib pitch and by the spanwise coordinate. For all the investigated geometries a heat transfer augmentation, relative to the fully developed smooth channel, was found; when inclined rib turbulators were placed on two opposite surfaces of the channel, the full-surface Nusselt number was higher (by 10–19%) than that for the one-ribbed wall channel, but pressure drop penalties also increased by a factor of about 3. For both the one- and two-ribbed wall channels, the best heat transfer performance for a constant pumping power, in the explored range of Reynolds number, was generally achieved by the larger rib pitch-to-height ratio (=13.33).
    keyword(s): Heat transfer , Channels (Hydraulic engineering) , Heat transfer coefficients , Flow (Dynamics) AND Friction ,
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      Forced Convection Heat Transfer in Channels With Rib Turbulators Inclined at 45 deg

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    http://yetl.yabesh.ir/yetl1/handle/yetl/142188
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    • Journal of Turbomachinery

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    contributor authorGiovanni Tanda
    contributor authorRoberto Abram
    date accessioned2017-05-09T00:35:51Z
    date available2017-05-09T00:35:51Z
    date copyrightApril, 2009
    date issued2009
    identifier issn0889-504X
    identifier otherJOTUEI-28754#021012_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142188
    description abstractLocal and average Nusselt numbers and friction factors are presented for rectangular channels with an aspect ratio of 5 and angled rib turbulators inclined at 45 deg with parallel orientations on one and two surfaces of the channel. The convective fluid was air, and the Reynolds number varied from 9000 to 35,500. The ratio of rib height to hydraulic diameter was 0.09, with the rib pitch-to-height ratio equal to 13.33 or 6.66. Experiments were based on the use of heating foils (for the attainment of uniform heat flux condition) and of the steady-state liquid crystal thermography (for the identification of isotherm lines and the reconstruction of local heat transfer coefficient). Local results showed quasiperiodic profiles of Nusselt number in the streamwise direction, whose features were strongly affected by the value of rib pitch and by the spanwise coordinate. For all the investigated geometries a heat transfer augmentation, relative to the fully developed smooth channel, was found; when inclined rib turbulators were placed on two opposite surfaces of the channel, the full-surface Nusselt number was higher (by 10–19%) than that for the one-ribbed wall channel, but pressure drop penalties also increased by a factor of about 3. For both the one- and two-ribbed wall channels, the best heat transfer performance for a constant pumping power, in the explored range of Reynolds number, was generally achieved by the larger rib pitch-to-height ratio (=13.33).
    publisherThe American Society of Mechanical Engineers (ASME)
    titleForced Convection Heat Transfer in Channels With Rib Turbulators Inclined at 45 deg
    typeJournal Paper
    journal volume131
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2987241
    journal fristpage21012
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsChannels (Hydraulic engineering)
    keywordsHeat transfer coefficients
    keywordsFlow (Dynamics) AND Friction
    treeJournal of Turbomachinery:;2009:;volume( 131 ):;issue: 002
    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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