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    The Effect of Inlet Conditions on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001::page 145
    Author:
    C. A. Long
    ,
    J. M. Owen
    DOI: 10.1115/1.3262014
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flow visualization and heat transfer measurements have been made in the cavity between two corotating discs. The discs were 762 mm in diameter and could be rotated up to 2000 rpm. Air, at flow rates up to 0.1 kg/s, entered the cavity through either a central hole 76 mm in diameter or a porous inner shroud 380 mm in diameter; in both cases, the air left via holes in an outer shroud attached to the periphery of the discs. Flow visualization confirmed that Ekman-layer flow could occur: A source region, Ekman layers, sink layers, and interior core were observed. A simple theoretical model provided estimates of the size of the source region that were in satisfactory agreement with the observations. At sufficiently high rotational speeds, where Ekman layers form over much of the surface of each disc, measured Nusselt numbers were in reasonable agreement with values computed from the momentum-and energy-integral equations.
    keyword(s): Heat transfer , Fluids , Cavities , Outflow , Disks , Flow visualization , Flow (Dynamics) , Momentum , Measurement , Ekman dynamics AND Equations ,
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      The Effect of Inlet Conditions on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101866
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    contributor authorC. A. Long
    contributor authorJ. M. Owen
    date accessioned2017-05-08T23:23:44Z
    date available2017-05-08T23:23:44Z
    date copyrightJuly, 1986
    date issued1986
    identifier issn0889-504X
    identifier otherJOTUEI-28577#145_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101866
    description abstractFlow visualization and heat transfer measurements have been made in the cavity between two corotating discs. The discs were 762 mm in diameter and could be rotated up to 2000 rpm. Air, at flow rates up to 0.1 kg/s, entered the cavity through either a central hole 76 mm in diameter or a porous inner shroud 380 mm in diameter; in both cases, the air left via holes in an outer shroud attached to the periphery of the discs. Flow visualization confirmed that Ekman-layer flow could occur: A source region, Ekman layers, sink layers, and interior core were observed. A simple theoretical model provided estimates of the size of the source region that were in satisfactory agreement with the observations. At sufficiently high rotational speeds, where Ekman layers form over much of the surface of each disc, measured Nusselt numbers were in reasonable agreement with values computed from the momentum-and energy-integral equations.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of Inlet Conditions on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid
    typeJournal Paper
    journal volume108
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262014
    journal fristpage145
    journal lastpage152
    identifier eissn1528-8900
    keywordsHeat transfer
    keywordsFluids
    keywordsCavities
    keywordsOutflow
    keywordsDisks
    keywordsFlow visualization
    keywordsFlow (Dynamics)
    keywordsMomentum
    keywordsMeasurement
    keywordsEkman dynamics AND Equations
    treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 001
    contenttypeFulltext
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