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    Theoretical Model of Buoyancy Induced Flow in Rotating Cavities

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 011::page 111005
    Author:
    Owen, J. Michael
    ,
    Tang, Hui
    DOI: 10.1115/1.4031353
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The Ekmanlayer equations, which have previously been solved for isothermal source–sink flow in a rotating cavity, are derived for buoyancyinduced flow. Although the flow in the inviscid core is threedimensional and unsteady, it is assumed that the flow in the Ekman layers is axisymmetric and steady; and, as for source–sink flow, the average mass flow rate in the Ekman layers is assumed to be invariant with radius. In addition, it is assumed that the flow in the core is adiabatic, and consequently the core temperature increases with radius and with rotational speed. Approximate solutions are obtained for laminar flow, and it is shown that the Nusselt numbers for the rotating disks and the mass flow rate in the Ekman layers are proportional to Grc1/4, where Grc is a Grashof number based on the rotational Reynolds number and the temperature difference between the disk and the core. The equation for the Nusselt numbers, which includes two empirical constants, depends strongly on the radial distribution of the temperature of the disks.
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      Theoretical Model of Buoyancy Induced Flow in Rotating Cavities

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/159987
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    • Journal of Turbomachinery

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    contributor authorOwen, J. Michael
    contributor authorTang, Hui
    date accessioned2017-05-09T01:24:48Z
    date available2017-05-09T01:24:48Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_11_111005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159987
    description abstractThe Ekmanlayer equations, which have previously been solved for isothermal source–sink flow in a rotating cavity, are derived for buoyancyinduced flow. Although the flow in the inviscid core is threedimensional and unsteady, it is assumed that the flow in the Ekman layers is axisymmetric and steady; and, as for source–sink flow, the average mass flow rate in the Ekman layers is assumed to be invariant with radius. In addition, it is assumed that the flow in the core is adiabatic, and consequently the core temperature increases with radius and with rotational speed. Approximate solutions are obtained for laminar flow, and it is shown that the Nusselt numbers for the rotating disks and the mass flow rate in the Ekman layers are proportional to Grc1/4, where Grc is a Grashof number based on the rotational Reynolds number and the temperature difference between the disk and the core. The equation for the Nusselt numbers, which includes two empirical constants, depends strongly on the radial distribution of the temperature of the disks.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTheoretical Model of Buoyancy Induced Flow in Rotating Cavities
    typeJournal Paper
    journal volume137
    journal issue11
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4031353
    journal fristpage111005
    journal lastpage111005
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 011
    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
    yabeshDSpacePersian