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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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