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contributor authorJ. W. Chew
contributor authorP. R. Farthing
contributor authorB. Stratford
contributor authorJ. M. Owen
date accessioned2017-05-08T23:31:21Z
date available2017-05-08T23:31:21Z
date copyrightJuly, 1989
date issued1989
identifier issn0889-504X
identifier otherJOTUEI-28596#349_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106173
description abstractA combined theoretical and experimental study of radial inflow through a rotating cavity is reported. It is shown that radial fins attached to one of the disks are effective in reducing the pressure drop across the cavity. The mathematical model, is an extension of earlier plane-disk momentum-integral methods; the fins are treated as rectangular rib elements and a rough-disk model is derived. Numerical solutions of the integral equations are given. An approximate linear solution is also derived. Experiments were conducted when both disks were plane and when one of the disks was fitted with 60 radial fins. Flow visualization revealed the flow structure in the cavity and confirmed some of the assumptions used in the theoretical model. Measurements and predictions of the pressure drop across the cavity were in reasonable agreement.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Use of Fins to Reduce the Pressure Drop in a Rotating Cavity With a Radial Inflow
typeJournal Paper
journal volume111
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262279
journal fristpage349
journal lastpage356
identifier eissn1528-8900
keywordsCavities
keywordsFins
keywordsPressure drop
keywordsInflow
keywordsDisks
keywordsIntegral equations
keywordsMomentum
keywordsFlow (Dynamics)
keywordsMeasurement
keywordsSurface roughness AND Flow visualization
treeJournal of Turbomachinery:;1989:;volume( 111 ):;issue: 003
contenttypeFulltext


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