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    The Use of Fins to Reduce the Pressure Drop in a Rotating Cavity With a Radial Inflow

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003::page 349
    Author:
    J. W. Chew
    ,
    P. R. Farthing
    ,
    B. Stratford
    ,
    J. M. Owen
    DOI: 10.1115/1.3262279
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A 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.
    keyword(s): Cavities , Fins , Pressure drop , Inflow , Disks , Integral equations , Momentum , Flow (Dynamics) , Measurement , Surface roughness AND Flow visualization ,
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      The Use of Fins to Reduce the Pressure Drop in a Rotating Cavity With a Radial Inflow

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/106173
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    • Journal of Turbomachinery

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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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