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    Visualization Studies in Rotating Disk Cavity Flows

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002::page 308
    Author:
    J. Nordquist
    ,
    S. Abrahamson
    ,
    J. Wechkin
    ,
    J. Eaton
    DOI: 10.1115/1.2927656
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study was performed in a simplified turbine disk cavity consisting of a single disk rotating near a stationary flat plate, bounded radially by an axial seal fixed to the plate. The disk Reynolds number was 6.2 × 105 . Cooling flow was supplied axially at a dimensionless radius of 0.33. Flow visualization showed boundary layers on both the rotating and stationary disks with the core between the layers rotating in solid body motion. At intermediate cooling flow rates, large vortical structures aligned with the disk spin axis and spanning the core were observed.
    keyword(s): Flow (Dynamics) , Cooling , Motion , Reynolds number , Flow visualization , Particle spin , Boundary layers , Cavity flows , Turbines , Visualization , Disks , Cavities , Flat plates AND Rotating Disks ,
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      Visualization Studies in Rotating Disk Cavity Flows

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/107772
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    • Journal of Turbomachinery

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    contributor authorJ. Nordquist
    contributor authorS. Abrahamson
    contributor authorJ. Wechkin
    contributor authorJ. Eaton
    date accessioned2017-05-08T23:34:09Z
    date available2017-05-08T23:34:09Z
    date copyrightApril, 1990
    date issued1990
    identifier issn0889-504X
    identifier otherJOTUEI-28601#308_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/107772
    description abstractAn experimental study was performed in a simplified turbine disk cavity consisting of a single disk rotating near a stationary flat plate, bounded radially by an axial seal fixed to the plate. The disk Reynolds number was 6.2 × 105 . Cooling flow was supplied axially at a dimensionless radius of 0.33. Flow visualization showed boundary layers on both the rotating and stationary disks with the core between the layers rotating in solid body motion. At intermediate cooling flow rates, large vortical structures aligned with the disk spin axis and spanning the core were observed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleVisualization Studies in Rotating Disk Cavity Flows
    typeJournal Paper
    journal volume112
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927656
    journal fristpage308
    journal lastpage310
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsCooling
    keywordsMotion
    keywordsReynolds number
    keywordsFlow visualization
    keywordsParticle spin
    keywordsBoundary layers
    keywordsCavity flows
    keywordsTurbines
    keywordsVisualization
    keywordsDisks
    keywordsCavities
    keywordsFlat plates AND Rotating Disks
    treeJournal of Turbomachinery:;1990:;volume( 112 ):;issue: 002
    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