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    Tip Leakage Flow in Linear Compressor Cascade

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004::page 657
    Author:
    S. Kang
    ,
    C. Hirsch
    DOI: 10.1115/1.2929458
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Tip leakage flow in a linear compressor cascade of NACA 65-1810 profiles is investigated, for tip clearance levels of 1.0, 2.0, and 3.25 percent of chord at design and off-design flow conditions. Velocity and pressure data are collected from three transverse sections inside tip clearance and sixteen sections within flow passage. Tip separation vortex influence is identified from the data. Leakage flow mixing is clearly present inside the clearance and has a significant influence on the internal loss.
    keyword(s): Compressors , Cascades (Fluid dynamics) , Leakage flows , Clearances (Engineering) , Flow (Dynamics) , Design , Vortices , Separation (Technology) , Chords (Trusses) AND Pressure ,
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      Tip Leakage Flow in Linear Compressor Cascade

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/114518
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    • Journal of Turbomachinery

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    contributor authorS. Kang
    contributor authorC. Hirsch
    date accessioned2017-05-08T23:45:46Z
    date available2017-05-08T23:45:46Z
    date copyrightOctober, 1994
    date issued1994
    identifier issn0889-504X
    identifier otherJOTUEI-28639#657_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114518
    description abstractTip leakage flow in a linear compressor cascade of NACA 65-1810 profiles is investigated, for tip clearance levels of 1.0, 2.0, and 3.25 percent of chord at design and off-design flow conditions. Velocity and pressure data are collected from three transverse sections inside tip clearance and sixteen sections within flow passage. Tip separation vortex influence is identified from the data. Leakage flow mixing is clearly present inside the clearance and has a significant influence on the internal loss.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTip Leakage Flow in Linear Compressor Cascade
    typeJournal Paper
    journal volume116
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929458
    journal fristpage657
    journal lastpage664
    identifier eissn1528-8900
    keywordsCompressors
    keywordsCascades (Fluid dynamics)
    keywordsLeakage flows
    keywordsClearances (Engineering)
    keywordsFlow (Dynamics)
    keywordsDesign
    keywordsVortices
    keywordsSeparation (Technology)
    keywordsChords (Trusses) AND Pressure
    treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 004
    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
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