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    An Open–Closed Flow Separation in a Compressor Radial Diffuser

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 010::page 101011-1
    Author:
    Duquesne, Pierre
    ,
    Dombard, Jerome
    ,
    Poujol, Nicolas
    ,
    Giauque, Alexis
    DOI: 10.1115/1.4065413
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large eddy simulations (LES) results are used to track flow separation zones in a splittered vaned radial diffuser near the compressor best efficiency at high rotation speed. The topology analysis reveals some closed separations at the corner of the blade and hub or shroud surface. In addition, an open–closed flow separation at the main blade pressure side is observed for the first time. The surface separation has the shape of a sheet at the blade mid-span, and the associated separation line is delimited only at its downstream extremity by a trailing edge node. This flow separation process is robust to a small shift in operating condition, and the separation surface remains essentially unchanged. A large flowrate variation converts the open–closed separation into a more classic closed separation. The evolution in time of the separation surface is also observed, and the authors conclude to the unsteady existence of the open–closed separation.
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      An Open–Closed Flow Separation in a Compressor Radial Diffuser

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4302636
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    contributor authorDuquesne, Pierre
    contributor authorDombard, Jerome
    contributor authorPoujol, Nicolas
    contributor authorGiauque, Alexis
    date accessioned2024-12-24T18:43:46Z
    date available2024-12-24T18:43:46Z
    date copyright5/8/2024 12:00:00 AM
    date issued2024
    identifier issn0889-504X
    identifier otherturbo_146_10_101011.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4302636
    description abstractLarge eddy simulations (LES) results are used to track flow separation zones in a splittered vaned radial diffuser near the compressor best efficiency at high rotation speed. The topology analysis reveals some closed separations at the corner of the blade and hub or shroud surface. In addition, an open–closed flow separation at the main blade pressure side is observed for the first time. The surface separation has the shape of a sheet at the blade mid-span, and the associated separation line is delimited only at its downstream extremity by a trailing edge node. This flow separation process is robust to a small shift in operating condition, and the separation surface remains essentially unchanged. A large flowrate variation converts the open–closed separation into a more classic closed separation. The evolution in time of the separation surface is also observed, and the authors conclude to the unsteady existence of the open–closed separation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Open–Closed Flow Separation in a Compressor Radial Diffuser
    typeJournal Paper
    journal volume146
    journal issue10
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4065413
    journal fristpage101011-1
    journal lastpage101011-8
    page8
    treeJournal of Turbomachinery:;2024:;volume( 146 ):;issue: 010
    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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