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    Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical Interpretation

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 012::page 121007
    Author:
    Vega, Almudena
    ,
    Corral, Roque
    DOI: 10.1115/1.4041377
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The dimensionless model presented in part I of the corresponding paper to describe the flutter onset of two-fin rotating seals is exploited to extract valuable engineering trends with the design parameters. The analytical expression for the nondimensional work-per-cycle depends on three dimensionless parameters of which two of them are new. These parameters are simple but interrelate the effect of the pressure ratio, the height, and length of the interfin geometry, the seal clearance, the nodal diameter (ND), the fluid swirl velocity, the vibration frequency, and the torsion center location in a compact and intricate manner. It is shown that nonrelated physical parameters can actually have an equivalent impact on seal stability. It is concluded that the pressure ratio can be stabilizing or destabilizing depending on the case, whereas the swirl of the flow is always destabilizing. Finally, a simple method to extend the model to multiple interfin cavities, neglecting the unsteady interaction among them, is described.
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      Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical Interpretation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4253373
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    contributor authorVega, Almudena
    contributor authorCorral, Roque
    date accessioned2019-02-28T11:09:58Z
    date available2019-02-28T11:09:58Z
    date copyright10/18/2018 12:00:00 AM
    date issued2018
    identifier issn0889-504X
    identifier otherturbo_140_12_121007.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253373
    description abstractThe dimensionless model presented in part I of the corresponding paper to describe the flutter onset of two-fin rotating seals is exploited to extract valuable engineering trends with the design parameters. The analytical expression for the nondimensional work-per-cycle depends on three dimensionless parameters of which two of them are new. These parameters are simple but interrelate the effect of the pressure ratio, the height, and length of the interfin geometry, the seal clearance, the nodal diameter (ND), the fluid swirl velocity, the vibration frequency, and the torsion center location in a compact and intricate manner. It is shown that nonrelated physical parameters can actually have an equivalent impact on seal stability. It is concluded that the pressure ratio can be stabilizing or destabilizing depending on the case, whereas the swirl of the flow is always destabilizing. Finally, a simple method to extend the model to multiple interfin cavities, neglecting the unsteady interaction among them, is described.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleConceptual Flutter Analysis of Labyrinth Seals Using Analytical Models—Part II: Physical Interpretation
    typeJournal Paper
    journal volume140
    journal issue12
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4041377
    journal fristpage121007
    journal lastpage121007-8
    treeJournal of Turbomachinery:;2018:;volume 140:;issue 012
    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