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    Inlet Condition Effects on the Tip Clearance Flow With Zonal Detached Eddy Simulation

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 004::page 41018
    Author:
    Riأ©ra, William
    ,
    Castillon, Lionel
    ,
    Marty, Julien
    ,
    Leboeuf, Francis
    DOI: 10.1115/1.4025216
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present study, the influence of the inlet condition on the tip clearance flow of an axial compressor is investigated. Two different zonal detached eddy simulations (ZDES) computations are carried out and compared to Reynoldsaveraged Navier–Stokes (RANS) and unsteady RANS (URANS) computations as well as to experimental data. A rotating distortion map of the flow cartography is set as inlet condition for the first ZDES computation. An azimuthally averaged inlet condition is used for the second one and uncouples the rotor tipleakage vortex flutter phenomenon, which stems from the arrival of the inlet guide vane wake from the behavior inherent to the rotor tipleakage vortex. In the studied configuration, the inlet guide vane tip vortex reveals to lower the effects from double leakage on the rotor. The topology of the rotor tipleakage vortex is described, and its development is analyzed.
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      Inlet Condition Effects on the Tip Clearance Flow With Zonal Detached Eddy Simulation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/156522
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    contributor authorRiأ©ra, William
    contributor authorCastillon, Lionel
    contributor authorMarty, Julien
    contributor authorLeboeuf, Francis
    date accessioned2017-05-09T01:13:16Z
    date available2017-05-09T01:13:16Z
    date issued2014
    identifier issn0889-504X
    identifier otherturb_136_04_041018.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156522
    description abstractIn the present study, the influence of the inlet condition on the tip clearance flow of an axial compressor is investigated. Two different zonal detached eddy simulations (ZDES) computations are carried out and compared to Reynoldsaveraged Navier–Stokes (RANS) and unsteady RANS (URANS) computations as well as to experimental data. A rotating distortion map of the flow cartography is set as inlet condition for the first ZDES computation. An azimuthally averaged inlet condition is used for the second one and uncouples the rotor tipleakage vortex flutter phenomenon, which stems from the arrival of the inlet guide vane wake from the behavior inherent to the rotor tipleakage vortex. In the studied configuration, the inlet guide vane tip vortex reveals to lower the effects from double leakage on the rotor. The topology of the rotor tipleakage vortex is described, and its development is analyzed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInlet Condition Effects on the Tip Clearance Flow With Zonal Detached Eddy Simulation
    typeJournal Paper
    journal volume136
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4025216
    journal fristpage41018
    journal lastpage41018
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2014:;volume( 136 ):;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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