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    Endwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005::page 51006
    Author:
    Lyall, M. Eric
    ,
    King, Paul I.
    ,
    Sondergaard, Rolf
    DOI: 10.1115/1.4007801
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A high lift low pressure turbine (LPT) profile designated L2A is used as a test bed for studying the origin of endwall mixing loss and the role of vortical structures in loss development. It is shown analytically and experimentally that the mixing forces within the endwall wake can be decoupled into either mean flow or turbulent forces and can be further classified as either reversible or irreversible. Among the irreversible forces, mean flow shear is negligible compared to turbulent shear, suggesting that turbulence dissipation is the dominant cause of loss generation. As a result, the mean flow components of the vortical structures do not generate significant mixing losses. Rather than mixing effects, the mean flow of the vortices causes the suction surface boundary layer to separate inside the passage, thereby generating the large low energy regions typical of endwall flows. Losses are generated as the low energy regions mix out. This vortex separation effect is demonstrated with an experiment using a profile fence and pressure surface modification near the endwall. The findings in this paper suggest that profile modifications near the endwall that suppress flow separation may provide loss reductions additive to modifications aimed at weakening vortical structures, such as endwall contouring.
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      Endwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade

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    contributor authorLyall, M. Eric
    contributor authorKing, Paul I.
    contributor authorSondergaard, Rolf
    date accessioned2017-05-09T01:03:48Z
    date available2017-05-09T01:03:48Z
    date issued2013
    identifier issn0889-504X
    identifier otherturb_135_05_051006.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153486
    description abstractA high lift low pressure turbine (LPT) profile designated L2A is used as a test bed for studying the origin of endwall mixing loss and the role of vortical structures in loss development. It is shown analytically and experimentally that the mixing forces within the endwall wake can be decoupled into either mean flow or turbulent forces and can be further classified as either reversible or irreversible. Among the irreversible forces, mean flow shear is negligible compared to turbulent shear, suggesting that turbulence dissipation is the dominant cause of loss generation. As a result, the mean flow components of the vortical structures do not generate significant mixing losses. Rather than mixing effects, the mean flow of the vortices causes the suction surface boundary layer to separate inside the passage, thereby generating the large low energy regions typical of endwall flows. Losses are generated as the low energy regions mix out. This vortex separation effect is demonstrated with an experiment using a profile fence and pressure surface modification near the endwall. The findings in this paper suggest that profile modifications near the endwall that suppress flow separation may provide loss reductions additive to modifications aimed at weakening vortical structures, such as endwall contouring.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEndwall Loss and Mixing Analysis of a High Lift Low Pressure Turbine Cascade
    typeJournal Paper
    journal volume135
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4007801
    journal fristpage51006
    journal lastpage51006
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 005
    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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