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    A Study of Trailing Edge Losses in Organic Rankine Cycle Turbines

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 012::page 121003
    Author:
    Durأ، Galiana, Francisco J.
    ,
    Wheeler, Andrew P.S.
    ,
    Ong, Jonathan
    DOI: 10.1115/1.4033473
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, vane trailingedge losses which occur in organic rankine cycle (ORC) turbines are investigated. Experiments are performed to study the influence of dense gas effects on trailingedge loss in supersonic flows using a novel Ludwieg tube facility for the study of densegas flows. The data is also used to validate a computational fluid dynamics (CFD) flow solver. The computational simulations are then used to determine the contributions to loss from shocks and viscous effects which occur at the vane trailing edge. The results show that dense gas effects play a vital role in the structure of the trailingedge flow, and control the extent of shock and viscous losses.
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      A Study of Trailing Edge Losses in Organic Rankine Cycle Turbines

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    http://yetl.yabesh.ir/yetl1/handle/yetl/162829
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    contributor authorDurأ، Galiana, Francisco J.
    contributor authorWheeler, Andrew P.S.
    contributor authorOng, Jonathan
    date accessioned2017-05-09T01:34:26Z
    date available2017-05-09T01:34:26Z
    date issued2016
    identifier issn0889-504X
    identifier otherbio_138_07_071001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162829
    description abstractIn this paper, vane trailingedge losses which occur in organic rankine cycle (ORC) turbines are investigated. Experiments are performed to study the influence of dense gas effects on trailingedge loss in supersonic flows using a novel Ludwieg tube facility for the study of densegas flows. The data is also used to validate a computational fluid dynamics (CFD) flow solver. The computational simulations are then used to determine the contributions to loss from shocks and viscous effects which occur at the vane trailing edge. The results show that dense gas effects play a vital role in the structure of the trailingedge flow, and control the extent of shock and viscous losses.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Study of Trailing Edge Losses in Organic Rankine Cycle Turbines
    typeJournal Paper
    journal volume138
    journal issue12
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4033473
    journal fristpage121003
    journal lastpage121003
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2016:;volume( 138 ):;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