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    Influence of Upstream Flow Conditions on the Heat Transfer to Nozzle Guide Vanes

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 003::page 412
    Author:
    V. Krishnamoorthy
    ,
    S. P. Sukhatme
    ,
    B. R. Pai
    DOI: 10.1115/1.3262212
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of a combustor located just upstream of a nozzle guide vane cascade on the heat flux distribution to the nozzle guide vane was experimentally investigated. The surface temperature distribution around the convectively cooled vane of the cascade was obtained by locating the cascade, firstly in a low-turbulence uniform hot gas stream, secondly in a high-turbulence, uniform hot gas stream, and thirdly in a high-turbulence, nonuniform hot gas stream present just downstream of the combustor exit. The results indicate that the increased blade surface temperatures observed for the cascade placed just downstream of the combustor can be accounted for by the prevailing turbulence level measured at cascade inlet in cold-flow conditions and the average gas temperature at the cascade inlet.
    keyword(s): Flow (Dynamics) , Heat transfer , Nozzles , Cascades (Fluid dynamics) , Turbulence , Combustion chambers , Temperature , Blades , Temperature distribution AND Heat flux ,
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      Influence of Upstream Flow Conditions on the Heat Transfer to Nozzle Guide Vanes

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/104654
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    • Journal of Turbomachinery

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    contributor authorV. Krishnamoorthy
    contributor authorS. P. Sukhatme
    contributor authorB. R. Pai
    date accessioned2017-05-08T23:28:36Z
    date available2017-05-08T23:28:36Z
    date copyrightJuly, 1988
    date issued1988
    identifier issn0889-504X
    identifier otherJOTUEI-28590#412_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/104654
    description abstractThe influence of a combustor located just upstream of a nozzle guide vane cascade on the heat flux distribution to the nozzle guide vane was experimentally investigated. The surface temperature distribution around the convectively cooled vane of the cascade was obtained by locating the cascade, firstly in a low-turbulence uniform hot gas stream, secondly in a high-turbulence, uniform hot gas stream, and thirdly in a high-turbulence, nonuniform hot gas stream present just downstream of the combustor exit. The results indicate that the increased blade surface temperatures observed for the cascade placed just downstream of the combustor can be accounted for by the prevailing turbulence level measured at cascade inlet in cold-flow conditions and the average gas temperature at the cascade inlet.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluence of Upstream Flow Conditions on the Heat Transfer to Nozzle Guide Vanes
    typeJournal Paper
    journal volume110
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262212
    journal fristpage412
    journal lastpage416
    identifier eissn1528-8900
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsNozzles
    keywordsCascades (Fluid dynamics)
    keywordsTurbulence
    keywordsCombustion chambers
    keywordsTemperature
    keywordsBlades
    keywordsTemperature distribution AND Heat flux
    treeJournal of Turbomachinery:;1988:;volume( 110 ):;issue: 003
    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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