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    Detailed Measurements of Local Heat Transfer Coefficient in the Entrance to Normal and Inclined Film Cooling Holes

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002::page 285
    Author:
    D. R. H. Gillespie
    ,
    S. T. Kohler
    ,
    A. R. Byerley
    ,
    P. T. Ireland
    ,
    Z. Wang
    ,
    T. V. Jones
    DOI: 10.1115/1.2836638
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The local heat transfer inside the entrance to large-scale models of film cooling holes has been measured using the transient heat transfer technique. The method employs temperature-sensitive liquid crystals to measure the surface temperature of large-scale perspex models. Full distributions of local Nusselt number were calculated based on the cooling passage centerline gas temperature ahead of the cooling hole. The circumferentially averaged Nusselt number was also calculated based on the local mixed bulk driving gas temperature to aid interpretation of the results, and to broaden the potential application of the data. Data are presented for a single film cooling hole inclined at 90 and 150 deg to the coolant duct wall. Both holes exhibited entry length heat transfer levels that were significantly lower than those predicted by entry length data in the presence of crossflow. The reasons for the comparative reduction are discussed in terms of the interpreted flow field.
    keyword(s): Cooling , Measurement , Heat transfer coefficients , Temperature , Heat transfer , Liquid crystals , Coolants , Ducts , Transient heat AND Flow (Dynamics) ,
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      Detailed Measurements of Local Heat Transfer Coefficient in the Entrance to Normal and Inclined Film Cooling Holes

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/117863
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    • Journal of Turbomachinery

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    contributor authorD. R. H. Gillespie
    contributor authorS. T. Kohler
    contributor authorA. R. Byerley
    contributor authorP. T. Ireland
    contributor authorZ. Wang
    contributor authorT. V. Jones
    date accessioned2017-05-08T23:51:58Z
    date available2017-05-08T23:51:58Z
    date copyrightApril, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28651#285_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117863
    description abstractThe local heat transfer inside the entrance to large-scale models of film cooling holes has been measured using the transient heat transfer technique. The method employs temperature-sensitive liquid crystals to measure the surface temperature of large-scale perspex models. Full distributions of local Nusselt number were calculated based on the cooling passage centerline gas temperature ahead of the cooling hole. The circumferentially averaged Nusselt number was also calculated based on the local mixed bulk driving gas temperature to aid interpretation of the results, and to broaden the potential application of the data. Data are presented for a single film cooling hole inclined at 90 and 150 deg to the coolant duct wall. Both holes exhibited entry length heat transfer levels that were significantly lower than those predicted by entry length data in the presence of crossflow. The reasons for the comparative reduction are discussed in terms of the interpreted flow field.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDetailed Measurements of Local Heat Transfer Coefficient in the Entrance to Normal and Inclined Film Cooling Holes
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2836638
    journal fristpage285
    journal lastpage290
    identifier eissn1528-8900
    keywordsCooling
    keywordsMeasurement
    keywordsHeat transfer coefficients
    keywordsTemperature
    keywordsHeat transfer
    keywordsLiquid crystals
    keywordsCoolants
    keywordsDucts
    keywordsTransient heat AND Flow (Dynamics)
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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