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    Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002::page 243
    Author:
    N. Hay
    ,
    D. Lampard
    ,
    S. Benmansour
    DOI: 10.1115/1.3227408
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The strongest flow parameter governing the film cooling effectiveness provided by a row of holes is the blowing rate. Precise setting of the blowing rate at the design stage requires accurate data for the discharge coefficient of the holes. The effects of crossflow on the discharge coefficient have received scant attention in published work to date. In the present work, the discharge coefficient of single rows of holes has been measured in a specially constructed isothermal rig over a wide range of geometric and flow conditions. Mainstream and coolant Mach numbers have been varied independently over the range 0 to 0.4 for pressure ratios in the range 0 to 2. Cooling hole length to diameter ratios were varied between 2 and 6, and inclinations of 30, 60, and 90 deg were used. The results show that the influence of crossflow is strong and complex, particularly with regard to that on the coolant side. A large range of data is presented sufficient to permit the discharge coefficient to be inferred for many cases of practical importance. Suggestions are also made for a promising theoretical approach to this problem.
    keyword(s): Cooling , Discharge coefficient , Coolants , Flow (Dynamics) , Mach number , Design AND Pressure ,
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      Effect of Crossflows on the Discharge Coefficient of Film Cooling Holes

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/97091
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorN. Hay
    contributor authorD. Lampard
    contributor authorS. Benmansour
    date accessioned2017-05-08T23:15:32Z
    date available2017-05-08T23:15:32Z
    date copyrightApril, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26781#243_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97091
    description abstractThe strongest flow parameter governing the film cooling effectiveness provided by a row of holes is the blowing rate. Precise setting of the blowing rate at the design stage requires accurate data for the discharge coefficient of the holes. The effects of crossflow on the discharge coefficient have received scant attention in published work to date. In the present work, the discharge coefficient of single rows of holes has been measured in a specially constructed isothermal rig over a wide range of geometric and flow conditions. Mainstream and coolant Mach numbers have been varied independently over the range 0 to 0.4 for pressure ratios in the range 0 to 2. Cooling hole length to diameter ratios were varied between 2 and 6, and inclinations of 30, 60, and 90 deg were used. The results show that the influence of crossflow is strong and complex, particularly with regard to that on the coolant side. A large range of data is presented sufficient to permit the discharge coefficient to be inferred for many cases of practical importance. Suggestions are also made for a promising theoretical approach to this problem.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Crossflows on the Discharge Coefficient of Film Cooling Holes
    typeJournal Paper
    journal volume105
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227408
    journal fristpage243
    journal lastpage248
    identifier eissn0742-4795
    keywordsCooling
    keywordsDischarge coefficient
    keywordsCoolants
    keywordsFlow (Dynamics)
    keywordsMach number
    keywordsDesign AND Pressure
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002
    contenttypeFulltext
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