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    Flow Distributions and Discharge Coefficient Effects for Jet Array Impingement With Initial Crossflow

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002::page 296
    Author:
    L. W. Florschuetz
    ,
    Y. Isoda
    DOI: 10.1115/1.3227415
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Two-dimensional arrays of circular air jets impinging on a surface parallel to the jet orifice plate are considered. The jet flow, after impingement is constrained to exit in a single direction along the channel formed by the jet orifice plate and the impingement surface. In addition to the crossflow which originates from the jets following impingement, an initial (independent) crossflow is present which approaches the array through an upstream extension of the channel. The configurations considered are intended to model the impingement cooled midchord region of gas turbine airfoils in cases where an initial crossflow is also present. Experimentally determined row-by-row streamwise distributions of the jet and crossflow velocities are presented for ratios of the initial crossflow rate to the total jet flow rate ranging from zero to unity. Comparisons are drawn between the measured flow distributions and a theoretical model which is presented. Effects of crossflow velocity and impingement surface proximity on jet hole discharge coefficients are also presented and discussed.
    keyword(s): Flow (Dynamics) , Discharge coefficient , Jets , Channels (Hydraulic engineering) , Air jets , Gas turbines AND Airfoils ,
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      Flow Distributions and Discharge Coefficient Effects for Jet Array Impingement With Initial Crossflow

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/97098
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorL. W. Florschuetz
    contributor authorY. Isoda
    date accessioned2017-05-08T23:15:33Z
    date available2017-05-08T23:15:33Z
    date copyrightApril, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26781#296_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97098
    description abstractTwo-dimensional arrays of circular air jets impinging on a surface parallel to the jet orifice plate are considered. The jet flow, after impingement is constrained to exit in a single direction along the channel formed by the jet orifice plate and the impingement surface. In addition to the crossflow which originates from the jets following impingement, an initial (independent) crossflow is present which approaches the array through an upstream extension of the channel. The configurations considered are intended to model the impingement cooled midchord region of gas turbine airfoils in cases where an initial crossflow is also present. Experimentally determined row-by-row streamwise distributions of the jet and crossflow velocities are presented for ratios of the initial crossflow rate to the total jet flow rate ranging from zero to unity. Comparisons are drawn between the measured flow distributions and a theoretical model which is presented. Effects of crossflow velocity and impingement surface proximity on jet hole discharge coefficients are also presented and discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFlow Distributions and Discharge Coefficient Effects for Jet Array Impingement With Initial Crossflow
    typeJournal Paper
    journal volume105
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227415
    journal fristpage296
    journal lastpage304
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsDischarge coefficient
    keywordsJets
    keywordsChannels (Hydraulic engineering)
    keywordsAir jets
    keywordsGas turbines AND Airfoils
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002
    contenttypeFulltext
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