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    Turbulent Jets in a Confined Crossflow

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 004::page 551
    Author:
    R. L. Stoy
    ,
    Y. Ben-Haim
    DOI: 10.1115/1.3447069
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and analytical study of the deflection and impingement of turbulent jets in a confined crossflow, a geometry which occurs in gas turbine blade impingement cooling schemes, is presented. The range of jet and crossflow Reynolds numbers investigated is directly applicable to turbine blade configuratons. A simple one-dimensional analysis using the basic conservation equations is developed to predict jet trajectory, average jet properties, and impingement point for spatially variable crossflow velocity profiles. The simplicity of the one-dimensional analysis makes it more suited to design calculations than two-dimensional jet analyses. Other crossflow velocity profiles are studied and jet development is successfully predicted by the analysis for all cases.
    keyword(s): Jets , Turbulence , Reynolds number , Turbine blades , Trajectories (Physics) , Design , Gas turbines , Impingement cooling , Blades , Deflection , Equations AND Geometry ,
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      Turbulent Jets in a Confined Crossflow

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/163861
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    contributor authorR. L. Stoy
    contributor authorY. Ben-Haim
    date accessioned2017-05-09T01:36:31Z
    date available2017-05-09T01:36:31Z
    date copyrightDecember, 1973
    date issued1973
    identifier issn0098-2202
    identifier otherJFEGA4-26851#551_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163861
    description abstractAn experimental and analytical study of the deflection and impingement of turbulent jets in a confined crossflow, a geometry which occurs in gas turbine blade impingement cooling schemes, is presented. The range of jet and crossflow Reynolds numbers investigated is directly applicable to turbine blade configuratons. A simple one-dimensional analysis using the basic conservation equations is developed to predict jet trajectory, average jet properties, and impingement point for spatially variable crossflow velocity profiles. The simplicity of the one-dimensional analysis makes it more suited to design calculations than two-dimensional jet analyses. Other crossflow velocity profiles are studied and jet development is successfully predicted by the analysis for all cases.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTurbulent Jets in a Confined Crossflow
    typeJournal Paper
    journal volume95
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3447069
    journal fristpage551
    journal lastpage556
    identifier eissn1528-901X
    keywordsJets
    keywordsTurbulence
    keywordsReynolds number
    keywordsTurbine blades
    keywordsTrajectories (Physics)
    keywordsDesign
    keywordsGas turbines
    keywordsImpingement cooling
    keywordsBlades
    keywordsDeflection
    keywordsEquations AND Geometry
    treeJournal of Fluids Engineering:;1973:;volume( 095 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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