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    The Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow

    Source: Journal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001::page 126
    Author:
    V. Scherer
    ,
    S. Wittig
    DOI: 10.1115/1.2906520
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Convective heat transfer is examined in two typical examples of separated flows, namely, the flow over a backward-facing step and a two-dimensional jet entering a crossflow. Local Nusselt numbers were determined in and behind the recirculation region. The main parameters influencing the heat transfer, the Reynolds number, and the momentum flux ratio of the jet and the crossflow have been varied over a wide range. In addition to heat transfer measurements, the flow field has been documented using an LDA system and oil film technique. The static pressure distribution at the wall within the separated flow is also given. The measurements are compared with the results of a numerical code, based on a finite volume method, where the well known k-ε model is employed. The differences in Nusselt numbers predicted with one- and two-layer models are shown to demonstrate the influence of wall functions on heat transfer. The numerical and experimental results are compared with available data, and the differences and similarities in the heat transfer behavior of separated flows are discussed.
    keyword(s): Foundry coatings , Convection , Flow (Dynamics) , Heat transfer , Measurement , Reynolds number , Finite volume methods , Functions , Laser Doppler anemometry , Pressure AND Momentum ,
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      The Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow

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    contributor authorV. Scherer
    contributor authorS. Wittig
    date accessioned2017-05-08T23:35:36Z
    date available2017-05-08T23:35:36Z
    date copyrightJanuary, 1991
    date issued1991
    identifier issn1528-8919
    identifier otherJETPEZ-26683#126_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108580
    description abstractConvective heat transfer is examined in two typical examples of separated flows, namely, the flow over a backward-facing step and a two-dimensional jet entering a crossflow. Local Nusselt numbers were determined in and behind the recirculation region. The main parameters influencing the heat transfer, the Reynolds number, and the momentum flux ratio of the jet and the crossflow have been varied over a wide range. In addition to heat transfer measurements, the flow field has been documented using an LDA system and oil film technique. The static pressure distribution at the wall within the separated flow is also given. The measurements are compared with the results of a numerical code, based on a finite volume method, where the well known k-ε model is employed. The differences in Nusselt numbers predicted with one- and two-layer models are shown to demonstrate the influence of wall functions on heat transfer. The numerical and experimental results are compared with available data, and the differences and similarities in the heat transfer behavior of separated flows are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Influence of the Recirculation Region: A Comparison of the Convective Heat Transfer Downstream of a Backward-Facing Step and Behind a Jet in a Crossflow
    typeJournal Paper
    journal volume113
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2906520
    journal fristpage126
    journal lastpage134
    identifier eissn0742-4795
    keywordsFoundry coatings
    keywordsConvection
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsMeasurement
    keywordsReynolds number
    keywordsFinite volume methods
    keywordsFunctions
    keywordsLaser Doppler anemometry
    keywordsPressure AND Momentum
    treeJournal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001
    contenttypeFulltext
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