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    Numerical Investigation of Boundary Layers in Wet Steam Nozzles

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 001::page 12606
    Author:
    Starzmann, Jörg
    ,
    Hughes, Fiona R.
    ,
    White, Alexander J.
    ,
    Grübel, Marius
    ,
    Vogt, Damian M.
    DOI: 10.1115/1.4034213
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Condensing nozzle flows have been used extensively to validate wet steam models. Many test cases are available in the literature, and in the past, a range of numerical studies have dealt with this challenging task. It is usually assumed that the nozzles provide a one- or two-dimensional flow with a fully turbulent boundary layer (BL). The present paper reviews these assumptions and investigates numerically the influence of boundary layers on dry and wet steam nozzle expansions. For the narrow nozzle of Moses and Stein, it is shown that the pressure distribution is significantly affected by the additional blockage due to the side wall boundary layer. Comparison of laminar and turbulent flow predictions for this nozzles suggests that laminar–turbulent transition only occurs after the throat. Other examples are the Binnie and Green nozzle and the Moore et al. nozzles for which it is known that sudden changes in wall curvature produce expansion and compression waves that interact with the boundary layers. The differences between two- and three-dimensional calculations for these cases and the influence of laminar and turbulent boundary layers are discussed. The present results reveal that boundary layer effects can have a considerable impact on the mean nozzle flow and thus on the validation process of condensation models. In order to verify the accuracy of turbulence modeling, a test case that is not widely known internationally is included within the present study. This experimental work is remarkable because it includes boundary layer data as well as the usual pressure measurements along the nozzle centerline. Predicted and measured boundary layer profiles are compared, and the effect of different turbulence models is discussed. Most of the numerical results are obtained with the in-house wet steam Reynolds-averaged Navier–Stokes (RANS) solver, Steamblock, but for the purpose of comparison, the commercial program ansys cfx is also used, providing a wider range of standard RANS-based turbulence models.
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      Numerical Investigation of Boundary Layers in Wet Steam Nozzles

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    contributor authorStarzmann, Jörg
    contributor authorHughes, Fiona R.
    contributor authorWhite, Alexander J.
    contributor authorGrübel, Marius
    contributor authorVogt, Damian M.
    date accessioned2017-11-25T07:21:23Z
    date available2017-11-25T07:21:23Z
    date copyright2016/8/9
    date issued2017
    identifier issn0742-4795
    identifier othergtp_139_01_012606.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4237034
    description abstractCondensing nozzle flows have been used extensively to validate wet steam models. Many test cases are available in the literature, and in the past, a range of numerical studies have dealt with this challenging task. It is usually assumed that the nozzles provide a one- or two-dimensional flow with a fully turbulent boundary layer (BL). The present paper reviews these assumptions and investigates numerically the influence of boundary layers on dry and wet steam nozzle expansions. For the narrow nozzle of Moses and Stein, it is shown that the pressure distribution is significantly affected by the additional blockage due to the side wall boundary layer. Comparison of laminar and turbulent flow predictions for this nozzles suggests that laminar–turbulent transition only occurs after the throat. Other examples are the Binnie and Green nozzle and the Moore et al. nozzles for which it is known that sudden changes in wall curvature produce expansion and compression waves that interact with the boundary layers. The differences between two- and three-dimensional calculations for these cases and the influence of laminar and turbulent boundary layers are discussed. The present results reveal that boundary layer effects can have a considerable impact on the mean nozzle flow and thus on the validation process of condensation models. In order to verify the accuracy of turbulence modeling, a test case that is not widely known internationally is included within the present study. This experimental work is remarkable because it includes boundary layer data as well as the usual pressure measurements along the nozzle centerline. Predicted and measured boundary layer profiles are compared, and the effect of different turbulence models is discussed. Most of the numerical results are obtained with the in-house wet steam Reynolds-averaged Navier–Stokes (RANS) solver, Steamblock, but for the purpose of comparison, the commercial program ansys cfx is also used, providing a wider range of standard RANS-based turbulence models.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Investigation of Boundary Layers in Wet Steam Nozzles
    typeJournal Paper
    journal volume139
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4034213
    journal fristpage12606
    journal lastpage012606-8
    treeJournal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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