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    Numerical Simulation of Unsteady Wake/Blade Interactions in Low-Pressure Turbine Flows Using an Intermittency Transport Equation

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 003::page 431
    Author:
    Y. B. Suzen
    ,
    P. G. Huang
    DOI: 10.1115/1.1860375
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An extensive computational investigation of the effects of unsteady wake/blade interactions on transition and separation in low-pressure turbines has been performed by numerical simulations of two recent sets of experiments using an intermittency transport equation. The experiments considered have been performed by Kaszeta and Simon and Stieger in order to investigate the effects of periodically passing wakes on laminar-to-turbulent transition and separation in low-pressure turbines. The test sections were designed to simulate unsteady wakes in turbine engines for studying their effects on boundary layers and separated flow regions over the suction surface. The numerical simulations of the unsteady wake/blade interaction experiments have been performed using an intermittency transport model. The intermittent behavior of the transitional flows is taken into account and incorporated into computations by modifying the eddy viscosity, with the intermittency factor. Turbulent quantities are predicted by using Menter’s two-equation turbulence model (SST). The intermittency factor is obtained from the transport equation model, which can produce both the experimentally observed streamwise variation of intermittency and a realistic profile in the cross-stream direction. Computational results are compared to the experiments. Overall, general trends are captured and prediction capabilities of the intermittency transport model for simulations of unsteady wake/blade interaction flowfields are demonstrated.
    keyword(s): Pressure , Flow (Dynamics) , Turbulence , Suction , Engineering simulation , Turbines , Blades , Wakes , Equations , Computer simulation , Separation (Technology) AND Boundary layers ,
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      Numerical Simulation of Unsteady Wake/Blade Interactions in Low-Pressure Turbine Flows Using an Intermittency Transport Equation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/132780
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    contributor authorY. B. Suzen
    contributor authorP. G. Huang
    date accessioned2017-05-09T00:18:06Z
    date available2017-05-09T00:18:06Z
    date copyrightJuly, 2005
    date issued2005
    identifier issn0889-504X
    identifier otherJOTUEI-28721#431_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/132780
    description abstractAn extensive computational investigation of the effects of unsteady wake/blade interactions on transition and separation in low-pressure turbines has been performed by numerical simulations of two recent sets of experiments using an intermittency transport equation. The experiments considered have been performed by Kaszeta and Simon and Stieger in order to investigate the effects of periodically passing wakes on laminar-to-turbulent transition and separation in low-pressure turbines. The test sections were designed to simulate unsteady wakes in turbine engines for studying their effects on boundary layers and separated flow regions over the suction surface. The numerical simulations of the unsteady wake/blade interaction experiments have been performed using an intermittency transport model. The intermittent behavior of the transitional flows is taken into account and incorporated into computations by modifying the eddy viscosity, with the intermittency factor. Turbulent quantities are predicted by using Menter’s two-equation turbulence model (SST). The intermittency factor is obtained from the transport equation model, which can produce both the experimentally observed streamwise variation of intermittency and a realistic profile in the cross-stream direction. Computational results are compared to the experiments. Overall, general trends are captured and prediction capabilities of the intermittency transport model for simulations of unsteady wake/blade interaction flowfields are demonstrated.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Simulation of Unsteady Wake/Blade Interactions in Low-Pressure Turbine Flows Using an Intermittency Transport Equation
    typeJournal Paper
    journal volume127
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.1860375
    journal fristpage431
    journal lastpage444
    identifier eissn1528-8900
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsTurbulence
    keywordsSuction
    keywordsEngineering simulation
    keywordsTurbines
    keywordsBlades
    keywordsWakes
    keywordsEquations
    keywordsComputer simulation
    keywordsSeparation (Technology) AND Boundary layers
    treeJournal of Turbomachinery:;2005:;volume( 127 ):;issue: 003
    contenttypeFulltext
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    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian