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    Large Eddy Simulation of Coflow Jet Airfoil at High Angle of Attack

    Source: Journal of Fluids Engineering:;2014:;volume( 136 ):;issue: 002::page 21101
    Author:
    Im, Hong
    ,
    Zha, Ge
    ,
    Dano, Bertrand P. E.
    DOI: 10.1115/1.4025649
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Large eddy simulation (LES) is conducted to investigate coflow jet (CFJ) airfoil flows at high angle of attack (AOA). The Smagorinsky model with Van Driest damping is employed to resolve the subgridscale stress. The fifthorder weighted essentially nonoscillatory (WENO) scheme is used for reconstruction of the inviscid flux and the fourthorder central differencing for the viscous flux. The LES results at an AOA of 0 deg, 12 deg, 25 deg, and 30 deg with momentum coefficients of Cخ¼â€‰= 0.15 and 0.08 are compared with the experiment to understand the flow structure of the jet mixing and flow separation. The quantitative prediction of lift and drag and qualitative prediction of vortex structures are in good agreement with experiment.
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      Large Eddy Simulation of Coflow Jet Airfoil at High Angle of Attack

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    http://yetl.yabesh.ir/yetl1/handle/yetl/154931
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    contributor authorIm, Hong
    contributor authorZha, Ge
    contributor authorDano, Bertrand P. E.
    date accessioned2017-05-09T01:08:23Z
    date available2017-05-09T01:08:23Z
    date issued2014
    identifier issn0098-2202
    identifier otherfe_136_02_021101.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/154931
    description abstractLarge eddy simulation (LES) is conducted to investigate coflow jet (CFJ) airfoil flows at high angle of attack (AOA). The Smagorinsky model with Van Driest damping is employed to resolve the subgridscale stress. The fifthorder weighted essentially nonoscillatory (WENO) scheme is used for reconstruction of the inviscid flux and the fourthorder central differencing for the viscous flux. The LES results at an AOA of 0 deg, 12 deg, 25 deg, and 30 deg with momentum coefficients of Cخ¼â€‰= 0.15 and 0.08 are compared with the experiment to understand the flow structure of the jet mixing and flow separation. The quantitative prediction of lift and drag and qualitative prediction of vortex structures are in good agreement with experiment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLarge Eddy Simulation of Coflow Jet Airfoil at High Angle of Attack
    typeJournal Paper
    journal volume136
    journal issue2
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4025649
    journal fristpage21101
    journal lastpage21101
    identifier eissn1528-901X
    treeJournal of Fluids Engineering:;2014:;volume( 136 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian