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    LES and RANS Studies of Oscillating Flows over Flat Plate

    Source: Journal of Engineering Mechanics:;2000:;Volume ( 126 ):;issue: 002
    Author:
    Chin-Tsau Hsu
    ,
    Xiyun Lu
    ,
    Man-Kim Kwan
    DOI: 10.1061/(ASCE)0733-9399(2000)126:2(186)
    Publisher: American Society of Civil Engineers
    Abstract: Oscillatory flows over a flat plate are studied by using Large Eddy Simulation (LES) and Reynolds-Average Navier-Stokes (RANS) methods. A dynamic subgrid scale (SGS) model is employed in LES, while the Saffman's turbulence model in RANS. The mean velocity profile, the turbulence intensity, and the wall shear stress are computed and compared with earlier experimental and numerical works. The results indicate that the flow behaviors are quite different during the accelerating and decelerating phases of the oscillating cycle. The transition from laminar to turbulent is also investigated as a function of the Reynolds number, R, which represents the square of the ratio of the oscillation amplitude at free stream to the thickness of the Stokes layer at the plate. The present results both from LES and RANS show that the transition occurs in the range of 5 × 10
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      LES and RANS Studies of Oscillating Flows over Flat Plate

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    http://yetl.yabesh.ir/yetl1/handle/yetl/85147
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    contributor authorChin-Tsau Hsu
    contributor authorXiyun Lu
    contributor authorMan-Kim Kwan
    date accessioned2017-05-08T22:39:09Z
    date available2017-05-08T22:39:09Z
    date copyrightFebruary 2000
    date issued2000
    identifier other%28asce%290733-9399%282000%29126%3A2%28186%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/85147
    description abstractOscillatory flows over a flat plate are studied by using Large Eddy Simulation (LES) and Reynolds-Average Navier-Stokes (RANS) methods. A dynamic subgrid scale (SGS) model is employed in LES, while the Saffman's turbulence model in RANS. The mean velocity profile, the turbulence intensity, and the wall shear stress are computed and compared with earlier experimental and numerical works. The results indicate that the flow behaviors are quite different during the accelerating and decelerating phases of the oscillating cycle. The transition from laminar to turbulent is also investigated as a function of the Reynolds number, R, which represents the square of the ratio of the oscillation amplitude at free stream to the thickness of the Stokes layer at the plate. The present results both from LES and RANS show that the transition occurs in the range of 5 × 10
    publisherAmerican Society of Civil Engineers
    titleLES and RANS Studies of Oscillating Flows over Flat Plate
    typeJournal Paper
    journal volume126
    journal issue2
    journal titleJournal of Engineering Mechanics
    identifier doi10.1061/(ASCE)0733-9399(2000)126:2(186)
    treeJournal of Engineering Mechanics:;2000:;Volume ( 126 ):;issue: 002
    contenttypeFulltext
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