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    Visualization of the Wing-Tip Vortex in Temporal and Spatial Pressure Gradients

    Source: Journal of Fluids Engineering:;1991:;volume( 113 ):;issue: 003::page 511
    Author:
    X. Liang
    ,
    B. R. Ramaprian
    DOI: 10.1115/1.2909527
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The evolution of the longitudinal vortex in the near field of a rectangular wing has been visualized using smoke and laser light sheet. The smoke photographs have been used to obtain qualitative and some quantitative information on the effect of small temporal and spatial pressure gradients on the evolution of the vortex in this region. The experiments indicate that even small temporal retardation of the flow can produce a significant increase in the vortex size. This effect becomes larger with increase in retardation, angle of incidence and distance downstream from the trailing edge. Also, vortex “breakdown” was found to occur in many temporal-deceleration experiments. The vortex evolution was, however, found to be relatively insensitive to the presence of small spatial adverse pressure gradients along the flow direction. The study is preliminary in nature and needs to be supported by more extensive quantitative measurements.
    keyword(s): Visualization , Vortices , Pressure gradient , Wings , Flow (Dynamics) , Smoke , Lasers AND Measurement ,
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      Visualization of the Wing-Tip Vortex in Temporal and Spatial Pressure Gradients

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/108725
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    contributor authorX. Liang
    contributor authorB. R. Ramaprian
    date accessioned2017-05-08T23:35:48Z
    date available2017-05-08T23:35:48Z
    date copyrightSeptember, 1991
    date issued1991
    identifier issn0098-2202
    identifier otherJFEGA4-27061#511_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108725
    description abstractThe evolution of the longitudinal vortex in the near field of a rectangular wing has been visualized using smoke and laser light sheet. The smoke photographs have been used to obtain qualitative and some quantitative information on the effect of small temporal and spatial pressure gradients on the evolution of the vortex in this region. The experiments indicate that even small temporal retardation of the flow can produce a significant increase in the vortex size. This effect becomes larger with increase in retardation, angle of incidence and distance downstream from the trailing edge. Also, vortex “breakdown” was found to occur in many temporal-deceleration experiments. The vortex evolution was, however, found to be relatively insensitive to the presence of small spatial adverse pressure gradients along the flow direction. The study is preliminary in nature and needs to be supported by more extensive quantitative measurements.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleVisualization of the Wing-Tip Vortex in Temporal and Spatial Pressure Gradients
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2909527
    journal fristpage511
    journal lastpage515
    identifier eissn1528-901X
    keywordsVisualization
    keywordsVortices
    keywordsPressure gradient
    keywordsWings
    keywordsFlow (Dynamics)
    keywordsSmoke
    keywordsLasers AND Measurement
    treeJournal of Fluids Engineering:;1991:;volume( 113 ):;issue: 003
    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