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    Investigation of the Calmed Region Behind a Turbulent Spot

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 004::page 802
    Author:
    J. P. Gostelow
    ,
    G. J. Walker
    ,
    G. Hong
    ,
    N. Melwani
    ,
    W. J. Solomon
    DOI: 10.1115/1.2841191
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements are presented of the calmed region behind triggered wave packets and turbulent spots under a controlled diffusion adverse pressure gradient in a wind tunnel. Similar measurements are also presented from the stator blades of an axial flow compressor, where turbulent spots are induced by the passing of rotor wakes. The purpose is to gain an appreciation of turbulent spot behavior under a strong adverse pressure gradient as a foundation for the more accurate modeling of spots and their environment in predictions of transitional boundary layer flows. Under an adverse pressure gradient the calmed region behind the spot is extensive; its interaction with the surrounding boundary layer is complex and is dependent on whether the surrounding natural boundary layer is laminar or turbulent. Some insights are gleaned concerning the behavior of the calmed region, which will subsequently be used in attempts to model the calmed region. Although these fundamental investigations of the calmed region have been extensive, much remains to be understood.
    keyword(s): Turbulence , Boundary layers , Pressure gradient , Measurement , Stators , Wind tunnels , Modeling , Rotors , Axial flow , Blades , Wakes , Wave packets , Flow (Dynamics) AND Diffusion (Physics) ,
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      Investigation of the Calmed Region Behind a Turbulent Spot

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119576
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    contributor authorJ. P. Gostelow
    contributor authorG. J. Walker
    contributor authorG. Hong
    contributor authorN. Melwani
    contributor authorW. J. Solomon
    date accessioned2017-05-08T23:55:03Z
    date available2017-05-08T23:55:03Z
    date copyrightOctober, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28663#802_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119576
    description abstractMeasurements are presented of the calmed region behind triggered wave packets and turbulent spots under a controlled diffusion adverse pressure gradient in a wind tunnel. Similar measurements are also presented from the stator blades of an axial flow compressor, where turbulent spots are induced by the passing of rotor wakes. The purpose is to gain an appreciation of turbulent spot behavior under a strong adverse pressure gradient as a foundation for the more accurate modeling of spots and their environment in predictions of transitional boundary layer flows. Under an adverse pressure gradient the calmed region behind the spot is extensive; its interaction with the surrounding boundary layer is complex and is dependent on whether the surrounding natural boundary layer is laminar or turbulent. Some insights are gleaned concerning the behavior of the calmed region, which will subsequently be used in attempts to model the calmed region. Although these fundamental investigations of the calmed region have been extensive, much remains to be understood.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation of the Calmed Region Behind a Turbulent Spot
    typeJournal Paper
    journal volume119
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841191
    journal fristpage802
    journal lastpage809
    identifier eissn1528-8900
    keywordsTurbulence
    keywordsBoundary layers
    keywordsPressure gradient
    keywordsMeasurement
    keywordsStators
    keywordsWind tunnels
    keywordsModeling
    keywordsRotors
    keywordsAxial flow
    keywordsBlades
    keywordsWakes
    keywordsWave packets
    keywordsFlow (Dynamics) AND Diffusion (Physics)
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 004
    contenttypeFulltext
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