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    Effects of Streamwise Pressure Gradient on Turbulent Spot Development

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004::page 737
    Author:
    J. P. Gostelow
    ,
    N. Melwani
    ,
    G. J. Walker
    DOI: 10.1115/1.2840929
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A pressure distribution representative of a controlled diffusion compressor blade suction surface is imposed on a flat plate. Boundary layer transition in this situation is investigated by triggering a wave packet, which evolves into a turbulent spot. The development from wave packet to turbulent spot is observed and the interactions of the turbulent spot with the ongoing natural transition and the ensuing turbulent boundary layer are examined. Under this steeply diffusing pressure distribution, strong amplification of primary instabilities prevails. Breakdown to turbulence is instigated near the centerline and propagates transversely along the wave packet until the turbulent region dominates. An extensive calmed region is present behind the spot, which persists well into the surrounding turbulent layer. Celerities of spot leading and trailing edges are presented, as is the spanwise spreading half-angle. Corresponding measurements for spots under a wide range of imposed pressure gradients are compiled and the present results are compared with those of other authors. Resulting correlations for spot propagation parameters are provided for use in computational modeling of the transition region under variable pressure gradients.
    keyword(s): Turbulence , Pressure gradient , Wave packets , Pressure , Diffusion (Physics) , Measurement , Boundary layers , Blades , Boundary layer turbulence , Flat plates , Suction , Computer simulation AND Compressors ,
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      Effects of Streamwise Pressure Gradient on Turbulent Spot Development

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/117803
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    • Journal of Turbomachinery

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    contributor authorJ. P. Gostelow
    contributor authorN. Melwani
    contributor authorG. J. Walker
    date accessioned2017-05-08T23:51:50Z
    date available2017-05-08T23:51:50Z
    date copyrightOctober, 1996
    date issued1996
    identifier issn0889-504X
    identifier otherJOTUEI-28655#737_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/117803
    description abstractA pressure distribution representative of a controlled diffusion compressor blade suction surface is imposed on a flat plate. Boundary layer transition in this situation is investigated by triggering a wave packet, which evolves into a turbulent spot. The development from wave packet to turbulent spot is observed and the interactions of the turbulent spot with the ongoing natural transition and the ensuing turbulent boundary layer are examined. Under this steeply diffusing pressure distribution, strong amplification of primary instabilities prevails. Breakdown to turbulence is instigated near the centerline and propagates transversely along the wave packet until the turbulent region dominates. An extensive calmed region is present behind the spot, which persists well into the surrounding turbulent layer. Celerities of spot leading and trailing edges are presented, as is the spanwise spreading half-angle. Corresponding measurements for spots under a wide range of imposed pressure gradients are compiled and the present results are compared with those of other authors. Resulting correlations for spot propagation parameters are provided for use in computational modeling of the transition region under variable pressure gradients.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffects of Streamwise Pressure Gradient on Turbulent Spot Development
    typeJournal Paper
    journal volume118
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2840929
    journal fristpage737
    journal lastpage743
    identifier eissn1528-8900
    keywordsTurbulence
    keywordsPressure gradient
    keywordsWave packets
    keywordsPressure
    keywordsDiffusion (Physics)
    keywordsMeasurement
    keywordsBoundary layers
    keywordsBlades
    keywordsBoundary layer turbulence
    keywordsFlat plates
    keywordsSuction
    keywordsComputer simulation AND Compressors
    treeJournal of Turbomachinery:;1996:;volume( 118 ):;issue: 004
    contenttypeFulltext
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