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    Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001::page 97
    Author:
    T. Valkov
    ,
    C. S. Tan
    DOI: 10.1115/1.2835647
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computational approach, based on a spectral-element Navier–Stokes solver, has been applied to the study of the unsteady flow arising from wake–stator interaction. Direct, as well as turbulence-model calculations, provide insight into the mechanics of the unsteady flow and demonstrate the potential for controlling its effects. The results show that the interaction between the wakes and the stator blades produces a characteristic pattern of vortical disturbances, which have been correlated to the pressure fluctuations. Within the stator passage, the wakes migrate toward the pressure surface where they evolve into counterrotating vortices. These vortices are the dominant source of disturbances over the pressure surface of the stator blade. Over the suction surface of the stator blade, the disturbances are due to the distortion and detachment of boundary layer fluid. They can be reduced by tailoring the blade loading or by applying nonuniform suction.
    keyword(s): Wakes , Blades , Stators , Unsteady flow , Pressure , Suction , Vortices , Fluctuations (Physics) , Fluids , Turbulence AND Boundary layers ,
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      Control of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes

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    http://yetl.yabesh.ir/yetl1/handle/yetl/116175
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    contributor authorT. Valkov
    contributor authorC. S. Tan
    date accessioned2017-05-08T23:48:39Z
    date available2017-05-08T23:48:39Z
    date copyrightJanuary, 1995
    date issued1995
    identifier issn0889-504X
    identifier otherJOTUEI-28642#97_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116175
    description abstractA computational approach, based on a spectral-element Navier–Stokes solver, has been applied to the study of the unsteady flow arising from wake–stator interaction. Direct, as well as turbulence-model calculations, provide insight into the mechanics of the unsteady flow and demonstrate the potential for controlling its effects. The results show that the interaction between the wakes and the stator blades produces a characteristic pattern of vortical disturbances, which have been correlated to the pressure fluctuations. Within the stator passage, the wakes migrate toward the pressure surface where they evolve into counterrotating vortices. These vortices are the dominant source of disturbances over the pressure surface of the stator blade. Over the suction surface of the stator blade, the disturbances are due to the distortion and detachment of boundary layer fluid. They can be reduced by tailoring the blade loading or by applying nonuniform suction.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleControl of the Unsteady Flow in a Stator Blade Row Interacting With Upstream Moving Wakes
    typeJournal Paper
    journal volume117
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2835647
    journal fristpage97
    journal lastpage105
    identifier eissn1528-8900
    keywordsWakes
    keywordsBlades
    keywordsStators
    keywordsUnsteady flow
    keywordsPressure
    keywordsSuction
    keywordsVortices
    keywordsFluctuations (Physics)
    keywordsFluids
    keywordsTurbulence AND Boundary layers
    treeJournal of Turbomachinery:;1995:;volume( 117 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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