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    Inviscid Approximations for Wall Jet-Receiver Interaction

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 001::page 60
    Author:
    H. S. Shen
    ,
    D. O. Rockwell
    DOI: 10.1115/1.3447217
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Potential flow, control volume, and frozen vorticity models have been used to analyze the wall jet-receiver system. The potential flow model predicts well the extent of the region of influence upstream of the receiver entrance for jet widths the same order as the receiver width, but the assumption of irrotationality drastically mispredicts the receiver spill flow angle. A control volume model which accounts for the extent of influence upstream of the receiver entrance and the possibility of continuous wall stall accurately predicts the receiver spill flow angle for most receiver spill flow ratios. The frozen vorticity model predicts velocity profiles in the receiver entrance region reasonably well, and slightly overpredicts the pressure recovery coefficient in the receiver entrance region.
    keyword(s): Approximation , Flow (Dynamics) , Vorticity , Entrance region , Flow control , Velocity AND Pressure ,
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      Inviscid Approximations for Wall Jet-Receiver Interaction

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/87693
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    • Journal of Fluids Engineering

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    contributor authorH. S. Shen
    contributor authorD. O. Rockwell
    date accessioned2017-05-08T22:59:01Z
    date available2017-05-08T22:59:01Z
    date copyrightMarch, 1975
    date issued1975
    identifier issn0098-2202
    identifier otherJFEGA4-26866#60_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/87693
    description abstractPotential flow, control volume, and frozen vorticity models have been used to analyze the wall jet-receiver system. The potential flow model predicts well the extent of the region of influence upstream of the receiver entrance for jet widths the same order as the receiver width, but the assumption of irrotationality drastically mispredicts the receiver spill flow angle. A control volume model which accounts for the extent of influence upstream of the receiver entrance and the possibility of continuous wall stall accurately predicts the receiver spill flow angle for most receiver spill flow ratios. The frozen vorticity model predicts velocity profiles in the receiver entrance region reasonably well, and slightly overpredicts the pressure recovery coefficient in the receiver entrance region.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInviscid Approximations for Wall Jet-Receiver Interaction
    typeJournal Paper
    journal volume97
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3447217
    journal fristpage60
    journal lastpage66
    identifier eissn1528-901X
    keywordsApproximation
    keywordsFlow (Dynamics)
    keywordsVorticity
    keywordsEntrance region
    keywordsFlow control
    keywordsVelocity AND Pressure
    treeJournal of Fluids Engineering:;1975:;volume( 097 ):;issue: 001
    contenttypeFulltext
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