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    Measurement of Compressible Flow Pressure Losses in Wye-Junctions

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 003::page 535
    Author:
    N. I. Abou-Haidar
    ,
    S. L. Dixon
    DOI: 10.1115/1.2929442
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the compressible flow pressure losses in sharp-cornered wye-junctions with symmetric branches under dividing and combining flow conditions. Determination of the additional total pressure losses occurring in flow through several three-leg junctions, using dry air as the working fluid, has been made experimentally. Results covering a wide speed range up to choking are presented for 30, 60, and 90 deg wye-junctions. Separate flow visualization schlieren tests detected the presence of normal shock waves, located at up to one duct diameter downstream of the junction, and therefore confirmed the choking of the flow at the vena contracta. The highest attainable Mach number (M3 ) of the averaged whole flow was 0.9 for one of the dividing flow geometries and 0.65 for several of the combining flow cases. These values of M3 were the maximum possible and hence represent a limiting condition dictated by choking. In general, the compressible flow loss coefficients, caused by the presence of the wye-junctions, can be expected to be higher for dividing flows and lower for combining flows than would be the case for incompressible flows because of the influence of Mach number, M3 .
    keyword(s): Pressure , Compressible flow , Junctions , Flow (Dynamics) , Mach number , Fluids , Shock waves , Flow visualization , Bifurcation AND Ducts ,
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      Measurement of Compressible Flow Pressure Losses in Wye-Junctions

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    http://yetl.yabesh.ir/yetl1/handle/yetl/114557
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    contributor authorN. I. Abou-Haidar
    contributor authorS. L. Dixon
    date accessioned2017-05-08T23:45:50Z
    date available2017-05-08T23:45:50Z
    date copyrightJuly, 1994
    date issued1994
    identifier issn0889-504X
    identifier otherJOTUEI-28637#535_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114557
    description abstractThis paper considers the compressible flow pressure losses in sharp-cornered wye-junctions with symmetric branches under dividing and combining flow conditions. Determination of the additional total pressure losses occurring in flow through several three-leg junctions, using dry air as the working fluid, has been made experimentally. Results covering a wide speed range up to choking are presented for 30, 60, and 90 deg wye-junctions. Separate flow visualization schlieren tests detected the presence of normal shock waves, located at up to one duct diameter downstream of the junction, and therefore confirmed the choking of the flow at the vena contracta. The highest attainable Mach number (M3 ) of the averaged whole flow was 0.9 for one of the dividing flow geometries and 0.65 for several of the combining flow cases. These values of M3 were the maximum possible and hence represent a limiting condition dictated by choking. In general, the compressible flow loss coefficients, caused by the presence of the wye-junctions, can be expected to be higher for dividing flows and lower for combining flows than would be the case for incompressible flows because of the influence of Mach number, M3 .
    publisherThe American Society of Mechanical Engineers (ASME)
    titleMeasurement of Compressible Flow Pressure Losses in Wye-Junctions
    typeJournal Paper
    journal volume116
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929442
    journal fristpage535
    journal lastpage541
    identifier eissn1528-8900
    keywordsPressure
    keywordsCompressible flow
    keywordsJunctions
    keywordsFlow (Dynamics)
    keywordsMach number
    keywordsFluids
    keywordsShock waves
    keywordsFlow visualization
    keywordsBifurcation AND Ducts
    treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 003
    contenttypeFulltext
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