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    A Study on Converging Thin Annular Jets

    Source: Journal of Fluids Engineering:;1997:;volume( 119 ):;issue: 004::page 923
    Author:
    D. Sivakumar
    ,
    B. N. Raghunandan
    DOI: 10.1115/1.2819518
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An interesting feature of jets from liquid-liquid coaxial swirl atomizers used in bipropellant rockets or elsewhere is that the outer jet results in a tulip shaped liquid bulb even at operating pressure levels. In this context, experiments have been performed to study the discharge and tulip characteristics of annular jets through qualitative simulation of outer jet flow conditions at which tulip bulb prevails. It is shown that the discharge coefficient increases steeply with Reynolds number, a trend which is distinct from that of circular orifices. The range of flow conditions at which tulip bulb prevails decreases with the annular gap. If a swirl component is introduced into the annular jet, it alters the discharge characteristics and the tulip range with a tendency to form multiple tulips. Variation of tulip length for different annular gaps shows a common trend when plotted against liquid flow rate. The experimental data of tulip length agree reasonably with the theoretical model reported in literature.
    keyword(s): Jets , Flow (Dynamics) , Reynolds number , Simulation , Pressure , Discharge coefficient , Orifices AND Rockets ,
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      A Study on Converging Thin Annular Jets

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    https://yetl.yabesh.ir/yetl1/handle/yetl/118858
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    contributor authorD. Sivakumar
    contributor authorB. N. Raghunandan
    date accessioned2017-05-08T23:53:46Z
    date available2017-05-08T23:53:46Z
    date copyrightDecember, 1997
    date issued1997
    identifier issn0098-2202
    identifier otherJFEGA4-27123#923_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118858
    description abstractAn interesting feature of jets from liquid-liquid coaxial swirl atomizers used in bipropellant rockets or elsewhere is that the outer jet results in a tulip shaped liquid bulb even at operating pressure levels. In this context, experiments have been performed to study the discharge and tulip characteristics of annular jets through qualitative simulation of outer jet flow conditions at which tulip bulb prevails. It is shown that the discharge coefficient increases steeply with Reynolds number, a trend which is distinct from that of circular orifices. The range of flow conditions at which tulip bulb prevails decreases with the annular gap. If a swirl component is introduced into the annular jet, it alters the discharge characteristics and the tulip range with a tendency to form multiple tulips. Variation of tulip length for different annular gaps shows a common trend when plotted against liquid flow rate. The experimental data of tulip length agree reasonably with the theoretical model reported in literature.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Study on Converging Thin Annular Jets
    typeJournal Paper
    journal volume119
    journal issue4
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2819518
    journal fristpage923
    journal lastpage928
    identifier eissn1528-901X
    keywordsJets
    keywordsFlow (Dynamics)
    keywordsReynolds number
    keywordsSimulation
    keywordsPressure
    keywordsDischarge coefficient
    keywordsOrifices AND Rockets
    treeJournal of Fluids Engineering:;1997:;volume( 119 ):;issue: 004
    contenttypeFulltext
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