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    Jet Breakup and Mixing Throat Lengths for the Liquid Jet Gas Pump

    Source: Journal of Fluids Engineering:;1974:;volume( 096 ):;issue: 003::page 216
    Author:
    R. G. Cunningham
    ,
    R. J. Dopkin
    DOI: 10.1115/1.3447144
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Gas compression with a liquid jet occurs isothermally and hence with minimum work. Performance characteristics of the liquid jet gas pump (efficiency and compression ratio versus inlet volumetric flow ratio) are predicted accurately by a one-dimensional analysis providing the mixing zone remains in the throat. Jet breakup was investigated to enable prediction of required throat length and to improve efficiency. Effects of throat length, nozzle contour and spacing, nozzle-throat area ratio (0.15 to 0.45), jet velocity and suction pressure were investigated. Optimum throat lengths were found; corresponding efficiencies exceed 40 percent. Two jet breakup flow regimes were found: impact and jet disintegration. For the impact regime, jet breakup length-depends on inlet velocity ratio, jet Reynolds number and nozzle-to-throat area ratio. Optimum throat lengths were found to be an empirical function of nozzle-to-throat area ratio and ranged from 12 to 32 throat dia. These results, coupled with the one-dimensional model, permit design of efficient liquid jet gas pumps.
    keyword(s): Pumps , Nozzles , Compression , Flow (Dynamics) , Suction , Reynolds number , Design , Performance characterization AND Pressure ,
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      Jet Breakup and Mixing Throat Lengths for the Liquid Jet Gas Pump

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/164871
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    • Journal of Fluids Engineering

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    contributor authorR. G. Cunningham
    contributor authorR. J. Dopkin
    date accessioned2017-05-09T01:38:18Z
    date available2017-05-09T01:38:18Z
    date copyrightSeptember, 1974
    date issued1974
    identifier issn0098-2202
    identifier otherJFEGA4-26860#216_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164871
    description abstractGas compression with a liquid jet occurs isothermally and hence with minimum work. Performance characteristics of the liquid jet gas pump (efficiency and compression ratio versus inlet volumetric flow ratio) are predicted accurately by a one-dimensional analysis providing the mixing zone remains in the throat. Jet breakup was investigated to enable prediction of required throat length and to improve efficiency. Effects of throat length, nozzle contour and spacing, nozzle-throat area ratio (0.15 to 0.45), jet velocity and suction pressure were investigated. Optimum throat lengths were found; corresponding efficiencies exceed 40 percent. Two jet breakup flow regimes were found: impact and jet disintegration. For the impact regime, jet breakup length-depends on inlet velocity ratio, jet Reynolds number and nozzle-to-throat area ratio. Optimum throat lengths were found to be an empirical function of nozzle-to-throat area ratio and ranged from 12 to 32 throat dia. These results, coupled with the one-dimensional model, permit design of efficient liquid jet gas pumps.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleJet Breakup and Mixing Throat Lengths for the Liquid Jet Gas Pump
    typeJournal Paper
    journal volume96
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3447144
    journal fristpage216
    journal lastpage226
    identifier eissn1528-901X
    keywordsPumps
    keywordsNozzles
    keywordsCompression
    keywordsFlow (Dynamics)
    keywordsSuction
    keywordsReynolds number
    keywordsDesign
    keywordsPerformance characterization AND Pressure
    treeJournal of Fluids Engineering:;1974:;volume( 096 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian