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    Performance of a Closed-Tube Aerosyphon With Large Length-Diameter Ratios

    Source: Journal of Offshore Mechanics and Arctic Engineering:;1989:;volume( 111 ):;issue: 004::page 337
    Author:
    G. S. H. Lock
    ,
    J. D. Kirchner
    DOI: 10.1115/1.3257104
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper reports an experimental investigation of heat transfer in the closed-tube aerosyphon (aerated-thermosyphon) for a range of conditions representative of northern field applications. In particular, attention is focused on the effect of using tubes with heated lengths not only greater than the cooled lengths, but very much greater than the tube diameter. Using three heated sections and one cooled section, the geometry of the device has been varied systematically with 10 < L H /d < 50 and 1 < L H /L C < 20. For any given geometry, the effect of air bubbling rate has been studied in the range of 0 < V̇ < 5 × 10−5 m3 /S. Using these ranges it has been possible to make comparisons with other thermosyphon and aerosyphon data. The results indicate that heat transfer coefficients are reduced by increasing either length-diameter ratio or heated-cooled length ratio. They also reveal that, in general terms, the aerosyphon is almost an order-of-magnitude more effective than the single-phase thermosyphon. Some obervations on the flow regimes are offered, and an empirical correlation is presented.
    keyword(s): Flow (Dynamics) , Heat transfer , Geometry AND Heat transfer coefficients ,
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      Performance of a Closed-Tube Aerosyphon With Large Length-Diameter Ratios

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/105790
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    contributor authorG. S. H. Lock
    contributor authorJ. D. Kirchner
    date accessioned2017-05-08T23:30:41Z
    date available2017-05-08T23:30:41Z
    date copyrightNovember, 1989
    date issued1989
    identifier issn0892-7219
    identifier otherJMOEEX-28061#337_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105790
    description abstractThe paper reports an experimental investigation of heat transfer in the closed-tube aerosyphon (aerated-thermosyphon) for a range of conditions representative of northern field applications. In particular, attention is focused on the effect of using tubes with heated lengths not only greater than the cooled lengths, but very much greater than the tube diameter. Using three heated sections and one cooled section, the geometry of the device has been varied systematically with 10 < L H /d < 50 and 1 < L H /L C < 20. For any given geometry, the effect of air bubbling rate has been studied in the range of 0 < V̇ < 5 × 10−5 m3 /S. Using these ranges it has been possible to make comparisons with other thermosyphon and aerosyphon data. The results indicate that heat transfer coefficients are reduced by increasing either length-diameter ratio or heated-cooled length ratio. They also reveal that, in general terms, the aerosyphon is almost an order-of-magnitude more effective than the single-phase thermosyphon. Some obervations on the flow regimes are offered, and an empirical correlation is presented.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance of a Closed-Tube Aerosyphon With Large Length-Diameter Ratios
    typeJournal Paper
    journal volume111
    journal issue4
    journal titleJournal of Offshore Mechanics and Arctic Engineering
    identifier doi10.1115/1.3257104
    journal fristpage337
    journal lastpage343
    identifier eissn1528-896X
    keywordsFlow (Dynamics)
    keywordsHeat transfer
    keywordsGeometry AND Heat transfer coefficients
    treeJournal of Offshore Mechanics and Arctic Engineering:;1989:;volume( 111 ):;issue: 004
    contenttypeFulltext
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