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    Fuel Droplet Evaporation in a Supercritical Environment

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 004::page 762
    Author:
    G. S. Zhu
    ,
    S. K. Aggarwal
    DOI: 10.1115/1.1385198
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports a numerical investigation of the transcritical droplet vaporization phenomena. The simulation is based on the time-dependent conservation equations for liquid and gas phases, pressure-dependent variable thermophysical properties, and a detailed treatment of liquid-vapor phase equilibrium at the droplet surface. The numerical solution of the two-phase equations employs an arbitrary Eulerian-Lagrangian, explicit-implicit method with a dynamically adaptive mesh. Three different equations of state (EOS), namely the Redlich-Kwong (RK), the Peng-Robinson (PR), and Soave-Redlich-Kwong (SRK) EOS, are employed to represent phase equilibrium at the droplet surface. In addition, two different methods are used to determine the liquid density. Results indicate that the predictions of RK-EOS are significantly different from those obtained by using the RK-EOS and SRK-EOS. For the phase-equilibrium of n-heptane-nitrogen system, the RK-EOS predicts higher liquid-phase solubility of nitrogen, higher fuel vapor concentration, lower critical-mixing-state temperature, and lower enthalpy of vaporization. As a consequence, it significantly overpredicts droplet vaporization rates, and underpredicts droplet lifetimes compared to those predicted by PR and SRK-EOS. In contrast, predictions using the PR-EOS and SRK-EOS show excellent agreement with each other and with experimental data over a wide range of conditions. A detailed investigation of the transcritical droplet vaporization phenomena indicates that at low to moderate ambient temperatures, the droplet lifetime first increases and then decreases as the ambient pressure is increased. At high ambient temperatures, however, the droplet lifetime decreases monotonically with pressure. This behavior is in accord with the reported experimental data.
    keyword(s): Pressure , Temperature , Vapors , Fuels , Evaporation , Equations , Nitrogen , Density , Phase equilibrium , Heptane , Equations of state AND High pressure (Physics) ,
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      Fuel Droplet Evaporation in a Supercritical Environment

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/126686
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorG. S. Zhu
    contributor authorS. K. Aggarwal
    date accessioned2017-05-09T00:07:19Z
    date available2017-05-09T00:07:19Z
    date copyrightOctober, 2002
    date issued2002
    identifier issn1528-8919
    identifier otherJETPEZ-26816#762_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126686
    description abstractThis paper reports a numerical investigation of the transcritical droplet vaporization phenomena. The simulation is based on the time-dependent conservation equations for liquid and gas phases, pressure-dependent variable thermophysical properties, and a detailed treatment of liquid-vapor phase equilibrium at the droplet surface. The numerical solution of the two-phase equations employs an arbitrary Eulerian-Lagrangian, explicit-implicit method with a dynamically adaptive mesh. Three different equations of state (EOS), namely the Redlich-Kwong (RK), the Peng-Robinson (PR), and Soave-Redlich-Kwong (SRK) EOS, are employed to represent phase equilibrium at the droplet surface. In addition, two different methods are used to determine the liquid density. Results indicate that the predictions of RK-EOS are significantly different from those obtained by using the RK-EOS and SRK-EOS. For the phase-equilibrium of n-heptane-nitrogen system, the RK-EOS predicts higher liquid-phase solubility of nitrogen, higher fuel vapor concentration, lower critical-mixing-state temperature, and lower enthalpy of vaporization. As a consequence, it significantly overpredicts droplet vaporization rates, and underpredicts droplet lifetimes compared to those predicted by PR and SRK-EOS. In contrast, predictions using the PR-EOS and SRK-EOS show excellent agreement with each other and with experimental data over a wide range of conditions. A detailed investigation of the transcritical droplet vaporization phenomena indicates that at low to moderate ambient temperatures, the droplet lifetime first increases and then decreases as the ambient pressure is increased. At high ambient temperatures, however, the droplet lifetime decreases monotonically with pressure. This behavior is in accord with the reported experimental data.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFuel Droplet Evaporation in a Supercritical Environment
    typeJournal Paper
    journal volume124
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1385198
    journal fristpage762
    journal lastpage770
    identifier eissn0742-4795
    keywordsPressure
    keywordsTemperature
    keywordsVapors
    keywordsFuels
    keywordsEvaporation
    keywordsEquations
    keywordsNitrogen
    keywordsDensity
    keywordsPhase equilibrium
    keywordsHeptane
    keywordsEquations of state AND High pressure (Physics)
    treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 004
    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