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    Dependence of Shock Characteristics on Droplet Size in Supersonic Two-Phase Mixtures

    Source: Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 001::page 54
    Author:
    W. J. Comfort
    ,
    C. T. Crowe
    DOI: 10.1115/1.3240624
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a dispersed two-phase flow, the mixture chokes at a velocity well below the vapor choking velocity, as shown by the velocity at the throat of a converging-diverging, two-phase, supersonic nozzle. The formation and abruptness of a normal shock wave in a two-phase mixture depends strongly on the coupling between phases, particularly upon droplet size. As droplet size becomes small, the mixture behaves as a continuum, and sharp discontinuities can occur at velocities above the two-phase choking velocity but below the vapor sonic velocity. An approximate analysis is performed to incidate the droplet size at which continuum behavior might be expected to occur. A numerical model, which includes the drag, buoyancy, Basset force, and the force associated with the virtual mass effect, is used to show droplet-size dependence in two-phase normal shock waves. For the examples presented, continuum behavior apparently is approached at droplet diameters between 1 and 2 μm, even through normal shock waves.
    keyword(s): Shock (Mechanics) , Mixtures , Shock waves , Force , Vapors , Computer simulation , Drag (Fluid dynamics) , Buoyancy , Nozzles AND Two-phase flow ,
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      Dependence of Shock Characteristics on Droplet Size in Supersonic Two-Phase Mixtures

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    http://yetl.yabesh.ir/yetl1/handle/yetl/93527
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    contributor authorW. J. Comfort
    contributor authorC. T. Crowe
    date accessioned2017-05-08T23:09:11Z
    date available2017-05-08T23:09:11Z
    date copyrightMarch, 1980
    date issued1980
    identifier issn0098-2202
    identifier otherJFEGA4-26955#54_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93527
    description abstractIn a dispersed two-phase flow, the mixture chokes at a velocity well below the vapor choking velocity, as shown by the velocity at the throat of a converging-diverging, two-phase, supersonic nozzle. The formation and abruptness of a normal shock wave in a two-phase mixture depends strongly on the coupling between phases, particularly upon droplet size. As droplet size becomes small, the mixture behaves as a continuum, and sharp discontinuities can occur at velocities above the two-phase choking velocity but below the vapor sonic velocity. An approximate analysis is performed to incidate the droplet size at which continuum behavior might be expected to occur. A numerical model, which includes the drag, buoyancy, Basset force, and the force associated with the virtual mass effect, is used to show droplet-size dependence in two-phase normal shock waves. For the examples presented, continuum behavior apparently is approached at droplet diameters between 1 and 2 μm, even through normal shock waves.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDependence of Shock Characteristics on Droplet Size in Supersonic Two-Phase Mixtures
    typeJournal Paper
    journal volume102
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3240624
    journal fristpage54
    journal lastpage58
    identifier eissn1528-901X
    keywordsShock (Mechanics)
    keywordsMixtures
    keywordsShock waves
    keywordsForce
    keywordsVapors
    keywordsComputer simulation
    keywordsDrag (Fluid dynamics)
    keywordsBuoyancy
    keywordsNozzles AND Two-phase flow
    treeJournal of Fluids Engineering:;1980:;volume( 102 ):;issue: 001
    contenttypeFulltext
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