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    Study on Expansion Process and Interaction of High Speed Twin Combustion-Gas Jets in Liquid

    Source: Journal of Applied Mechanics:;2010:;volume( 077 ):;issue: 005::page 51404
    Author:
    Yonggang Yu
    ,
    Shanheng Yan
    ,
    Na Zhao
    ,
    Xin Lu
    ,
    Yanhuang Zhou
    DOI: 10.1115/1.4001288
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The multilevel stepped-wall and rectangular observation chambers are designed to study the multipoint ignition process and the combustion stability control mechanism of the bulk-loaded liquid propellant gun. The expansion process and interaction of high-speed twin combustion-gas jets in liquid are studied by means of a high-speed digital camera system. The influence of the nozzle diameter, dual-orifice interval, jet pressure, and chamber structure on the jet expansion shape is discussed. The results indicate that a larger ratio of diameter-to-length can suppress the jet instability in stepped-wall chambers. Higher axial expansion velocity is found under the larger injection pressure, which it increases the instability of jet expansion process. Compared with a rectangular chamber, the axial expansion velocity is smaller, and the radial expansion velocity is larger in stepped-wall chambers under the same conditions. The theoretical studies of interaction of the gas jet with liquid were developed based on the experiment. Two-dimensional unsteady models are used to get the pressure, density, and velocity contours. The numerical simulation results coincide well with the experiment.
    keyword(s): Pressure , Jets , Nozzles , Computer simulation AND Combustion gases ,
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      Study on Expansion Process and Interaction of High Speed Twin Combustion-Gas Jets in Liquid

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    http://yetl.yabesh.ir/yetl1/handle/yetl/142370
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    contributor authorYonggang Yu
    contributor authorShanheng Yan
    contributor authorNa Zhao
    contributor authorXin Lu
    contributor authorYanhuang Zhou
    date accessioned2017-05-09T00:36:09Z
    date available2017-05-09T00:36:09Z
    date copyrightSeptember, 2010
    date issued2010
    identifier issn0021-8936
    identifier otherJAMCAV-26794#051404_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142370
    description abstractThe multilevel stepped-wall and rectangular observation chambers are designed to study the multipoint ignition process and the combustion stability control mechanism of the bulk-loaded liquid propellant gun. The expansion process and interaction of high-speed twin combustion-gas jets in liquid are studied by means of a high-speed digital camera system. The influence of the nozzle diameter, dual-orifice interval, jet pressure, and chamber structure on the jet expansion shape is discussed. The results indicate that a larger ratio of diameter-to-length can suppress the jet instability in stepped-wall chambers. Higher axial expansion velocity is found under the larger injection pressure, which it increases the instability of jet expansion process. Compared with a rectangular chamber, the axial expansion velocity is smaller, and the radial expansion velocity is larger in stepped-wall chambers under the same conditions. The theoretical studies of interaction of the gas jet with liquid were developed based on the experiment. Two-dimensional unsteady models are used to get the pressure, density, and velocity contours. The numerical simulation results coincide well with the experiment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStudy on Expansion Process and Interaction of High Speed Twin Combustion-Gas Jets in Liquid
    typeJournal Paper
    journal volume77
    journal issue5
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.4001288
    journal fristpage51404
    identifier eissn1528-9036
    keywordsPressure
    keywordsJets
    keywordsNozzles
    keywordsComputer simulation AND Combustion gases
    treeJournal of Applied Mechanics:;2010:;volume( 077 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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