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    Rankine-Hugoniot Relations for Lennard-Jones Liquids

    Source: Journal of Fluids Engineering:;1994:;volume( 116 ):;issue: 003::page 625
    Author:
    Akira Satoh
    DOI: 10.1115/1.2910323
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The purpose of the present study is to clarify the Rankine-Hugoniot relations for Lennard-Jones liquids. First, Monte Carlo simulations are conducted to evaluate the state quantities such as the pressures, the internal energies, and the sound velocities. These computed values are used to obtain the approximate expressions for the state quantities by the method of least squares. The Rankine-Hugoniot relations are then clarified numerically as a function of the shock Mach number by solving the basic equations together with those approximate expressions. For liquid shock waves, not only the pressure but also the temperature increases much larger than those for an ideal gas. The results obtained here enable us to conduct more efficient molecular dynamics simulations such as simulating shock fronts alone for the investigation of the internal structures of liquid shock waves.
    keyword(s): Pressure , Mach number , Temperature , Sound , Shock waves , Shock (Mechanics) , Engineering simulation , Equations AND Molecular dynamics simulation ,
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      Rankine-Hugoniot Relations for Lennard-Jones Liquids

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/113810
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    contributor authorAkira Satoh
    date accessioned2017-05-08T23:44:34Z
    date available2017-05-08T23:44:34Z
    date copyrightSeptember, 1994
    date issued1994
    identifier issn0098-2202
    identifier otherJFEGA4-27087#625_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113810
    description abstractThe purpose of the present study is to clarify the Rankine-Hugoniot relations for Lennard-Jones liquids. First, Monte Carlo simulations are conducted to evaluate the state quantities such as the pressures, the internal energies, and the sound velocities. These computed values are used to obtain the approximate expressions for the state quantities by the method of least squares. The Rankine-Hugoniot relations are then clarified numerically as a function of the shock Mach number by solving the basic equations together with those approximate expressions. For liquid shock waves, not only the pressure but also the temperature increases much larger than those for an ideal gas. The results obtained here enable us to conduct more efficient molecular dynamics simulations such as simulating shock fronts alone for the investigation of the internal structures of liquid shock waves.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleRankine-Hugoniot Relations for Lennard-Jones Liquids
    typeJournal Paper
    journal volume116
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.2910323
    journal fristpage625
    journal lastpage630
    identifier eissn1528-901X
    keywordsPressure
    keywordsMach number
    keywordsTemperature
    keywordsSound
    keywordsShock waves
    keywordsShock (Mechanics)
    keywordsEngineering simulation
    keywordsEquations AND Molecular dynamics simulation
    treeJournal of Fluids Engineering:;1994:;volume( 116 ):;issue: 003
    contenttypeFulltext
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