Rankine-Hugoniot Relations for Lennard-Jones LiquidsSource: Journal of Fluids Engineering:;1994:;volume( 116 ):;issue: 003::page 625Author:Akira Satoh
DOI: 10.1115/1.2910323Publisher: 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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contributor author | Akira Satoh | |
date accessioned | 2017-05-08T23:44:34Z | |
date available | 2017-05-08T23:44:34Z | |
date copyright | September, 1994 | |
date issued | 1994 | |
identifier issn | 0098-2202 | |
identifier other | JFEGA4-27087#625_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/113810 | |
description 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. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Rankine-Hugoniot Relations for Lennard-Jones Liquids | |
type | Journal Paper | |
journal volume | 116 | |
journal issue | 3 | |
journal title | Journal of Fluids Engineering | |
identifier doi | 10.1115/1.2910323 | |
journal fristpage | 625 | |
journal lastpage | 630 | |
identifier eissn | 1528-901X | |
keywords | Pressure | |
keywords | Mach number | |
keywords | Temperature | |
keywords | Sound | |
keywords | Shock waves | |
keywords | Shock (Mechanics) | |
keywords | Engineering simulation | |
keywords | Equations AND Molecular dynamics simulation | |
tree | Journal of Fluids Engineering:;1994:;volume( 116 ):;issue: 003 | |
contenttype | Fulltext |