Molecular Dynamics Simulations on Internal Structures of Normal Shock Waves in Lennard-Jones LiquidsSource: Journal of Fluids Engineering:;1995:;volume( 117 ):;issue: 001::page 97Author:Akira Satoh
DOI: 10.1115/1.2816836Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The present paper describes a highly efficient method for simulating the generation of shock waves in liquids by using the periodic-shell boundary condition, which is an outer boundary condition for molecular dynamics simulations. This method is used to simulate normal shock waves in Lennard-Jones liquids, clarifying the internal structures of shock fronts and the dependence of shock thicknesses on the shock Mach number. The present method significantly decreases computation times because it enables us to simulate only the shock fronts. Some of the main results derived by these simulations of molecular dynamics are that an overshoot in the profile of longitudinal temperature arises in liquid shock waves as well as in gas shock waves, that the thickness of shock front decreases with increasing Mach number, and that this thickness is about two times the diameter of molecules when the Mach number is 4.
keyword(s): Shock waves , Molecular dynamics simulation , Mach number , Shock (Mechanics) , Boundary-value problems , Thickness , Computation , Shells , Engineering simulation , Temperature AND Molecular dynamics ,
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contributor author | Akira Satoh | |
date accessioned | 2017-05-08T23:47:37Z | |
date available | 2017-05-08T23:47:37Z | |
date copyright | March, 1995 | |
date issued | 1995 | |
identifier issn | 0098-2202 | |
identifier other | JFEGA4-27093#97_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/115549 | |
description abstract | The present paper describes a highly efficient method for simulating the generation of shock waves in liquids by using the periodic-shell boundary condition, which is an outer boundary condition for molecular dynamics simulations. This method is used to simulate normal shock waves in Lennard-Jones liquids, clarifying the internal structures of shock fronts and the dependence of shock thicknesses on the shock Mach number. The present method significantly decreases computation times because it enables us to simulate only the shock fronts. Some of the main results derived by these simulations of molecular dynamics are that an overshoot in the profile of longitudinal temperature arises in liquid shock waves as well as in gas shock waves, that the thickness of shock front decreases with increasing Mach number, and that this thickness is about two times the diameter of molecules when the Mach number is 4. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Molecular Dynamics Simulations on Internal Structures of Normal Shock Waves in Lennard-Jones Liquids | |
type | Journal Paper | |
journal volume | 117 | |
journal issue | 1 | |
journal title | Journal of Fluids Engineering | |
identifier doi | 10.1115/1.2816836 | |
journal fristpage | 97 | |
journal lastpage | 103 | |
identifier eissn | 1528-901X | |
keywords | Shock waves | |
keywords | Molecular dynamics simulation | |
keywords | Mach number | |
keywords | Shock (Mechanics) | |
keywords | Boundary-value problems | |
keywords | Thickness | |
keywords | Computation | |
keywords | Shells | |
keywords | Engineering simulation | |
keywords | Temperature AND Molecular dynamics | |
tree | Journal of Fluids Engineering:;1995:;volume( 117 ):;issue: 001 | |
contenttype | Fulltext |