Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas
Self-similar solutions of the system of non-linear partial differential equations are obtained using the Lie group of invariance technique. The system of equations governs the one dimensional and unsteady motion for the isothermal flow of an ideal gas. The medium has been taken the uniform. From the...
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doaj-6f04088ed8894efeb5c386f9c16539da2020-11-25T02:45:09ZengInternational Journal of Mathematical, Engineering and Management SciencesInternational Journal of Mathematical, Engineering and Management Sciences2455-77492455-77492019-10-01451094110710.33889/IJMEMS.2019.4.5-087Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal GasAstha Chauhan0Rajan Arora1Department of Applied Science and Engineering, Indian Institute of Technology Roorkee, Roorkee, Uttarakhand, IndiaDepartment of Applied Science and Engineering, Indian Institute of Technology Roorkee, Roorkee, Uttarakhand, IndiaSelf-similar solutions of the system of non-linear partial differential equations are obtained using the Lie group of invariance technique. The system of equations governs the one dimensional and unsteady motion for the isothermal flow of an ideal gas. The medium has been taken the uniform. From the expressions of infinitesimal generators involving arbitrary constants, different cases arise as per the choice of the arbitrary constants. In this paper, the case of a collapse of an implosion of a cylindrical shock wave is shown in detail along with the comparison between the similarity exponent obtained by Guderley's method and by Crammer's rule. Also, the effects of the adiabatic index and the ambient density exponent on the flow variables are illustrated through the figures. The flow variables are computed behind the leading shock and are shown graphically. https://www.ijmems.in/assets//87-IJMEMS-FD-02-Vol.%204,%20No.%205,%201094%E2%80%931107,%202019.pdfLie groupShock wavesRankine-Hugoniot conditionsSimilarity solutionsIdeal gas |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Astha Chauhan Rajan Arora |
spellingShingle |
Astha Chauhan Rajan Arora Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas International Journal of Mathematical, Engineering and Management Sciences Lie group Shock waves Rankine-Hugoniot conditions Similarity solutions Ideal gas |
author_facet |
Astha Chauhan Rajan Arora |
author_sort |
Astha Chauhan |
title |
Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas |
title_short |
Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas |
title_full |
Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas |
title_fullStr |
Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas |
title_full_unstemmed |
Similarity Solutions of Strong Shock Waves for Isothermal Flow in an Ideal Gas |
title_sort |
similarity solutions of strong shock waves for isothermal flow in an ideal gas |
publisher |
International Journal of Mathematical, Engineering and Management Sciences |
series |
International Journal of Mathematical, Engineering and Management Sciences |
issn |
2455-7749 2455-7749 |
publishDate |
2019-10-01 |
description |
Self-similar solutions of the system of non-linear partial differential equations are obtained using the Lie group of invariance technique. The system of equations governs the one dimensional and unsteady motion for the isothermal flow of an ideal gas. The medium has been taken the uniform. From the expressions of infinitesimal generators involving arbitrary constants, different cases arise as per the choice of the arbitrary constants. In this paper, the case of a collapse of an implosion of a cylindrical shock wave is shown in detail along with the comparison between the similarity exponent obtained by Guderley's method and by Crammer's rule. Also, the effects of the adiabatic index and the ambient density exponent on the flow variables are illustrated through the figures. The flow variables are computed behind the leading shock and are shown graphically. |
topic |
Lie group Shock waves Rankine-Hugoniot conditions Similarity solutions Ideal gas |
url |
https://www.ijmems.in/assets//87-IJMEMS-FD-02-Vol.%204,%20No.%205,%201094%E2%80%931107,%202019.pdf |
work_keys_str_mv |
AT asthachauhan similaritysolutionsofstrongshockwavesforisothermalflowinanidealgas AT rajanarora similaritysolutionsofstrongshockwavesforisothermalflowinanidealgas |
_version_ |
1724763909156503552 |