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...

Full description

Bibliographic Details
Main Authors: Astha Chauhan, Rajan Arora
Format: Article
Language:English
Published: International Journal of Mathematical, Engineering and Management Sciences 2019-10-01
Series:International Journal of Mathematical, Engineering and Management Sciences
Subjects:
Online Access:https://www.ijmems.in/assets//87-IJMEMS-FD-02-Vol.%204,%20No.%205,%201094%E2%80%931107,%202019.pdf
id doaj-6f04088ed8894efeb5c386f9c16539da
record_format Article
spelling 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