CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number

In this paper, analytical and numerical methods are used to evaluate flow over a wedge at supersonic Mach numbers. Closed form solutions are obtained for the various semi-vertex angle of the wedge and the Mach numbers. Supersonic similarity parameter has been used to obtain the pressure distribution...

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Main Authors:	Khan, Sher Afghan, Aabid, Abdul, Saleel, Ahamad C.
Format:	Article
Language:	English English
Published:	International Journals of Engineering & Sciences 2019
Subjects:	QA76 Computer software
Online Access:	http://irep.iium.edu.my/71239/ http://irep.iium.edu.my/71239/ http://irep.iium.edu.my/71239/1/71239_CFD%20Simulation%20with%20Analytical%20and%20Theoretical.pdf http://irep.iium.edu.my/71239/7/71239_CFD%20simulation%20with%20analytical%20and%20theoretical_SCOPUS.pdf

id	iium-71239
recordtype	eprints
spelling	iium-712392019-08-30T09:08:10Z http://irep.iium.edu.my/71239/ CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number Khan, Sher Afghan Aabid, Abdul Saleel, Ahamad C. QA76 Computer software In this paper, analytical and numerical methods are used to evaluate flow over a wedge at supersonic Mach numbers. Closed form solutions are obtained for the various semi-vertex angle of the wedge and the Mach numbers. Supersonic similarity parameter has been used to obtain the pressure distribution over wedge at a different angle of attack with the attached shock wave case. Results are in good agreement with the theory. For the analysis a strip theory is used which are independent in the direction of the flow. To simulate the results, the finite element (FE) method has been used. The validation has been done using the second order shock-expansion theory and the analytical solution obtained by Ghosh’s unified supersonic/hypersonic theory. International Journals of Engineering & Sciences 2019-02-09 Article PeerReviewed application/pdf en http://irep.iium.edu.my/71239/1/71239_CFD%20Simulation%20with%20Analytical%20and%20Theoretical.pdf application/pdf en http://irep.iium.edu.my/71239/7/71239_CFD%20simulation%20with%20analytical%20and%20theoretical_SCOPUS.pdf Khan, Sher Afghan and Aabid, Abdul and Saleel, Ahamad C. (2019) CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number. International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS, 19 (1). pp. 170-177. ISSN 2227-2771 E-ISSN 2077-124X http://ijens.org/Vol_19_I_01/193101-4545-IJMME-IJENS.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	QA76 Computer software
spellingShingle	QA76 Computer software Khan, Sher Afghan Aabid, Abdul Saleel, Ahamad C. CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
description	In this paper, analytical and numerical methods are used to evaluate flow over a wedge at supersonic Mach numbers. Closed form solutions are obtained for the various semi-vertex angle of the wedge and the Mach numbers. Supersonic similarity parameter has been used to obtain the pressure distribution over wedge at a different angle of attack with the attached shock wave case. Results are in good agreement with the theory. For the analysis a strip theory is used which are independent in the direction of the flow. To simulate the results, the finite element (FE) method has been used. The validation has been done using the second order shock-expansion theory and the analytical solution obtained by Ghosh’s unified supersonic/hypersonic theory.
format	Article
author	Khan, Sher Afghan Aabid, Abdul Saleel, Ahamad C.
author_facet	Khan, Sher Afghan Aabid, Abdul Saleel, Ahamad C.
author_sort	Khan, Sher Afghan
title	CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
title_short	CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
title_full	CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
title_fullStr	CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
title_full_unstemmed	CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
title_sort	cfd simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic mach number
publisher	International Journals of Engineering & Sciences
publishDate	2019
url	http://irep.iium.edu.my/71239/ http://irep.iium.edu.my/71239/ http://irep.iium.edu.my/71239/1/71239_CFD%20Simulation%20with%20Analytical%20and%20Theoretical.pdf http://irep.iium.edu.my/71239/7/71239_CFD%20simulation%20with%20analytical%20and%20theoretical_SCOPUS.pdf
first_indexed	2023-09-18T21:41:07Z
last_indexed	2023-09-18T21:41:07Z
_version_	1777413147056930816

CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number

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