Numerical analysis of convergent-divergent nozzle using finite element method

In this paper, Finite element method (FEM) were used to simulate the different flow configuration. Convergent divergent (CD) nozzle was considered with extended divergent duct. 1 mm of micro jets orifice diameter were arranged at ninety degrees at PCD 13 mm to control base pressure in a suddenly exp...

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Main Authors:	G M, Fharukh Ahmed, Al-Robaian, Abdul Rehman A, Aabid, Abdul, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Transstellar Journal Publications and Research Consultancy Private Limited 2018
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/7/67481%20NUMERICAL%20ANALYSIS%20OF%20CONVERGENT-DIVERGENT%20NOZZLE.pdf http://irep.iium.edu.my/67481/13/67481_Numerical%20analysis%20of%20convergent-divergent%20nozzle%20using%20finite%20element%20method_scopus.pdf

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spelling	iium-674812019-01-04T02:38:21Z http://irep.iium.edu.my/67481/ Numerical analysis of convergent-divergent nozzle using finite element method G M, Fharukh Ahmed Al-Robaian, Abdul Rehman A Aabid, Abdul Khan, Sher Afghan TL500 Aeronautics In this paper, Finite element method (FEM) were used to simulate the different flow configuration. Convergent divergent (CD) nozzle was considered with extended divergent duct. 1 mm of micro jets orifice diameter were arranged at ninety degrees at PCD 13 mm to control base pressure in a suddenly expanded flow. The designed Mach number of CD nozzle is 1.87 and area ratio 3.24 was considered. The different L/D of the duct was used from 2 to 10. The nozzle pressure simulated for 3, 5, 7, 9 and 11. In this case. Two-dimensional planar model was designed using ANSYS fluent analysis. The total wall pressure distribution and Mach number from inlet to the outlet was observed. From the results, it is detected that the micro jets control the loss of pressure and decreases the drag at the suddenly expanded region. The results also show, we can fix the flow parameter which will result in the maximum gain in the base pressure and velocity. In present study, the CD nozzle designed and modelled using available ANSYS fluent database: K-ε standard wall function turbulence model has been used and validated with the commercial computational fluid dynamics (CFD) Transstellar Journal Publications and Research Consultancy Private Limited 2018-12 Article PeerReviewed application/pdf en http://irep.iium.edu.my/67481/7/67481%20NUMERICAL%20ANALYSIS%20OF%20CONVERGENT-DIVERGENT%20NOZZLE.pdf application/pdf en http://irep.iium.edu.my/67481/13/67481_Numerical%20analysis%20of%20convergent-divergent%20nozzle%20using%20finite%20element%20method_scopus.pdf G M, Fharukh Ahmed and Al-Robaian, Abdul Rehman A and Aabid, Abdul and Khan, Sher Afghan (2018) Numerical analysis of convergent-divergent nozzle using finite element method. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD), 8 (6). pp. 373-382. ISSN 2249-6890 E-ISSN 2249-8001 http://www.tjprc.org/publishpapers/2-67-1541583801-42.IJMPERDDEC201842.pdf 10.24247/ijmperddec201842
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics G M, Fharukh Ahmed Al-Robaian, Abdul Rehman A Aabid, Abdul Khan, Sher Afghan Numerical analysis of convergent-divergent nozzle using finite element method
description	In this paper, Finite element method (FEM) were used to simulate the different flow configuration. Convergent divergent (CD) nozzle was considered with extended divergent duct. 1 mm of micro jets orifice diameter were arranged at ninety degrees at PCD 13 mm to control base pressure in a suddenly expanded flow. The designed Mach number of CD nozzle is 1.87 and area ratio 3.24 was considered. The different L/D of the duct was used from 2 to 10. The nozzle pressure simulated for 3, 5, 7, 9 and 11. In this case. Two-dimensional planar model was designed using ANSYS fluent analysis. The total wall pressure distribution and Mach number from inlet to the outlet was observed. From the results, it is detected that the micro jets control the loss of pressure and decreases the drag at the suddenly expanded region. The results also show, we can fix the flow parameter which will result in the maximum gain in the base pressure and velocity. In present study, the CD nozzle designed and modelled using available ANSYS fluent database: K-ε standard wall function turbulence model has been used and validated with the commercial computational fluid dynamics (CFD)
format	Article
author	G M, Fharukh Ahmed Al-Robaian, Abdul Rehman A Aabid, Abdul Khan, Sher Afghan
author_facet	G M, Fharukh Ahmed Al-Robaian, Abdul Rehman A Aabid, Abdul Khan, Sher Afghan
author_sort	G M, Fharukh Ahmed
title	Numerical analysis of convergent-divergent nozzle using finite element method
title_short	Numerical analysis of convergent-divergent nozzle using finite element method
title_full	Numerical analysis of convergent-divergent nozzle using finite element method
title_fullStr	Numerical analysis of convergent-divergent nozzle using finite element method
title_full_unstemmed	Numerical analysis of convergent-divergent nozzle using finite element method
title_sort	numerical analysis of convergent-divergent nozzle using finite element method
publisher	Transstellar Journal Publications and Research Consultancy Private Limited
publishDate	2018
url	http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/ http://irep.iium.edu.my/67481/7/67481%20NUMERICAL%20ANALYSIS%20OF%20CONVERGENT-DIVERGENT%20NOZZLE.pdf http://irep.iium.edu.my/67481/13/67481_Numerical%20analysis%20of%20convergent-divergent%20nozzle%20using%20finite%20element%20method_scopus.pdf
first_indexed	2023-09-18T21:35:48Z
last_indexed	2023-09-18T21:35:48Z
_version_	1777412811579719680

Numerical analysis of convergent-divergent nozzle using finite element method

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