CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS

This paper presents numerical study was undertaken to identify the use of the micro-jets to regulate the pressure in the region from two-dimensional convergent-divergent (CD) Nozzle. At the exit of the divergent nozzle in the base region 1 mm of two micro-jets orifice diameter has been arranged at n...

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Main Authors: Khan, Ambareen, Abid, Abdul, Khan, Sher Afghan
Format: Article
Language:English
English
Published: Science Publishing Corporation 2018
Subjects:
Online Access:http://irep.iium.edu.my/66141/
http://irep.iium.edu.my/66141/
http://irep.iium.edu.my/66141/
http://irep.iium.edu.my/66141/1/66141_CFD%20analysis%20of%20convergent-divergent.pdf
http://irep.iium.edu.my/66141/7/66141_CFD%20analysis%20of%20convergent-divergent%20nozzle%20flow%20and%20base%20pressure%20control%20using%20micro-JETS_scopus.pdf
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spelling iium-661412019-01-08T08:12:12Z http://irep.iium.edu.my/66141/ CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS Khan, Ambareen Abid, Abdul Khan, Sher Afghan TL787 Astronautics This paper presents numerical study was undertaken to identify the use of the micro-jets to regulate the pressure in the region from two-dimensional convergent-divergent (CD) Nozzle. At the exit of the divergent nozzle in the base region 1 mm of two micro-jets orifice diameter has been arranged at ninety degrees at pcd 13 mm to control base pressure. The inertia level at the inlet to suddenly expanded duct was 1.87. The micro-jets are suddenly expanded into a two-dimensional planar area ratio of 3.24. The L/D of the duct was 1, 2, 4, 5, 6, 8 and 10. The total wall pressure distribution from inlet to the outlet too was recorded. The results indicate that the micro-jets can oblige as the effective regulators of the pressure in the base area. The duct wall pressure field is not negatively affected by the dynamic control. Nozzles were operated with the NPR in the range from 3 to 11. The results show that we can fix the flow parameter which will result in the maximum gain in the base pressure, velocity and temperature. The convergent-divergent nozzle geometry has been modeled and sim-ulated employing turbulence models: K-ε standard wall function turbulence model from the code was validated with the commercial com-putational fluid dynamics. Science Publishing Corporation 2018-08-24 Article PeerReviewed application/pdf en http://irep.iium.edu.my/66141/1/66141_CFD%20analysis%20of%20convergent-divergent.pdf application/pdf en http://irep.iium.edu.my/66141/7/66141_CFD%20analysis%20of%20convergent-divergent%20nozzle%20flow%20and%20base%20pressure%20control%20using%20micro-JETS_scopus.pdf Khan, Ambareen and Abid, Abdul and Khan, Sher Afghan (2018) CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS. International Journal of Engineering & Technology, 7 (3.29 (Special issue 29)). pp. 232-235. ISSN 2227-524X https://www.sciencepubco.com/index.php/ijet/article/view/18802/8601 10.14419/ijet.v7i3.29.18802
repository_type Digital Repository
institution_category Local University
institution International Islamic University Malaysia
building IIUM Repository
collection Online Access
language English
English
topic TL787 Astronautics
spellingShingle TL787 Astronautics
Khan, Ambareen
Abid, Abdul
Khan, Sher Afghan
CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
description This paper presents numerical study was undertaken to identify the use of the micro-jets to regulate the pressure in the region from two-dimensional convergent-divergent (CD) Nozzle. At the exit of the divergent nozzle in the base region 1 mm of two micro-jets orifice diameter has been arranged at ninety degrees at pcd 13 mm to control base pressure. The inertia level at the inlet to suddenly expanded duct was 1.87. The micro-jets are suddenly expanded into a two-dimensional planar area ratio of 3.24. The L/D of the duct was 1, 2, 4, 5, 6, 8 and 10. The total wall pressure distribution from inlet to the outlet too was recorded. The results indicate that the micro-jets can oblige as the effective regulators of the pressure in the base area. The duct wall pressure field is not negatively affected by the dynamic control. Nozzles were operated with the NPR in the range from 3 to 11. The results show that we can fix the flow parameter which will result in the maximum gain in the base pressure, velocity and temperature. The convergent-divergent nozzle geometry has been modeled and sim-ulated employing turbulence models: K-ε standard wall function turbulence model from the code was validated with the commercial com-putational fluid dynamics.
format Article
author Khan, Ambareen
Abid, Abdul
Khan, Sher Afghan
author_facet Khan, Ambareen
Abid, Abdul
Khan, Sher Afghan
author_sort Khan, Ambareen
title CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
title_short CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
title_full CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
title_fullStr CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
title_full_unstemmed CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS
title_sort cfd analysis of convergent-divergent nozzle flow and base pressure control using micro-jets
publisher Science Publishing Corporation
publishDate 2018
url http://irep.iium.edu.my/66141/
http://irep.iium.edu.my/66141/
http://irep.iium.edu.my/66141/
http://irep.iium.edu.my/66141/1/66141_CFD%20analysis%20of%20convergent-divergent.pdf
http://irep.iium.edu.my/66141/7/66141_CFD%20analysis%20of%20convergent-divergent%20nozzle%20flow%20and%20base%20pressure%20control%20using%20micro-JETS_scopus.pdf
first_indexed 2023-09-18T21:33:51Z
last_indexed 2023-09-18T21:33:51Z
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