Effect of ribs in a suddenly expanded flow at sonic Mach number

This study aims to assess the influence of a rib on the base pressure and the flow development in an abruptly expanded duct at sonic Mach number. Initially, the simulations were done to validate the experimental results, keeping all the parameters the same. Accordingly, a duct-of-area ratio of 6.25...

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Main Authors: Khan, Ambareen, Khan, Sher Afghan, Raja, Vijayanandh, Aabid, Abdul, Baig, Muneer
Format: Article
Language:English
English
Published: Cell Press 2024
Subjects:
Online Access:http://irep.iium.edu.my/112094/2/112094_Effect%20of%20ribs%20in%20a%20suddenly%20expanded%20flow.pdf
http://irep.iium.edu.my/112094/3/112094_Effect%20of%20ribs%20in%20a%20suddenly%20expanded%20flow_Scopus.pdf
http://irep.iium.edu.my/112094/
https://www.cell.com/heliyon/fulltext/S2405-8440(24)06344-8
https://doi.org/10.1016/j.heliyon.2024.e30313
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spelling my.iium.irep.1120942024-05-07T01:38:43Z http://irep.iium.edu.my/112094/ Effect of ribs in a suddenly expanded flow at sonic Mach number Khan, Ambareen Khan, Sher Afghan Raja, Vijayanandh Aabid, Abdul Baig, Muneer TL780 Rockets This study aims to assess the influence of a rib on the base pressure and the flow development in an abruptly expanded duct at sonic Mach number. Initially, the simulations were done to validate the experimental results, keeping all the parameters the same. Accordingly, a duct-of-area ratio of 6.25 was considered for validation. Five ribs of aspect ratios 3:1, 3:2, and 3:3 were used as a first step, and simulations were performed for the same nozzle pressure ratios. Results indicate that for an area ratio of 6.25, there is a continuous decrease in the base pressure despite the nozzles being highly under-expanded. The lower aspect ratio of the rib tends to reduce the base pressure, whereas a higher aspect ratio effectively increases the base pressure for an area ratio of 6.25. Later simulations considered a single rib instead of five ribs, varying the rib’s heights from 1 mm to 5 mm. Results show that the base pressure increases considerably when rib heights are 4 mm and 5 mm. The influence of ribs at two duct diameters (25 mm and 18 mm) is studied to assess the impact of a decrease in the area ratio and, hence, a decrease in the relief available to the flow. Results of duct 18 mm show that passive control becomes very effective when a rib of 3 mm height is located at a 3D position. The differences in the base pressure, velocity, and pressure field for each case are explored. The simulation results indicate that the rib breaks the primary vortex at the base and forms multiple vortices. Turbulent kinetic energy increases in the presence of ribs more than without a rib. Cell Press 2024-04-26 Article PeerReviewed application/pdf en http://irep.iium.edu.my/112094/2/112094_Effect%20of%20ribs%20in%20a%20suddenly%20expanded%20flow.pdf application/pdf en http://irep.iium.edu.my/112094/3/112094_Effect%20of%20ribs%20in%20a%20suddenly%20expanded%20flow_Scopus.pdf Khan, Ambareen and Khan, Sher Afghan and Raja, Vijayanandh and Aabid, Abdul and Baig, Muneer (2024) Effect of ribs in a suddenly expanded flow at sonic Mach number. Heliyon, 10. pp. 1-17. ISSN 2405-8440 https://www.cell.com/heliyon/fulltext/S2405-8440(24)06344-8 https://doi.org/10.1016/j.heliyon.2024.e30313
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TL780 Rockets
spellingShingle TL780 Rockets
Khan, Ambareen
Khan, Sher Afghan
Raja, Vijayanandh
Aabid, Abdul
Baig, Muneer
Effect of ribs in a suddenly expanded flow at sonic Mach number
description This study aims to assess the influence of a rib on the base pressure and the flow development in an abruptly expanded duct at sonic Mach number. Initially, the simulations were done to validate the experimental results, keeping all the parameters the same. Accordingly, a duct-of-area ratio of 6.25 was considered for validation. Five ribs of aspect ratios 3:1, 3:2, and 3:3 were used as a first step, and simulations were performed for the same nozzle pressure ratios. Results indicate that for an area ratio of 6.25, there is a continuous decrease in the base pressure despite the nozzles being highly under-expanded. The lower aspect ratio of the rib tends to reduce the base pressure, whereas a higher aspect ratio effectively increases the base pressure for an area ratio of 6.25. Later simulations considered a single rib instead of five ribs, varying the rib’s heights from 1 mm to 5 mm. Results show that the base pressure increases considerably when rib heights are 4 mm and 5 mm. The influence of ribs at two duct diameters (25 mm and 18 mm) is studied to assess the impact of a decrease in the area ratio and, hence, a decrease in the relief available to the flow. Results of duct 18 mm show that passive control becomes very effective when a rib of 3 mm height is located at a 3D position. The differences in the base pressure, velocity, and pressure field for each case are explored. The simulation results indicate that the rib breaks the primary vortex at the base and forms multiple vortices. Turbulent kinetic energy increases in the presence of ribs more than without a rib.
format Article
author Khan, Ambareen
Khan, Sher Afghan
Raja, Vijayanandh
Aabid, Abdul
Baig, Muneer
author_facet Khan, Ambareen
Khan, Sher Afghan
Raja, Vijayanandh
Aabid, Abdul
Baig, Muneer
author_sort Khan, Ambareen
title Effect of ribs in a suddenly expanded flow at sonic Mach number
title_short Effect of ribs in a suddenly expanded flow at sonic Mach number
title_full Effect of ribs in a suddenly expanded flow at sonic Mach number
title_fullStr Effect of ribs in a suddenly expanded flow at sonic Mach number
title_full_unstemmed Effect of ribs in a suddenly expanded flow at sonic Mach number
title_sort effect of ribs in a suddenly expanded flow at sonic mach number
publisher Cell Press
publishDate 2024
url http://irep.iium.edu.my/112094/2/112094_Effect%20of%20ribs%20in%20a%20suddenly%20expanded%20flow.pdf
http://irep.iium.edu.my/112094/3/112094_Effect%20of%20ribs%20in%20a%20suddenly%20expanded%20flow_Scopus.pdf
http://irep.iium.edu.my/112094/
https://www.cell.com/heliyon/fulltext/S2405-8440(24)06344-8
https://doi.org/10.1016/j.heliyon.2024.e30313
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