Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24

The primary goal of this study is to use CFD analysis to investigate the impact that a cavity has on the pressure at the base of a structure. In this analysis, we considered the NPR, the cavity aspect ratio, and the cavity position. In this case, the area ratio is 3.24, and the Mach number is 2.0. S...

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Main Authors: Anuar, Farhana Nur Danisyah Mohd Anuar, Ghasi Mahaboobali, Fharukh Ahmed, Khan, Ambareen, Akhtar, Mohammad Nishat, Khan, Sher Afghan
Format: Article
Language:English
English
Published: Semarak Ilmu Publishing 2024
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Online Access:http://irep.iium.edu.my/112466/2/112466_Effect%20of%20cavity%20geometry%20and%20location%20on%20base%20pressure.pdf
http://irep.iium.edu.my/112466/8/112466_Effect%20of%20cavity%20geometry%20and%20location%20on%20base%20pressure_SCOPUS.pdf
http://irep.iium.edu.my/112466/
https://semarakilmu.com.my/journals/index.php/appl_mech/article/view/3840/4924le/view/3840/4924
https://doi.org/10.37934/aram.117.1.121
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Institution: Universiti Islam Antarabangsa Malaysia
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spelling my.iium.irep.1124662024-09-21T06:17:29Z http://irep.iium.edu.my/112466/ Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24 Anuar, Farhana Nur Danisyah Mohd Anuar Ghasi Mahaboobali, Fharukh Ahmed Khan, Ambareen Akhtar, Mohammad Nishat Khan, Sher Afghan TL500 Aeronautics The primary goal of this study is to use CFD analysis to investigate the impact that a cavity has on the pressure at the base of a structure. In this analysis, we considered the NPR, the cavity aspect ratio, and the cavity position. In this case, the area ratio is 3.24, and the Mach number is 2.0. Simulations were run with L/D ratios between 1 and 6 and NPRs of 3, 5, 7.8, 9, and 12. The 2-dimensional model was developed using ANSYS Fluent's Design Modeler. The nozzle is operating at Mach 2.0. Base pressure and wall pressure in the duct were the primary research foci. The C-D nozzle was created for this research. ANSYS Fluent was used to verify the CFD findings. When the nozzles are under-expanded and the cavity is at 0.5D, passive control as a cavity is shown to be effective. It appears that 1D is the bare minimum for duct length. Because the shear layer gets reattached to the duct wall at 1D and the boundary layer grows after reattachment, passive control is not observed in the flow process, regardless of whether the cavity is located at 1D, 1.5D, 2D, or 3D. An oscillating base pressure is seen at shorter duct lengths. This phenomenon does not occur at longer duct lengths. Whether or not there are cavities in the duct, the flow field is the same. Semarak Ilmu Publishing 2024-05-30 Article PeerReviewed application/pdf en http://irep.iium.edu.my/112466/2/112466_Effect%20of%20cavity%20geometry%20and%20location%20on%20base%20pressure.pdf application/pdf en http://irep.iium.edu.my/112466/8/112466_Effect%20of%20cavity%20geometry%20and%20location%20on%20base%20pressure_SCOPUS.pdf Anuar, Farhana Nur Danisyah Mohd Anuar and Ghasi Mahaboobali, Fharukh Ahmed and Khan, Ambareen and Akhtar, Mohammad Nishat and Khan, Sher Afghan (2024) Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24. Journal of Advanced Research in Applied Mechanics, 117 (1). pp. 1-21. E-ISSN 2289-7895 https://semarakilmu.com.my/journals/index.php/appl_mech/article/view/3840/4924le/view/3840/4924 https://doi.org/10.37934/aram.117.1.121
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 TL500 Aeronautics
spellingShingle TL500 Aeronautics
Anuar, Farhana Nur Danisyah Mohd Anuar
Ghasi Mahaboobali, Fharukh Ahmed
Khan, Ambareen
Akhtar, Mohammad Nishat
Khan, Sher Afghan
Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
description The primary goal of this study is to use CFD analysis to investigate the impact that a cavity has on the pressure at the base of a structure. In this analysis, we considered the NPR, the cavity aspect ratio, and the cavity position. In this case, the area ratio is 3.24, and the Mach number is 2.0. Simulations were run with L/D ratios between 1 and 6 and NPRs of 3, 5, 7.8, 9, and 12. The 2-dimensional model was developed using ANSYS Fluent's Design Modeler. The nozzle is operating at Mach 2.0. Base pressure and wall pressure in the duct were the primary research foci. The C-D nozzle was created for this research. ANSYS Fluent was used to verify the CFD findings. When the nozzles are under-expanded and the cavity is at 0.5D, passive control as a cavity is shown to be effective. It appears that 1D is the bare minimum for duct length. Because the shear layer gets reattached to the duct wall at 1D and the boundary layer grows after reattachment, passive control is not observed in the flow process, regardless of whether the cavity is located at 1D, 1.5D, 2D, or 3D. An oscillating base pressure is seen at shorter duct lengths. This phenomenon does not occur at longer duct lengths. Whether or not there are cavities in the duct, the flow field is the same.
format Article
author Anuar, Farhana Nur Danisyah Mohd Anuar
Ghasi Mahaboobali, Fharukh Ahmed
Khan, Ambareen
Akhtar, Mohammad Nishat
Khan, Sher Afghan
author_facet Anuar, Farhana Nur Danisyah Mohd Anuar
Ghasi Mahaboobali, Fharukh Ahmed
Khan, Ambareen
Akhtar, Mohammad Nishat
Khan, Sher Afghan
author_sort Anuar, Farhana Nur Danisyah Mohd Anuar
title Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
title_short Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
title_full Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
title_fullStr Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
title_full_unstemmed Effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
title_sort effect of cavity geometry and location on base pressure in a suddenly expanded flow at mach 2.0 for area ratio 3.24
publisher Semarak Ilmu Publishing
publishDate 2024
url http://irep.iium.edu.my/112466/2/112466_Effect%20of%20cavity%20geometry%20and%20location%20on%20base%20pressure.pdf
http://irep.iium.edu.my/112466/8/112466_Effect%20of%20cavity%20geometry%20and%20location%20on%20base%20pressure_SCOPUS.pdf
http://irep.iium.edu.my/112466/
https://semarakilmu.com.my/journals/index.php/appl_mech/article/view/3840/4924le/view/3840/4924
https://doi.org/10.37934/aram.117.1.121
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