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...
Saved in:
Main Authors: | , , , , |
---|---|
Format: | Article |
Language: | English English |
Published: |
Semarak Ilmu Publishing
2024
|
Subjects: | |
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 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Universiti Islam Antarabangsa Malaysia |
Language: | English English |
id |
my.iium.irep.112466 |
---|---|
record_format |
dspace |
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 |
_version_ |
1811679606391963648 |