Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator
This paper presents a study on the influence of inlet radial angle in a multi-inlet cyclone separator using Eulerian-Lagrangian (EL) fluid dynamics approach. The investigation focuses on the behavior of air and solid particles within the cyclone. Air circulation was simulated at velocities ranging f...
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Elsevier
2023-09-01
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Series: | Alexandria Engineering Journal |
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Online Access: | http://www.sciencedirect.com/science/article/pii/S1110016823006476 |
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author | Ibrahim Ademola Fetuga Olabode Thomas Olakoyejo Sogo Mayokun Abolarin Adekunle O. Adelaja Samuel Olajide Ologunoba Omotayo Oluwatusin Oluwaseun Fetuata Olayinka Omowunmi Adewumi Udo David Robinson Antonio Marcos de Oliveira Siqueira |
author_facet | Ibrahim Ademola Fetuga Olabode Thomas Olakoyejo Sogo Mayokun Abolarin Adekunle O. Adelaja Samuel Olajide Ologunoba Omotayo Oluwatusin Oluwaseun Fetuata Olayinka Omowunmi Adewumi Udo David Robinson Antonio Marcos de Oliveira Siqueira |
author_sort | Ibrahim Ademola Fetuga |
collection | DOAJ |
description | This paper presents a study on the influence of inlet radial angle in a multi-inlet cyclone separator using Eulerian-Lagrangian (EL) fluid dynamics approach. The investigation focuses on the behavior of air and solid particles within the cyclone. Air circulation was simulated at velocities ranging from 2 to 6 m/s, with inlet radial angles of 15°, 32°, 45°, 61°, and 72°. To model the turbulent flow, the Reynolds stress model (RSM) and renormalization group k-model (RNG) were employed, while the particle trajectories were simulated using the discrete phase model (DPM) in ANSYS Fluent. The purpose of this study was to determine how the inlet radial angle impacts various parameters: collection efficiency, pressure drop, cut-off diameter, axial velocity, and tangential velocity. The numerical data obtained from the simulations were validated and found to be consistent with the existing literature. The results revealed interesting findings. In the case of an inlet velocity of 6 m/s, the highest pressure drop of 84.5 Pa was observed for the 15° inlet radial angle, while the lowest pressure drop of 77.42 Pa was observed for the 32° inlet radial angle. It was found that the collection efficiency varied according to the radial angle of the inlet, with values of 89.00%, 91.70%, 92.50%, 94.77%, and 94.83% for 32°, 45°, 15°, 72°, and 61°, respectively. Additionally, at an inlet velocity of 2 m/s and a radial angle of 72°, 61°, 15°, 45°, and 32°, the corresponding cut-off sizes were determined to be 1.17 μm, 1.19 μm, 1.25 μm, 1.33 μm, and 1.38 μm, respectively. At an inlet velocity of 6 m/s, the peak tangential velocities were found to be approximately 1.48, 1.44, 1.44, 1.39, and 1.34 times the inlet velocity for the 15°, 72°, 61°, 45°, and 32° radial angles, respectively, within the axial location range of z = 1.5D to z = 3.4D. The peak axial velocity values for the 32°, 72°, 45°, 15°, and 61° radial angles, were reported as 0.85, 0.89, 0.92, 0.94, and 0.96 times the inlet velocity respectively. |
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language | English |
last_indexed | 2024-03-12T13:19:07Z |
publishDate | 2023-09-01 |
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spelling | doaj.art-0fd970a889b74119886af1db118afb602023-08-26T04:42:58ZengElsevierAlexandria Engineering Journal1110-01682023-09-0178453468Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separatorIbrahim Ademola Fetuga0Olabode Thomas Olakoyejo1Sogo Mayokun Abolarin2Adekunle O. Adelaja3Samuel Olajide Ologunoba4Omotayo Oluwatusin5Oluwaseun Fetuata6Olayinka Omowunmi Adewumi7Udo David Robinson8Antonio Marcos de Oliveira Siqueira9Department of Mechanical Engineering, University of Lagos, Akoka, Lagos, NigeriaDepartment of Mechanical Engineering, University of Lagos, Akoka, Lagos, NigeriaDepartment Engineering Sciences, University of the Free State, Bloemfontein, South Africa; Corresponding author.Department of Mechanical Engineering, University of Lagos, Akoka, Lagos, NigeriaDepartment of Computer Engineering, Bell University of Technology, Ogun State, NigeriaDepartment of Mechanical Engineering, University of Lagos, Akoka, Lagos, NigeriaDepartment of Mechanical Engineering, Obafemi Awolowo University, NigeriaDepartment of Mechanical Engineering, University of Lagos, Akoka, Lagos, NigeriaDepartment of Chemical Engineering, Federal University of Technology Minna, NigeriaChemical Engineering Graduate Program, Department of Chemistry, Federal University of Viçosa, BrazilThis paper presents a study on the influence of inlet radial angle in a multi-inlet cyclone separator using Eulerian-Lagrangian (EL) fluid dynamics approach. The investigation focuses on the behavior of air and solid particles within the cyclone. Air circulation was simulated at velocities ranging from 2 to 6 m/s, with inlet radial angles of 15°, 32°, 45°, 61°, and 72°. To model the turbulent flow, the Reynolds stress model (RSM) and renormalization group k-model (RNG) were employed, while the particle trajectories were simulated using the discrete phase model (DPM) in ANSYS Fluent. The purpose of this study was to determine how the inlet radial angle impacts various parameters: collection efficiency, pressure drop, cut-off diameter, axial velocity, and tangential velocity. The numerical data obtained from the simulations were validated and found to be consistent with the existing literature. The results revealed interesting findings. In the case of an inlet velocity of 6 m/s, the highest pressure drop of 84.5 Pa was observed for the 15° inlet radial angle, while the lowest pressure drop of 77.42 Pa was observed for the 32° inlet radial angle. It was found that the collection efficiency varied according to the radial angle of the inlet, with values of 89.00%, 91.70%, 92.50%, 94.77%, and 94.83% for 32°, 45°, 15°, 72°, and 61°, respectively. Additionally, at an inlet velocity of 2 m/s and a radial angle of 72°, 61°, 15°, 45°, and 32°, the corresponding cut-off sizes were determined to be 1.17 μm, 1.19 μm, 1.25 μm, 1.33 μm, and 1.38 μm, respectively. At an inlet velocity of 6 m/s, the peak tangential velocities were found to be approximately 1.48, 1.44, 1.44, 1.39, and 1.34 times the inlet velocity for the 15°, 72°, 61°, 45°, and 32° radial angles, respectively, within the axial location range of z = 1.5D to z = 3.4D. The peak axial velocity values for the 32°, 72°, 45°, 15°, and 61° radial angles, were reported as 0.85, 0.89, 0.92, 0.94, and 0.96 times the inlet velocity respectively.http://www.sciencedirect.com/science/article/pii/S1110016823006476CFDRadial angleMulti-inlet CyclonePressure dropCollection efficiencyCut-off size |
spellingShingle | Ibrahim Ademola Fetuga Olabode Thomas Olakoyejo Sogo Mayokun Abolarin Adekunle O. Adelaja Samuel Olajide Ologunoba Omotayo Oluwatusin Oluwaseun Fetuata Olayinka Omowunmi Adewumi Udo David Robinson Antonio Marcos de Oliveira Siqueira Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator Alexandria Engineering Journal CFD Radial angle Multi-inlet Cyclone Pressure drop Collection efficiency Cut-off size |
title | Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator |
title_full | Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator |
title_fullStr | Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator |
title_full_unstemmed | Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator |
title_short | Eulerian–Lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi-inlet cyclone separator |
title_sort | eulerian lagrangian fluid dynamics study on the effects of inlet radial angle on the performance and flow pattern of multi inlet cyclone separator |
topic | CFD Radial angle Multi-inlet Cyclone Pressure drop Collection efficiency Cut-off size |
url | http://www.sciencedirect.com/science/article/pii/S1110016823006476 |
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