Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform

The high-altitude platform was built as an alternative approach to address the weakness of the terrestrial and satellite communication networks. It can be an aircraft or balloon positioned 20 to 50 km above the earth’s atmosphere. The use of the Magnus effect was not noticeable in the production of...

Full description

Saved in:
Bibliographic Details
Main Authors: Mohammad Ali, Hidayatullah, Mohd Rafie, Azmin Shakrine, Abdul Hamid, Mohd Faisal, Md Ali, Syaril Azrad
Format: Article
Language:English
Published: Universiti Putra Malaysia Press 2022
Online Access:http://psasir.upm.edu.my/id/eprint/100737/1/Comparative%20computational%20study%20of%20double%20rotating%20cylinder%20embedded.pdf
http://psasir.upm.edu.my/id/eprint/100737/
http://journals-jd.upm.edu.my/pjst/browse/regular-issue?article=JST-3309-2021
Tags: Add Tag
No Tags, Be the first to tag this record!
id my.upm.eprints.100737
record_format eprints
spelling my.upm.eprints.1007372023-09-11T08:03:19Z http://psasir.upm.edu.my/id/eprint/100737/ Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform Mohammad Ali, Hidayatullah Mohd Rafie, Azmin Shakrine Abdul Hamid, Mohd Faisal Md Ali, Syaril Azrad The high-altitude platform was built as an alternative approach to address the weakness of the terrestrial and satellite communication networks. It can be an aircraft or balloon positioned 20 to 50 km above the earth’s atmosphere. The use of the Magnus effect was not noticeable in the production of the high-altitude platform, while past research study has denoted its aerodynamic performance in generating greater lift and stall angle delay, which would be beneficial in creating such a flying device. This research delineates the proposed designs using the computational fluid dynamics approach utilizing ANSYS WORKBENCH 2019 software. The embedment of the rotating cylinder onto the design would best portray the use of the Magnus effect in generating higher lift coefficients with probable delay in stall angle. Hereby, the design of embedding rotating cylinder onto Selig S1223 aerofoil and the flat plate is proposed to test their aerodynamic performances for high altitude platform purposes. Here, Fluent fluid flow analysis was simulated for 500 RPM and 1000 RPM momentum injection with free stream velocities from 5 m/s to 30 m/s for different angles of attack of 0 to 20 degrees. The analysis has resulted in a greater impact on its lift coefficient and stall angle delay of about 39% and 53% enhancement for modified aerofoil while showing 128% and 204% betterment for modified flat plate than their respective unmodified model. Therefore, it is perceived that the CyFlaP has better stability yet is simplistic in a design suitable for HAP application. Universiti Putra Malaysia Press 2022-09-23 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/100737/1/Comparative%20computational%20study%20of%20double%20rotating%20cylinder%20embedded.pdf Mohammad Ali, Hidayatullah and Mohd Rafie, Azmin Shakrine and Abdul Hamid, Mohd Faisal and Md Ali, Syaril Azrad (2022) Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform. UPM Press, 30 (4). art. no. 26. 2767 - 2788. ISSN 0128-7680; ESSN: 2231-8526 http://journals-jd.upm.edu.my/pjst/browse/regular-issue?article=JST-3309-2021 10.47836/pjst.30.4.26
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
description The high-altitude platform was built as an alternative approach to address the weakness of the terrestrial and satellite communication networks. It can be an aircraft or balloon positioned 20 to 50 km above the earth’s atmosphere. The use of the Magnus effect was not noticeable in the production of the high-altitude platform, while past research study has denoted its aerodynamic performance in generating greater lift and stall angle delay, which would be beneficial in creating such a flying device. This research delineates the proposed designs using the computational fluid dynamics approach utilizing ANSYS WORKBENCH 2019 software. The embedment of the rotating cylinder onto the design would best portray the use of the Magnus effect in generating higher lift coefficients with probable delay in stall angle. Hereby, the design of embedding rotating cylinder onto Selig S1223 aerofoil and the flat plate is proposed to test their aerodynamic performances for high altitude platform purposes. Here, Fluent fluid flow analysis was simulated for 500 RPM and 1000 RPM momentum injection with free stream velocities from 5 m/s to 30 m/s for different angles of attack of 0 to 20 degrees. The analysis has resulted in a greater impact on its lift coefficient and stall angle delay of about 39% and 53% enhancement for modified aerofoil while showing 128% and 204% betterment for modified flat plate than their respective unmodified model. Therefore, it is perceived that the CyFlaP has better stability yet is simplistic in a design suitable for HAP application.
format Article
author Mohammad Ali, Hidayatullah
Mohd Rafie, Azmin Shakrine
Abdul Hamid, Mohd Faisal
Md Ali, Syaril Azrad
spellingShingle Mohammad Ali, Hidayatullah
Mohd Rafie, Azmin Shakrine
Abdul Hamid, Mohd Faisal
Md Ali, Syaril Azrad
Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform
author_facet Mohammad Ali, Hidayatullah
Mohd Rafie, Azmin Shakrine
Abdul Hamid, Mohd Faisal
Md Ali, Syaril Azrad
author_sort Mohammad Ali, Hidayatullah
title Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform
title_short Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform
title_full Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform
title_fullStr Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform
title_full_unstemmed Comparative computational study of double rotating cylinder embedded on Selig S1223 aerofoil and flat plate for high altitude platform
title_sort comparative computational study of double rotating cylinder embedded on selig s1223 aerofoil and flat plate for high altitude platform
publisher Universiti Putra Malaysia Press
publishDate 2022
url http://psasir.upm.edu.my/id/eprint/100737/1/Comparative%20computational%20study%20of%20double%20rotating%20cylinder%20embedded.pdf
http://psasir.upm.edu.my/id/eprint/100737/
http://journals-jd.upm.edu.my/pjst/browse/regular-issue?article=JST-3309-2021
_version_ 1778163736982323200
score 13.211869