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Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge

The drone becomes more recognized in the civilian sector; the drone's popularity becomes increases as time goes by. Nevertheless, despite the excitement of flying drones, several types of issues occur caused by the drone. In some circumstances, the aeroacoustics noise is a big concern, and quie...

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Main Authors: Bahrom, Mohd Zaki, Manshoor, Bukhari, Md Zain, Badrul Aisham, Zaman, Izzuddin, Djamal Hissein Didane, Djamal Hissein Didane, Abdul Haq, Reazul Haq, Ibrahim, Mohd Nizam
Format: Article
Language:English
Published: semarak ilmu 2023
Subjects:
T Technology (General)
Online Access:http://eprints.uthm.edu.my/9345/1/J15832_e1e9339c6c07ebcf233c8c6a48d12c45.pdf
http://eprints.uthm.edu.my/9345/
https://doi.org/10.37934/arfmts.101.1.160173
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spelling my.uthm.eprints.93452023-07-17T07:51:05Z http://eprints.uthm.edu.my/9345/ Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge Bahrom, Mohd Zaki Manshoor, Bukhari Md Zain, Badrul Aisham Zaman, Izzuddin Djamal Hissein Didane, Djamal Hissein Didane Abdul Haq, Reazul Haq Ibrahim, Mohd Nizam T Technology (General) The drone becomes more recognized in the civilian sector; the drone's popularity becomes increases as time goes by. Nevertheless, despite the excitement of flying drones, several types of issues occur caused by the drone. In some circumstances, the aeroacoustics noise is a big concern, and quiet drone propellers would be more environmentally friendly to the surrounding area. Moreover, the noise from the drone can be a nuisance for the surrounding population and animals. Therefore, a solution needs to be proposed to reduce the sound level produced by the drone so that drone can be piloted in a surrounding area without breaking any noise level limit set by the government. Hence, the propeller's serrated trailing edge type is the proposed solution to this problem. The serrated trailing edge propeller can reduce several drone noise decibels based on past research. Thus, an investigation is conducted to study the thrust force between the normal propeller and the serrated propeller. The aerodynamic performance of the serrated propeller is analysed using computational fluid dynamic simulation and compared to that of the normal propeller. Ansys Fluent 2021 is used to solve the dependable RNG k-epsilon turbulence model. The thrust force, thrust coefficient, and lift coefficient operating on both propellers were all simulated. The results obtained by the transient approach for propellers have been validated by earlier experimental studies. semarak ilmu 2023 Article PeerReviewed text en http://eprints.uthm.edu.my/9345/1/J15832_e1e9339c6c07ebcf233c8c6a48d12c45.pdf Bahrom, Mohd Zaki and Manshoor, Bukhari and Md Zain, Badrul Aisham and Zaman, Izzuddin and Djamal Hissein Didane, Djamal Hissein Didane and Abdul Haq, Reazul Haq and Ibrahim, Mohd Nizam (2023) Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 101 (1). pp. 160-173. ISSN 2289-7879 https://doi.org/10.37934/arfmts.101.1.160173
institution Universiti Tun Hussein Onn Malaysia
building UTHM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tun Hussein Onn Malaysia
content_source UTHM Institutional Repository
url_provider http://eprints.uthm.edu.my/
language English
topic T Technology (General)
spellingShingle T Technology (General)
Bahrom, Mohd Zaki
Manshoor, Bukhari
Md Zain, Badrul Aisham
Zaman, Izzuddin
Djamal Hissein Didane, Djamal Hissein Didane
Abdul Haq, Reazul Haq
Ibrahim, Mohd Nizam
Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
description The drone becomes more recognized in the civilian sector; the drone's popularity becomes increases as time goes by. Nevertheless, despite the excitement of flying drones, several types of issues occur caused by the drone. In some circumstances, the aeroacoustics noise is a big concern, and quiet drone propellers would be more environmentally friendly to the surrounding area. Moreover, the noise from the drone can be a nuisance for the surrounding population and animals. Therefore, a solution needs to be proposed to reduce the sound level produced by the drone so that drone can be piloted in a surrounding area without breaking any noise level limit set by the government. Hence, the propeller's serrated trailing edge type is the proposed solution to this problem. The serrated trailing edge propeller can reduce several drone noise decibels based on past research. Thus, an investigation is conducted to study the thrust force between the normal propeller and the serrated propeller. The aerodynamic performance of the serrated propeller is analysed using computational fluid dynamic simulation and compared to that of the normal propeller. Ansys Fluent 2021 is used to solve the dependable RNG k-epsilon turbulence model. The thrust force, thrust coefficient, and lift coefficient operating on both propellers were all simulated. The results obtained by the transient approach for propellers have been validated by earlier experimental studies.
format Article
author Bahrom, Mohd Zaki
Manshoor, Bukhari
Md Zain, Badrul Aisham
Zaman, Izzuddin
Djamal Hissein Didane, Djamal Hissein Didane
Abdul Haq, Reazul Haq
Ibrahim, Mohd Nizam
author_facet Bahrom, Mohd Zaki
Manshoor, Bukhari
Md Zain, Badrul Aisham
Zaman, Izzuddin
Djamal Hissein Didane, Djamal Hissein Didane
Abdul Haq, Reazul Haq
Ibrahim, Mohd Nizam
author_sort Bahrom, Mohd Zaki
title Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
title_short Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
title_full Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
title_fullStr Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
title_full_unstemmed Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge
title_sort thrust force for drone propeller with normal and serrated trailing edge
publisher semarak ilmu
publishDate 2023
url http://eprints.uthm.edu.my/9345/1/J15832_e1e9339c6c07ebcf233c8c6a48d12c45.pdf
http://eprints.uthm.edu.my/9345/
https://doi.org/10.37934/arfmts.101.1.160173
_version_ 1772813831490240512
score 13.211869

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