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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| Language: | English |
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| Online Access: | http://eprints.uthm.edu.my/8807/ http://eprints.uthm.edu.my/8807/1/J15832_e1e9339c6c07ebcf233c8c6a48d12c45.pdf |
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| author | Mohd Zaki Bahrom, Mohd Zaki Bahrom Bukhari Manshoor, Bukhari Manshoor Badrul Aisham Md Zain, Badrul Aisham Md Zain Izzuddin Zaman, Izzuddin Zaman Djamal Hissein Didane, Djamal Hissein Didane Reazul Haq Abdul Haq, Reazul Haq Abdul Haq Mohd Nizam Ibrahim, Mohd Nizam Ibrahim |
| author_facet | Mohd Zaki Bahrom, Mohd Zaki Bahrom Bukhari Manshoor, Bukhari Manshoor Badrul Aisham Md Zain, Badrul Aisham Md Zain Izzuddin Zaman, Izzuddin Zaman Djamal Hissein Didane, Djamal Hissein Didane Reazul Haq Abdul Haq, Reazul Haq Abdul Haq Mohd Nizam Ibrahim, Mohd Nizam Ibrahim |
| author_sort | Mohd Zaki Bahrom, Mohd Zaki Bahrom |
| building | UTHM Institutional Repository |
| collection | Online Access |
| 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. |
| first_indexed | 2025-11-15T20:27:13Z |
| format | Article |
| id | uthm-8807 |
| institution | Universiti Tun Hussein Onn Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T20:27:13Z |
| publisher | semarak ilmu |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | uthm-88072023-06-14T00:37:54Z http://eprints.uthm.edu.my/8807/ Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge Mohd Zaki Bahrom, Mohd Zaki Bahrom Bukhari Manshoor, Bukhari Manshoor Badrul Aisham Md Zain, Badrul Aisham Md Zain Izzuddin Zaman, Izzuddin Zaman Djamal Hissein Didane, Djamal Hissein Didane Reazul Haq Abdul Haq, Reazul Haq Abdul Haq Mohd Nizam Ibrahim, Mohd Nizam Ibrahim TL Motor vehicles. Aeronautics. Astronautics 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 Article PeerReviewed text en http://eprints.uthm.edu.my/8807/1/J15832_e1e9339c6c07ebcf233c8c6a48d12c45.pdf Mohd Zaki Bahrom, Mohd Zaki Bahrom and Bukhari Manshoor, Bukhari Manshoor and Badrul Aisham Md Zain, Badrul Aisham Md Zain and Izzuddin Zaman, Izzuddin Zaman and Djamal Hissein Didane, Djamal Hissein Didane and Reazul Haq Abdul Haq, Reazul Haq Abdul Haq and Mohd Nizam Ibrahim, Mohd Nizam Ibrahim 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 |
| spellingShingle | TL Motor vehicles. Aeronautics. Astronautics Mohd Zaki Bahrom, Mohd Zaki Bahrom Bukhari Manshoor, Bukhari Manshoor Badrul Aisham Md Zain, Badrul Aisham Md Zain Izzuddin Zaman, Izzuddin Zaman Djamal Hissein Didane, Djamal Hissein Didane Reazul Haq Abdul Haq, Reazul Haq Abdul Haq Mohd Nizam Ibrahim, Mohd Nizam Ibrahim Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge |
| title | 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_short | Thrust Force for Drone Propeller with Normal and Serrated Trailing Edge |
| title_sort | thrust force for drone propeller with normal and serrated trailing edge |
| topic | TL Motor vehicles. Aeronautics. Astronautics |
| url | http://eprints.uthm.edu.my/8807/ http://eprints.uthm.edu.my/8807/ http://eprints.uthm.edu.my/8807/1/J15832_e1e9339c6c07ebcf233c8c6a48d12c45.pdf |