Performance estimation of Twin Propeller in Unmanned Aerial Vehicle
The article deals with the experimental investigation of the thrust performance of a twin propeller used in a typical Unmanned Aerial Vehicle. The propeller is fabricated and tested using low speed subsonic wind tunnel to study the performance characteristics. The results obtained show better perfor...
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Format: | Article |
Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2020-06-01
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Series: | INCAS Bulletin |
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Online Access: | https://bulletin.incas.ro/files/prasad__vol_12_iss_2.pdf |
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author | G. PRASAD |
author_facet | G. PRASAD |
author_sort | G. PRASAD |
collection | DOAJ |
description | The article deals with the experimental investigation of the thrust performance of a twin propeller used in a typical Unmanned Aerial Vehicle. The propeller is fabricated and tested using low speed subsonic wind tunnel to study the performance characteristics. The results obtained show better performance compared to conventional propellers. The presence of twin propeller has increased the stall characteristics at low Reynolds number. The results indicate a substantial increase in thrust generation of up to 25 percent. The payload carrying capacity and handling quality will improve using this technique during pandemic to spray disinfectants. The results obtained provide an alternate design for future propellers applications. Further it is observed that the endurance of the Unmanned Aerial Vehicle can be reduced considerably, by few alternate solution. |
first_indexed | 2024-12-18T04:55:42Z |
format | Article |
id | doaj.art-79519217b9ad4328a6be0ab6e03193d5 |
institution | Directory Open Access Journal |
issn | 2066-8201 2247-4528 |
language | English |
last_indexed | 2024-12-18T04:55:42Z |
publishDate | 2020-06-01 |
publisher | National Institute for Aerospace Research “Elie Carafoli” - INCAS |
record_format | Article |
series | INCAS Bulletin |
spelling | doaj.art-79519217b9ad4328a6be0ab6e03193d52022-12-21T21:20:17ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282020-06-0112214314910.13111/2066-8201.2020.12.2.12Performance estimation of Twin Propeller in Unmanned Aerial VehicleG. PRASAD0Satyam College of Engineering and Technology, Kanyakumari, Tamilnadu, India, prasadjithu@gmail.comThe article deals with the experimental investigation of the thrust performance of a twin propeller used in a typical Unmanned Aerial Vehicle. The propeller is fabricated and tested using low speed subsonic wind tunnel to study the performance characteristics. The results obtained show better performance compared to conventional propellers. The presence of twin propeller has increased the stall characteristics at low Reynolds number. The results indicate a substantial increase in thrust generation of up to 25 percent. The payload carrying capacity and handling quality will improve using this technique during pandemic to spray disinfectants. The results obtained provide an alternate design for future propellers applications. Further it is observed that the endurance of the Unmanned Aerial Vehicle can be reduced considerably, by few alternate solution.https://bulletin.incas.ro/files/prasad__vol_12_iss_2.pdftwin propellerpayloadunmanned aerial vehicleendurance |
spellingShingle | G. PRASAD Performance estimation of Twin Propeller in Unmanned Aerial Vehicle INCAS Bulletin twin propeller payload unmanned aerial vehicle endurance |
title | Performance estimation of Twin Propeller in Unmanned Aerial Vehicle |
title_full | Performance estimation of Twin Propeller in Unmanned Aerial Vehicle |
title_fullStr | Performance estimation of Twin Propeller in Unmanned Aerial Vehicle |
title_full_unstemmed | Performance estimation of Twin Propeller in Unmanned Aerial Vehicle |
title_short | Performance estimation of Twin Propeller in Unmanned Aerial Vehicle |
title_sort | performance estimation of twin propeller in unmanned aerial vehicle |
topic | twin propeller payload unmanned aerial vehicle endurance |
url | https://bulletin.incas.ro/files/prasad__vol_12_iss_2.pdf |
work_keys_str_mv | AT gprasad performanceestimationoftwinpropellerinunmannedaerialvehicle |