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...

Full description

Bibliographic Details
Main Author: G. PRASAD
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2020-06-01
Series:INCAS Bulletin
Subjects:
Online Access:https://bulletin.incas.ro/files/prasad__vol_12_iss_2.pdf
_version_ 1818752705097629696
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