DocumentCode
113242
Title
Performance analysis of aerofoil for Unmanned Aerial Vehicle
Author
Md Faisal, Kh. ; Papon, Md Easir Arafat ; Nafi, Akhter Mahmud
Author_Institution
Aeronaut. Eng. Dept., Mil. Inst. of Sci. & Technol., Dhaka, Bangladesh
fYear
2014
fDate
10-12 April 2014
Firstpage
1
Lastpage
5
Abstract
The growing interest in development of UAV has created a need for the comparative analysis of performance parameters of different aerofoils. Using this concept different characteristics of aerofoils are explored to design the wing of various UAV fulfilling various purposes. In this research work, the requirements of our desired UAV are established. These requirements are translated into performance parameters. Then the aerofoil that best meet the requirements was optimized from different arbitrary aerofoils through experimental investigation of the performance parameters.
Keywords
aerospace components; autonomous aerial vehicles; vehicle dynamics; UAV; aerofoil performance analysis; design; unmanned aerial vehicles; wings; Aerodynamics; Airplanes; Fluids; Performance analysis; Shape; Unmanned aerial vehicles; Aerofoil; Drag; Lift co-efficient; UAV; lift-drag ratio; pitching moment;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical Engineering and Information & Communication Technology (ICEEICT), 2014 International Conference on
Conference_Location
Dhaka
Print_ISBN
978-1-4799-4820-8
Type
conf
DOI
10.1109/ICEEICT.2014.6919157
Filename
6919157
Link To Document