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
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;
Conference_Titel :
Electrical Engineering and Information & Communication Technology (ICEEICT), 2014 International Conference on
Conference_Location :
Dhaka
Print_ISBN :
978-1-4799-4820-8
DOI :
10.1109/ICEEICT.2014.6919157
