Design of a High Altitude Fixed Wing Mini UAV – Aerodynamic Challenges

Hemant , Sharma and Suraj, CS and Roshan, Antony and Ramesh, G and Sajeer, Ahmed and Prasobh, Narayan Design of a High Altitude Fixed Wing Mini UAV – Aerodynamic Challenges. In: ICIUS 2013, 25 Sep 2013, Jaipur.

[img] PDF
cp135.pdf

Download (354kB)

Abstract

This paper attempts to bring out the challenges associated with the design of a high altitude mini UAV especially from the aerodynamics perspective. The mini UAV under consideration is a 2 kg class conventional, high wing and T-Tail configuration. A comparative study of various high lift airfoils has been done to illustrate that the selection of a suitable airfoil for high altitude applications is indeed an important part of the design activity and it shows that the wing loading of a UAV designed for high altitudes does not depend on the changes in air density alone. The chosen high lift low Reynolds number airfoil is found to have a minor effect on the aerodynamic parameters (Cl and Cd) with changes in Reynolds number. This paper also addresses the performance variation due to operation at off design condition such as at sea level.

Item Type: Conference or Workshop Item (Paper)
Subjects: AERONAUTICS > Aerodynamics
Depositing User: Mrs SK Pratibha
Date Deposited: 29 May 2015 07:29
Last Modified: 29 May 2015 07:29
URI: http://nal-ir.nal.res.in/id/eprint/12109

Actions (login required)

View Item View Item