Conceptual Aerodynamic Studies Of A Small Tailless Unmanned Air Vehicle

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Conceptual Aerodynamic Studies Of A Small Tailless Unmanned Air Vehicle

In principle, the tailless model configuration can be equipped with any airfoil as long as the design is compensated with an appropriate combination of some parameter such as aspect ratio, sweep angle and twist. This thesis presents a parametric study of subsonic Tailless UAV conceptual design with...

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Bibliographic Details
Main Author:	Hashim, Afida
Format:	Thesis
Language:	English
Published:	2014
Subjects:	TL500-777 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.usm.my/46369/ http://eprints.usm.my/46369/1/Afida%20Binti%20Hashim24.pdf

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