Conceptual Aerodynamic Studies Of A Small Tailless Unmanned Air Vehicle

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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书目详细资料
主要作者:	Hashim, Afida
格式:	Thesis
语言:	English
出版:	2014
主题:	TL500-777 Aeronautics Aeronautical engineering
在线阅读:	http://eprints.usm.my/46369/1/Afida%20Binti%20Hashim24.pdf
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