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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書目詳細資料
主要作者:	Hashim, Afida
格式:	Thesis
語言:	English
出版:	2014
主題:	TL500-777 Aeronautics Aeronautical engineering
在線閱讀:	http://eprints.usm.my/46369/1/Afida%20Binti%20Hashim24.pdf
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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