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...
| 第一著者: | |
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| フォーマット: | 学位論文 |
| 言語: | 英語 |
| 出版事項: |
2014
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| 主題: | |
| オンライン･アクセス: | http://eprints.usm.my/46369/ |
| Abstract | Abstract here |