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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| 格式: | Thesis |
| 語言: | 英语 |
| 出版: |
2014
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| 在線閱讀: | http://eprints.usm.my/46369/ |
| Abstract | Abstract here |