Design and analysis of yaw stability and control surfaces for UiTM’s BWB UAV baseline-II E-4 / Firdaus Mohamad.
UiTM is currently developing a blended wing body aircraft known as UiTM’s BWB UAV Baseline-II. There are a few revolutions made since 2009. The one which concealed with directional control is known as UiTM’s BWB UAV Baseline-II E-4. This aircraft is categorized as a tailless aircraft. Hence, it is u...
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
2012
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| 在線閱讀: | https://ir.uitm.edu.my/id/eprint/39638/1/39638.pdf https://ir.uitm.edu.my/id/eprint/39638/ |
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