Optimization of transition maneuvers through aerodynamic vectoring
This paper discusses the optimization of transition maneuvers between hover and cruise for small aircraft using a novel aerodynamic vectoring feature, which is achieved by allowing the wing to have variable incidence angle with respect to the fuselage. Compared to the fixed-wing aircraft case, the a...
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Main Authors: | Maqsood, Adnan., Go, Tiauw Hiong. |
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其他作者: | School of Mechanical and Aerospace Engineering |
格式: | Article |
語言: | English |
出版: |
2013
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在線閱讀: | https://hdl.handle.net/10356/85444 http://hdl.handle.net/10220/12360 |
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