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: | , |
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Other Authors: | |
Format: | Article |
Language: | English |
Published: |
2013
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Online Access: | https://hdl.handle.net/10356/85444 http://hdl.handle.net/10220/12360 |
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Institution: | Nanyang Technological University |
Language: | English |
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