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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Bibliographic Details
Main Authors: Maqsood, Adnan., Go, Tiauw Hiong.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2013
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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