Dynamics of flapping wing MAV during takeoff and hovering

To understand Flapping Wing Aerodynamics during low Reynolds Number and High AOA.To simulate Dynamics of Flapping Wing MAV during takeoff and Hovering.To built MAV which demonstrates independent Vertical Takeoff and Hovering capability. [2nd Award]

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Bibliographic Details
Main Author: Wang, Hao
Other Authors: Yongki Go Tiauw Hiong
Format: Student Research Poster
Language:English
Published: 2013
Online Access:https://hdl.handle.net/10356/95255
http://hdl.handle.net/10220/9054
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Institution: Nanyang Technological University
Language: English
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