Investigation of wing clappers for micro-air vehicle

An experimental study was conducted to assess the aerodynamic benefits of using ‘Clap-and-Fling’ flapping flight mechanics for the development of Micro-Aerial Vehicle (MAV). The overall flight performance in terms of thrust generation of the ‘Clap-and-Fling’ flight was compared with the ‘no-clap’ fl...

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Bibliographic Details
Main Author: Ho, Aaron Kiu Hieng
Other Authors: Lau Gih Keong
Format: Final Year Project
Language:English
Published: 2015
Subjects:
Online Access:http://hdl.handle.net/10356/64022
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Institution: Nanyang Technological University
Language: English
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