Design and development of composite structure for a micro-UAV

This report describes the design process and fabrication of a composite fuselage for a 2kg class micro-UAV which is propelled by flapping wings. It begins with the comparison and selection of fabrication process. The carbon fibre reinforced plastic was selected for its low speci...

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Bibliographic Details
Main Author: Loke, Jun Jie.
Other Authors: Sunil Chandrakant Joshi
Format: Final Year Project
Language:English
Published: 2012
Subjects:
Online Access:http://hdl.handle.net/10356/49719
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Institution: Nanyang Technological University
Language: English