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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Format: | Final Year Project |
Language: | English |
Published: |
2012
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Online Access: | http://hdl.handle.net/10356/49719 |
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Institution: | Nanyang Technological University |
Language: | English |