Solar UAV: aerodynamic design and model testing in a wind tunnel
The baseline configuration of a solar-powered unmanned aerial vehicle (UAV) with an endurance of 24 hours at a cruise altitude of 8000m is determined through market research, analysis of the mission requirements and aerodynamic considerations. Using the baseline configuration, a 1:27 scale...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2012
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| Online Access: | http://hdl.handle.net/10356/50167 |