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...
Main Author: | Wee, Raun Joshua Guanwei. |
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Other Authors: | School of Mechanical and Aerospace Engineering |
Format: | Final Year Project (FYP) |
Language: | English |
Published: |
2012
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Subjects: | |
Online Access: | http://hdl.handle.net/10356/50167 |
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