Development and testing of fuel-cell powered UAV
This report serves to investigate and derive an fuel cell powered unmanned aerial vehicle (UAV) design. Being a fuel cell UAV, this design is centred around the power and thrust output of the fuel cell. Primarily, the drag of UAV must be lower than the thrust provided and the lift must be greater th...
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2011
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| Online Access: | http://hdl.handle.net/10356/46158 |