Development of a multi-rotor VTOL UAV : numerical study of the tilting-transition phase
Development of Numerical Simulation Capability through CFD to analyse aerodynamic effects on UAV body during transition for a 2D case. Analyses of the acceptable tilt rates appropriate for level transitions for a 2D case.
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| Format: | Final Year Project (FYP) |
| Language: | English |
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2018
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| Online Access: | http://hdl.handle.net/10356/75224 |