Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go
The paper discusses the aerodynamic design improvement of a ducted fan unmanned Aerial vehicle (UAV). The UAV is capable of take-off vertically, hover and transition to cruise and is equipped with wing. the aerodynamics of the UAV is estimated through wind-tunnel experiments. The design improvement...
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| Autores principales: | , |
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| Formato: | Libro |
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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),
2012.
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| Acceso en línea: | Link Metadata |
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| Sumario: | The paper discusses the aerodynamic design improvement of a ducted fan unmanned Aerial vehicle (UAV). The UAV is capable of take-off vertically, hover and transition to cruise and is equipped with wing. the aerodynamics of the UAV is estimated through wind-tunnel experiments. The design improvement is carried out for the two phases of mission profile: hover and cruise. |
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| Notas: | https://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf |