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...
Na minha lista:
| Main Authors: | , |
|---|---|
| Formato: | Livro |
| Publicado em: |
Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),
2012.
|
| Assuntos: | |
| Acesso em linha: | Link Metadata |
| Tags: |
Adicionar Tag
Sem tags, seja o primeiro a adicionar uma tag!
|
| Resumo: | 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. |
|---|---|
| Descrição do item: | https://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf |