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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| Format: | Book |
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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM),
2012.
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| Online Access: | Link Metadata |
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| LEADER | 00000 am a22000003u 4500 | ||
|---|---|---|---|
| 001 | repouitm_8397 | ||
| 042 | |a dc | ||
| 100 | 1 | 0 | |a Maqsood, Adnan |e author |
| 700 | 1 | 0 | |a Tiauw, Hiong Go |e author |
| 245 | 0 | 0 | |a Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
| 260 | |b Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM), |c 2012. | ||
| 500 | |a https://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf | ||
| 520 | |a 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. | ||
| 546 | |a en | ||
| 690 | |a TJ Mechanical engineering and machinery | ||
| 655 | 7 | |a Article |2 local | |
| 655 | 7 | |a PeerReviewed |2 local | |
| 787 | 0 | |n https://ir.uitm.edu.my/id/eprint/8397/ | |
| 787 | 0 | |n https://jmeche.uitm.edu.my/ | |
| 856 | 4 | 1 | |u https://ir.uitm.edu.my/id/eprint/8397/ |z Link Metadata |