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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Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM)
2012
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Online Access: | http://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf http://ir.uitm.edu.my/id/eprint/8397/ https://jmeche.uitm.edu.my/ |
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my.uitm.ir.83972016-08-05T07:57:59Z http://ir.uitm.edu.my/id/eprint/8397/ Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go Maqsood, Adnan Tiauw, Hiong Go TJ Mechanical engineering and machinery 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. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) 2012 Article PeerReviewed text en http://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf Maqsood, Adnan and Tiauw, Hiong Go (2012) Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go. Journal of Mechanical Engineering (JMechE), 9 (1). pp. 1-17. ISSN 1823-5514 ; 2550-164X https://jmeche.uitm.edu.my/ |
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TJ Mechanical engineering and machinery Maqsood, Adnan Tiauw, Hiong Go Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
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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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Article |
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Maqsood, Adnan Tiauw, Hiong Go |
author_facet |
Maqsood, Adnan Tiauw, Hiong Go |
author_sort |
Maqsood, Adnan |
title |
Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
title_short |
Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
title_full |
Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
title_fullStr |
Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
title_full_unstemmed |
Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go |
title_sort |
design improvement of a versatile ducted-fan uav / adnan maqsood and tiauw hiong go |
publisher |
Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM) |
publishDate |
2012 |
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http://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf http://ir.uitm.edu.my/id/eprint/8397/ https://jmeche.uitm.edu.my/ |
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