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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uitm-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. UiTM Press 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, 9 (1). pp. 1-17. ISSN 1823-5514 http://www-scopus-com.ezaccess.library.uitm.edu.my/record/display.uri?eid=2-s2.0-84865407133&origin=resultslist&sort=plf-f&src=s&imp=t&sid=31672AEE10B2D927A78B91A5746FEF92.CnvicAmOODVwpVrjSeqQ%3a60&sot=br&sdt=a&sl=62&s=SOURCE-ID%2821100198715%29+AND+PUBYEAR+IS+2012+AND+NOT+DOCTYPE%28ip%29&relpos=10&citeCnt=0&searchTerm= |
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TJ Mechanical engineering and machinery |
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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 |
description |
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. |
format |
Article |
author |
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 |
UiTM Press |
publishDate |
2012 |
url |
http://ir.uitm.edu.my/id/eprint/8397/ http://ir.uitm.edu.my/id/eprint/8397/ http://ir.uitm.edu.my/id/eprint/8397/1/AJ_ADNAN%20MAQSOOD%20JME%2012.pdf |
first_indexed |
2023-09-18T22:47:21Z |
last_indexed |
2023-09-18T22:47:21Z |
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1777417313195130880 |