Design improvement of a versatile ducted-fan UAV / Adnan Maqsood and Tiauw Hiong Go

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

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Abstract

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.

Item Type: Article
Uncontrolled Keywords: Ummanned Ducted-Fan, UAV, Wind-Tunnel Testing
Subjects: T Technology > TJ Mechanical engineering and machinery
Divisions: Faculty of Mechanical Engineering
Depositing User: Staf Pendigitan 1
Date Deposited: 17 Mar 2014 06:12
Last Modified: 05 Aug 2016 07:57
URI: http://ir.uitm.edu.my/id/eprint/8397

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