Design of a ducted fan for an unmanned aerial vehicle

The development of ducted fan propulsion systems in the model and full scale light aircraft has shown steady increase in the recent years due to its advantages under static and low speed thrust. This work is focused on the conceptual design, fabrication and testing of the ducted fan blades in an...

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Bibliographic Details
Main Author: Tay, Rooney Yong Seah.
Other Authors: Go Tiauw Hiong
Format: Final Year Project
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/16233
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Institution: Nanyang Technological University
Language: English

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