Investigation On The Propulsive Efficiency Of The Small Uav Conceptual Design

A parametric study of low altitude small Unmanned Autonomous Vehicle (UAV) conceptual design was performed. The purpose was to estimate constraint diagram propulsive efficiency of propeller-Brushless Direct Current (BLDC) motor propulsion system at two different flight conditions with the considerat...

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Bibliographic Details
Main Author:	Yahya, Khairul Ikhsan
Format:	Thesis
Language:	English
Published:	2012
Subjects:	TL500-777 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.usm.my/41889/
Abstract	Abstract here

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