Design and analysis of yaw stability and control surfaces for UiTM’s BWB UAV baseline-II E-4 / Firdaus Mohamad.

UiTM is currently developing a blended wing body aircraft known as UiTM’s BWB UAV Baseline-II. There are a few revolutions made since 2009. The one which concealed with directional control is known as UiTM’s BWB UAV Baseline-II E-4. This aircraft is categorized as a tailless aircraft. Hence, it is u...

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Bibliographic Details
Main Author: Mohamad, Firdaus
Format: Thesis
Language:English
Published: 2012
Subjects:
Online Access:https://ir.uitm.edu.my/id/eprint/39638/1/39638.pdf
https://ir.uitm.edu.my/id/eprint/39638/
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