Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software

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Stability is one aspect of the aircraft performance. Conventional methods such as wind tunnel test, flight test and Computational Fluid Dynamics (CFD) are used for the estimation and analysis of the stability during aircraft design process. Those methods are time consuming and expensive because they...

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Bibliographic Details
Main Author:	Abdullah, Azizul
Format:	Thesis
Language:	English
Published:	2012
Subjects:	TL500-777 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.usm.my/44783/
Abstract	Abstract here

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