On the development of computer code for aircraft flight dynamics analysis

The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stability analysis and the lateral – directional stability analysis. The present work focused on the second mode of flight. The stability analysis carried out by evaluates the behavior of three flight par...

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Bibliographic Details
Main Author:	Mohamed Alazomui, Outman
Format:	Thesis
Language:	English English
Published:	2014
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL500-777 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.uthm.edu.my/1630/
Abstract	Abstract here

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