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
Published: 2014
Online Access:http://eprints.uthm.edu.my/1630/1/24p%20OUTMAN%20MOHAMED%20ALAZOMUI.pdf
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