On the development of computer code for aircraft flight dynamics analysis

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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書目詳細資料
主要作者:	Mohamed Alazomui, Outman
格式:	Thesis
語言:	English English
出版:	2014
主題:	TL Motor vehicles Aeronautics Astronautics
在線閱讀:	http://eprints.uthm.edu.my/1630/1/24p%20OUTMAN%20MOHAMED%20ALAZOMUI.pdf http://eprints.uthm.edu.my/1630/2/OUTMAN%20MOHAMED%20ALAZOMUI%20WATERMARK.pdf
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