Preliminary Stability Estimation And Analysis Of Aeromech I Uav Using Datcom Software

Preliminary Stability Estimation And Analysis Of Aeromech I Uav Using Datcom Software

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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书目详细资料
主要作者:	Abdullah , Azizul
格式:	Thesis
语言:	English
出版:	2012
主题:	TL Motor vehicles Aeronautics Astronautics
在线阅读:	http://eprints.usm.my/41530/1/AZIZUL_BIN_ABDULLAH_24_Pages.pdf
标签:	添加标签没有标签, 成为第一个标记此记录!

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