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...

書誌詳細
第一著者:	Abdullah, Azizul
フォーマット:	学位論文
言語:	英語
出版事項:	2012
主題:	TL500-777 Aeronautics. Aeronautical engineering
オンライン･アクセス:	http://eprints.usm.my/44783/
Abstract	Abstract here

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