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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書目詳細資料
主要作者:	Abdullah, Azizul
格式:	Thesis
語言:	English
出版:	2012
主題:	TL500-777 Aeronautics Aeronautical engineering
在線閱讀:	http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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