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...
Saved in:
主要作者: | Abdullah , Azizul |
---|---|
格式: | Thesis |
語言: | English |
出版: |
2012
|
主題: | |
在線閱讀: | http://eprints.usm.my/41530/1/AZIZUL_BIN_ABDULLAH_24_Pages.pdf |
標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|
相似書籍
-
The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
由: Al Aian, Ahmad Eshtiwey
出版: (2011) -
Performance characteristics monitoring of turboprop engine for the development of preliminary requirement of an engine testing facility
由: Mohd Yunos, Siti Nur Mariani
出版: (2011) -
Conceptual design of a small non-rigid airship with particular attention to its static and dynamic stability
由: Hariri, Azian
出版: (2009) -
The flight trajectory analysis on the existing aircraft
由: M Khalifa, Tarek M.
出版: (2012) -
On the development of computer code for aircraft flight dynamics analysis
由: Mohamed Alazomui, Outman
出版: (2014)