Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software

Abdullah, Azizul (2012) Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software. Masters thesis, Universiti Sains Malaysia.

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Abstract

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 cannot determine the stability coefficients directly. Thus, as one of the promising alternative methods, the DATCOM software was employed in the present study, in order to estimate the aerodynamic coefficients and analyze the static and dynamic stabilities at the preliminary design stage of a small Unmanned Aerial Vehicle,

Item Type:	Thesis (Masters)
Subjects:	T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500-777 Aeronautics. Aeronautical engineering
Divisions:	Kampus Kejuruteraan (Engineering Campus) > Pusat Pengajian Kejuruteraan Aeroangkasa (School of Aerospace Engineering) > Thesis
Depositing User:	ASM Ab Shukor Mustapa
Date Deposited:	01 Jul 2019 02:55
Last Modified:	01 Jul 2019 02:55
URI:	http://eprints.usm.my/id/eprint/44783

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