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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Bibliographic Details
Main Author:	Abdullah, Azizul
Format:	Thesis
Language:	English
Published:	2012
Subjects:	TL500-777 Aeronautics Aeronautical engineering
Online Access:	http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf
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id	my-usm-ep.44783
record_format	uketd_dc
spelling	my-usm-ep.447832019-07-01T02:55:28Z Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software 2012-06 Abdullah, Azizul TL500-777 Aeronautics. Aeronautical engineering 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, 2012-06 Thesis http://eprints.usm.my/44783/ http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuteraan Aeroangkasa
institution	Universiti Sains Malaysia
collection	USM Institutional Repository
language	English
topic	TL500-777 Aeronautics Aeronautical engineering
spellingShingle	TL500-777 Aeronautics Aeronautical engineering Abdullah, Azizul Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software
description	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,
format	Thesis
qualification_level	Master's degree
author	Abdullah, Azizul
author_facet	Abdullah, Azizul
author_sort	Abdullah, Azizul
title	Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software
title_short	Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software
title_full	Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software
title_fullStr	Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software
title_full_unstemmed	Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software
title_sort	preliminary stability estimation and analysis of aeromech i uav using datcom software
granting_institution	Universiti Sains Malaysia
granting_department	Pusat Pengajian Kejuteraan Aeroangkasa
publishDate	2012
url	http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf
_version_	1747821397825028096

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

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