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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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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
http://eprints.usm.my/44783/
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spelling my.usm.eprints.44783 http://eprints.usm.my/44783/ Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software 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 NonPeerReviewed application/pdf en http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf Abdullah, Azizul (2012) Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software. Masters thesis, Universiti Sains Malaysia.
institution Universiti Sains Malaysia
building Hamzah Sendut Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Sains Malaysia
content_source USM Institutional Repository
url_provider http://eprints.usm.my/
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
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
publishDate 2012
url http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf
http://eprints.usm.my/44783/
_version_ 1643711103824297984
score 13.214268

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