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...
| Main Author: | |
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| Format: | Thesis |
| Language: | English |
| Published: |
2012
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| Online Access: | http://eprints.usm.my/44783/ http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf |
| _version_ | 1848880152631574528 |
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| author | Abdullah, Azizul |
| author_facet | Abdullah, Azizul |
| author_sort | Abdullah, Azizul |
| building | USM Institutional Repository |
| collection | Online Access |
| 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, |
| first_indexed | 2025-11-15T17:58:35Z |
| format | Thesis |
| id | usm-44783 |
| institution | Universiti Sains Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T17:58:35Z |
| publishDate | 2012 |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | usm-447832019-07-01T02:55:28Z 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. |
| spellingShingle | TL500-777 Aeronautics. Aeronautical engineering Abdullah, Azizul Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software |
| title | 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_short | 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 |
| topic | TL500-777 Aeronautics. Aeronautical engineering |
| url | http://eprints.usm.my/44783/ http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf |