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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| Format: | Thesis |
| Language: | English |
| Published: |
2012
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| Online Access: | http://eprints.usm.my/44783/1/AZIZUL%20BIN%20ABDULLAH.pdf http://eprints.usm.my/44783/ |
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