On the development of computer code for aircraft flight dynamics analysis
The stability analysis of the aircraft can be evaluated in two flight modes: longitudinal stability analysis and the lateral – directional stability analysis. The present work focused on the second mode of flight. The stability analysis carried out by evaluates the behavior of three flight parameter...
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| Format: | Thesis |
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2014
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| Online Access: | http://eprints.uthm.edu.my/7561/ http://eprints.uthm.edu.my/7561/1/OUTMAN_MOHAMED_ALAZOMUI.pdf |
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