Aerodynamics analysis for several fuselage geometries using fluent software and aerodynamics semi empirical method
This study presents aerodynamics analysis over several generic fuselage geometries. The aerodynamics analysis carried out by use of DATCOM Software, Fluent and own developed computer code. The own developed computer code is computer code which developed based on semi empirical aerodynamics method ad...
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| Format: | Thesis |
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2011
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| Online Access: | http://eprints.uthm.edu.my/2415/ http://eprints.uthm.edu.my/2415/1/Hasan_Taher.pdf |