Effects of Wake Turbulence on Aircraft Wing Section Numerical Study
Fundamental of wake turbulence effects on aircraft wing section is determined by using numerical approach. NACA 2412 wing section is selected in this study and the wing is model using GAMBIT 2.2 software. For the numerical analysis, the flow past over the wing was simulated using computational fluid...
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| Format: | Final Year Project |
| Language: | English |
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Universiti Teknologi Petronas
2009
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| Online Access: | http://utpedia.utp.edu.my/522/1/Nur_Hazwany_Bt_Mohd_Hatta.pdf http://utpedia.utp.edu.my/522/ |
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