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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Universiti Teknologi Petronas
2009
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my-utp-utpedia.5222017-01-25T09:44:37Z http://utpedia.utp.edu.my/522/ Effects of Wake Turbulence on Aircraft Wing Section Numerical Study Nur Hazwany Bt Mohd Hatta, Nur Hazwany TJ Mechanical engineering and machinery 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 dynamics (CFD) software FLUENT 6.2. Simulations were carried out at different velocities at low Reynolds number and different angle of attack, α. The fundamental aerodynamic of wake effects analyzed from lift and drag coefficient values obtained from simulations that have been carried out. The outcome shows that the wake turbulence affected the lift and drag force of preceding aircraft is subjected to separation distance. Universiti Teknologi Petronas 2009 Final Year Project NonPeerReviewed application/pdf en http://utpedia.utp.edu.my/522/1/Nur_Hazwany_Bt_Mohd_Hatta.pdf Nur Hazwany Bt Mohd Hatta, Nur Hazwany (2009) Effects of Wake Turbulence on Aircraft Wing Section Numerical Study. Universiti Teknologi Petronas. (Unpublished) |
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TJ Mechanical engineering and machinery Nur Hazwany Bt Mohd Hatta, Nur Hazwany Effects of Wake Turbulence on Aircraft Wing Section Numerical Study |
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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 dynamics (CFD) software FLUENT 6.2. Simulations were carried out at different velocities at low Reynolds number and different angle of attack, α. The fundamental aerodynamic of wake effects analyzed from lift and drag coefficient values obtained from simulations that have been carried out. The outcome shows that the wake turbulence affected the lift and drag force of preceding aircraft is subjected to separation distance. |
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Final Year Project |
author |
Nur Hazwany Bt Mohd Hatta, Nur Hazwany |
author_facet |
Nur Hazwany Bt Mohd Hatta, Nur Hazwany |
author_sort |
Nur Hazwany Bt Mohd Hatta, Nur Hazwany |
title |
Effects of Wake Turbulence on Aircraft Wing Section Numerical Study |
title_short |
Effects of Wake Turbulence on Aircraft Wing Section Numerical Study |
title_full |
Effects of Wake Turbulence on Aircraft Wing Section Numerical Study |
title_fullStr |
Effects of Wake Turbulence on Aircraft Wing Section Numerical Study |
title_full_unstemmed |
Effects of Wake Turbulence on Aircraft Wing Section Numerical Study |
title_sort |
effects of wake turbulence on aircraft wing section numerical study |
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Universiti Teknologi Petronas |
publishDate |
2009 |
url |
http://utpedia.utp.edu.my/522/1/Nur_Hazwany_Bt_Mohd_Hatta.pdf http://utpedia.utp.edu.my/522/ |
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1739830669825015808 |
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13.160551 |