STUDI AERODINAMIKA KONFIGURASI HIGH LIFT DEVICES OPTIMUM DARI PENAMPANG SAYAP PESAWAT AIRBUS A380
Take off and landing are considered to be crucial for an aircraft, that is the reason why High Lift Devices analysis is need to be done because in those phases they contributes for producing a better lift. Analitical and numerical method will be used to obtain the highest lift with optimum geomet...
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| Format: | Final Project |
| Language: | Indonesia |
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| Online Access: | https://digilib.itb.ac.id/gdl/view/40709 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
| Summary: | Take off and landing are considered to be crucial for an aircraft, that is the reason why
High Lift Devices analysis is need to be done because in those phases they contributes
for producing a better lift. Analitical and numerical method will be used to obtain the
highest lift with optimum geometry of slat and flap for take off and landing. Despite
of that, the flow behavior for High Lift Devices will also be observed.
The wing section of Airbus A380 will be modeled with CATIA, and then the
meshing process will be done with ICEM CFD. The numerical approach to analyse
flow behaviour surrounding the wing section will be carried out using FLUENT.
Based on the result therefore can be concluded that the geometry of slat gap and
overlap, also flap gap and overlap will affect the lift that can be produced |
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