THE EFFECT OF SLIPSTREAM FLOW BY PROPELLER ON WINGS AERODYNAMIC CHARACTERISTICS OF UAV HALE AIRCRAFT
Research on the effect of slipstream flow by propellers has been carried out using simulation and experimental methods. The simulation method used is CFD while the experimental method is carried out in the LAPAN Subsonic Wind Tunnel. The research was conducted on a HALE UAV aircraft which has a span...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/62032 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |