Amrulloh, Dimas (2022) ANALISIS DAMPAK PERUBAHAN WING TIP PADA WAHANA PESAWAT MODEL TAILLESS. Undergraduate thesis, UPN Veteran Jawa Timur.
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Abstract
The manufacture of aeromodelling is used to support flight compatible systems for unmanned aircraft or Unnmmed Aerial Vehicles (UAV). Although there are many aircraft manufactures, some applications of flight effectiveness in the field of UAV need to be considered aerodynamics to reach appropriate maneuvers. Airplanes are designed to produce sufficient lift for each flight mission. Airfoils work by utilizing air velocity to change the pressure on the top and bottom surfaces of the wing. For this reason, it is designed to improve aerodynamics by adding wing performance without having to increase the wingspan length by adding wingtips. wing tip serves to dampen the rotation in the air (vortex) at the tip of the wing caused by the meeting of the air at the bottom of the high-pressure wing with the air at the top of the wing with low pressure, which causes turbulence. Kata kunci: : Unammed Aerial Vehicle (UAV), aerodinamika, wingtip.
| Item Type: | Thesis (Undergraduate) | ||||||||||||
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| Subjects: | Q Science > QA Mathematics > QA76 Computer software | ||||||||||||
| Divisions: | Faculty of Computer Science | ||||||||||||
| Depositing User: | Dimas Amrulloh | ||||||||||||
| Date Deposited: | 25 Jan 2022 04:56 | ||||||||||||
| Last Modified: | 25 Jan 2022 04:56 | ||||||||||||
| URI: | http://repository.upnjatim.ac.id/id/eprint/4741 |
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