Yılmaz, Oğuz Tuna (2025) How does the width and percentage of throttle applied on a model helicopter affect its lift force? Other thesis, TED Ankara Koleji.
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Abstract
The flight physics and aerodynamics describe the dynamics of the lift of a helicopter. Lift, the force that allows an aircraft to rise and remain airborne, depends on parameters such as throttle input to the rotor and the physical characteristics of the wings. In the experiment, the roles of throttle percentage and the width of the wings on the force of lift, two parameters that contribute to the flight mechanics, were investigated. These two parameters decide the ability of the helicopter to generate sufficient lift to counter the forces of gravity, therefore affecting the overall flight performance.
| Item Type: | Thesis (Other) |
|---|---|
| Uncontrolled Keywords: | helicopter affect, lift |
| Subjects: | Q Science > QC Physics |
| Depositing User: | Kamil Çömlekçi |
| Date Deposited: | 22 Jul 2025 11:30 |
| Last Modified: | 22 Jul 2025 11:30 |
| URI: | http://tedprints.tedankara.k12.tr/id/eprint/1408 |
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