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What is Aerodynamic Design and Optimization of Propellers For Multirotor about?
This paper presents a methodology for designing custom propellers for unmanned air vehicles (UAVs) using evolutionary algorithms and Blade Element Theory. The approach includes realistic constraints and investigates the interactions between propellers in a hex-rotor configuration, resulting in a propeller design that improves efficiency and reduces power consumption by approximately 7%. The findings suggest that the methodology can be generalized to various blade design problems, adapting to specific requir
- Author
- Raneem Saad
- Language
- EN