Optimization of Quadcopter Propeller Aerodynamics Using Blade Element and Vortex Theory


Authors : Solomon Ileanaju Ugbane; Chima Umeaku; Idoko Peter Idoko; Lawrence Anebi Enyejo; Comfort Idongesit Michael; Onuh Matthew Ijiga

Volume/Issue : Volume 9 - 2024, Issue 10 - October

Google Scholar : https://tinyurl.com/2nfc3kxv

Scribd : https://tinyurl.com/hpmpcrz6

DOI : https://doi.org/10.38124/ijisrt/IJISRT24OCT1820

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Abstract : The optimization of quadcopter propeller aerodynamics is crucial for enhancing the efficiency and stability of unmanned aerial vehicles (UAVs), especially in their increasing applications across various sectors, including humanitarian relief and delivery services. This study focuses on optimizing quadcopter propeller performance using Blade Element Theory and Glauert Vortex Theory to analyze the aerodynamic properties and predict thrust generation accurately. Experimental methods, including wind tunnel testing and static thrust measurements, were used to validate the theoretical models. The results indicate a close correlation between theoretical predictions and experimental data, providing insights into improving propeller efficiency and mitigating aerodynamic losses. By understanding the propeller characteristics, this research contributes to the development of advanced drone propulsion systems with enhanced thrust, reduced drag, and better overall flight performance. The findings also highlight the impact of environmental factors such as turbulence and blade geometry on quadcopter stability, pointing toward areas for further improvement in propeller design. This paper serves as a valuable resource for drone hobbyists, engineers, and researchers seeking to enhance UAV performance through optimized propeller aerodynamics.

Keywords : Quadcopter, Propeller Aerodynamics, Blade Element Theory, Vortex Theory, UAV Optimization, Thrust Prediction, Drag Reduction, Drone Propulsion, Wind Tunnel Testing, Aerodynamic Efficiency.

References :

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The optimization of quadcopter propeller aerodynamics is crucial for enhancing the efficiency and stability of unmanned aerial vehicles (UAVs), especially in their increasing applications across various sectors, including humanitarian relief and delivery services. This study focuses on optimizing quadcopter propeller performance using Blade Element Theory and Glauert Vortex Theory to analyze the aerodynamic properties and predict thrust generation accurately. Experimental methods, including wind tunnel testing and static thrust measurements, were used to validate the theoretical models. The results indicate a close correlation between theoretical predictions and experimental data, providing insights into improving propeller efficiency and mitigating aerodynamic losses. By understanding the propeller characteristics, this research contributes to the development of advanced drone propulsion systems with enhanced thrust, reduced drag, and better overall flight performance. The findings also highlight the impact of environmental factors such as turbulence and blade geometry on quadcopter stability, pointing toward areas for further improvement in propeller design. This paper serves as a valuable resource for drone hobbyists, engineers, and researchers seeking to enhance UAV performance through optimized propeller aerodynamics.

Keywords : Quadcopter, Propeller Aerodynamics, Blade Element Theory, Vortex Theory, UAV Optimization, Thrust Prediction, Drag Reduction, Drone Propulsion, Wind Tunnel Testing, Aerodynamic Efficiency.

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