Design and Analysis of UAV Propeller for Composite Materials

Abstract

Unmanned Aerial Vehicles (UAVs) have witnessed significant advancements and growth in recent years, where the efficiency and performance of propellers play a vital role. This study focuses on the design and analysis of UAV propellers utilizing ANSYS software. The propeller's structural behavior and aerodynamic effects are investigated through advanced engineering approaches. This study involves using ANSYS software to conduct a comprehensive analysis of UAV propellers, focusing on a comparative study of three distinct materials: Carbon Fiber Reinforced Polymer (CFRP), Glass Fiber Reinforced Polymer (GFRP), and aluminum alloy. A comparative study is conducted by analyzing various results such as maxim stress, maximum deformation and also the fluid flows. By considering the advantages and limitations of CFRP, GFRP, and aluminum alloy, this research contributes to the advancement of unmanned aerial technology, driving innovation and efficiency in UAV design and performance optimization.