Aerodynamic Characteristics of the Design of Liam Propeller Blades: An Investigation

Abstract

By looking at new design changes, this study examines how well Low-Induction Axial Momentum (LIAM) propeller blades function aerodynamically. By comparing blade designs that include airfoil geometries and wave patterns along the edges, the research hopes to boost UAV performance and assist humanitarian operations. Results on lift, drag, and total efficiency under different operating circumstances may be gleaned using ANSYS simulations. This design adjustment has a considerable influence on aerodynamic performance, according to early-stage studies. It provides a platform for additional optimization and refining. Aerodynamics, Unmanned Aerial Vehicle Propellers, LIAM Blades, ANSYS Models, Airfoil Templates, Wave Formations