This laboratory course complements the theoretical concepts learned in Aerodynamics for UAVs. Students will gain hands-on experience with aerodynamic principles through a series of experiments and simulations. The lab will involve the use of wind tunnels, aerodynamic test rigs, and computational fluid dynamics (CFD) software to investigate the aerodynamic characteristics of various UAV components, including airfoils, wings, propellers, and rotors. Students will learn experimental techniques, data acquisition and analysis, and the interpretation of experimental results. This lab will enhance students' understanding of aerodynamic phenomena and their practical application in UAV design.