Experiment on aerodynamic characteristics of a novel micro tilt ducted fan aircraft with wings

Wind tunnel experiment is employed to study the aerodynamic characteristics of a novel micro tilt ducted fan MAV. Fullscale model is adopted in the wind tunnel experiment. The experiment focus on three modes: no motor, single motor and dual motors, respectively. The influences of design parameters on aerodynamic forces and moments are measured to get some typical aerodynamic characteristics. The test results are useful for theoretical modeling.