This study aims to design and evaluate an efficient setup for a flapping wing operating in artificially generated gusts created by a Windshaper (WS) with dimensions 2 × 1.5 m. The WS allows flow speeds up to 20 m/s and enables the generation of various time-dependent wind profiles. The setup features a NACA0018 airfoil equipped with a dynamically actuated flap, controlled in real time by a servo motor. The flapping wing structure and its lateral support are 3D-printed and attached to a vertical beam. Two pressure sensors are embedded in the airfoil’s upper surface: one positioned before the maximum thickness point and the other after it.