Flight Demonstration Wind Tunnel-F116

Product Introduction：

This product is used as a basic experimental platform for studying the basic flight characteristics of aircraft at low speeds and verifying relevant theories; The wind tunnel is mainly composed of a tunnel body, a model display section, a drive system, and a measurement and control system. The control system can adjust the tail angle and wind speed to study the interaction between air and the model, such as lift and drag. Through intuitive control, it simulates takeoff, horizontal flight, landing, stall, center of gravity displacement, pitch oscillation, heave oscillation, etc; By combining variable frequency speed regulation, resistance sensors, and smoke generator modules, experimental research and theoretical verification can be carried out on the drawing of lift curves for various flight postures of aircraft models. The wing module model supports customization and expansion, as well as experimental design and expansion;