The laboratory features an advanced low-turbulence closed circuit wind tunnel covering an area of approximately 250m², capable of achieving wind speeds exceeding 40m/s with turbulence below 0.2%. Coupled with a 1m diameter three-dimensional attitude turntable support, it provides a reliable, comprehensive, and rich aerodynamic experimental platform for the design, research, and testing of bio-inspired flight and small unmanned aerial vehicles, meeting all measurement requirements for the full range of flight speeds and attitudes of micro aerial vehicles. Additionally, the laboratory also houses a multi-functional low-turbulence closed circuit water tunnel/tank covering an area of approximately 150m², capable of achieving flow speeds exceeding 1m/s with turbulence below 0.5%, providing a stable and diverse fluid mechanics experimental platform for the design, research, and testing of surface vessels and underwater gliders by switching between water tunnel/tank operating modes.