The Transonic Wind Tunnel (TSWT) is a closed-circuit ejector driven tunnel, designed, built and commissioned by the Aeromechanical Systems Group. The Applied Aerodynamics group has a wide range of skills encompassing experimental aeronautical, automotive and industrial aerodynamics.
Summary of applications
Type: Closed-circuit ejector driven
Working section: 200mm x 230mm
Speed range: M=0.5 to 1.4
Other features: Variable incidence sting support, working-section wall suction