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