The transonic wind tunnel (TSWT) is a closed-circuit ejector-driven tunnel, designed, built and commissioned by the Aeromechanical Systems Group. The Aeromechanical Systems 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.