Supersonic Wind Tunnels

A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2Mach number and flow are determined by the nozzle geometry. The Reynolds number is varied by changing the density level (pressure in the settling chamber). Therefore, a high-pressure ratio is required (for a supersonic regime at M=4, this ratio is of the order of 10). Apart from that, condensation of moisture or even gas liquefaction can occur if the static temperature becomes cold enough. This means that a supersonic wind tunnel usually needs a drying or a pre-heating facility. A supersonic wind tunnel has a large power demand, so most are designed for intermittent instead of continuous operation.

  • Supersonic Wind Tunnel (Continuous) AF302
    Item Number:
    AF302 - Experiment

    A suction-type continuous operation supersonic (up to Mach 1.8) wind tunnel for investigations into subsonic and supersonic airflow around two-dimensional models. Also, for analysis of the profile of the tunnel working section.

  • TecQuipment | Aerodynamics Education
    Item Number:
    AF300 - Experiment

    The AF300 is an intermittent operation induction type supersonic wind tunnel that allows investigations into the flow around 2-dimensional models at supersonic airspeeds.