Supersonic Wind Tunnels
Experiment
SUPERSONIC WIND TUNNEL (INTERMITTENT)
AF300 - Experiment
An intermittent supersonic (up to Mach 1.8) wind tunnel for investigations into subsonic and supersonic air flow around two dimensional models. Also for analysis of the profile of the tunnel
working section.
SUPERSONIC WIND TUNNEL (CONTINUOUS)
AF302 - Experiment
A suction-type, continuous-operation supersonic (up to Mach 1.8) wind tunnel for investigations into subsonic and supersonic air flow around two-dimensional models. Also for analysis of the profile of the tunnel working section.
Ancillary
SCHLIEREN APPARATUS FOR AF300
The Schilieren apparatus enables students to see air flow (including supersonic shock waves) around two-dimensional models as variations in the intensity of illumination. For use with the AF300 Intermittent Supersonic Wind Tunnel.
AIR COMPRESSOR AND RECEIVER
The Air Compressor Receiver and Dryer (AF300B) compresses, stores and delivers clean, dry compressed air for the Intermittent Supersonic Wind Tunnel.
SCHLIEREN APPARATUS FOR AF302
The Schilieren apparatus enables students to see air flow (including supersonic shock waves) around two-dimensional models as variations in the intensity of illumination. For use with the AF302 Continuious Supersonic Wind Tunnel.