University of Glasgow Indraft Trisonic Tunnel
21 Nov 2018





The wind tunnel is equipped with high-speed shadow and schlieren photography, pressure measurements and PSP, and PIV. It is used to drive innovation in the design of high-speed intakes, scramjet engines and secondary flows injection systems. Details:

  • Test section 10 x 5 x 60cm (width x height x length)
  • Mach number range M = 0.8 to 2.5
  • Run time = 20 seconds
Indraft Trisonic tunnel.jpg
  ​ Indraft Trisonic Tunnel