0.6m Trisonic Wind Tunnel

0.6m Trisonic Wind Tunnel



Working section

0.6m x 0.6m


Intermittent blowdown

Mach number range

0.2 to 4.0

Stagnation pressure

1.5 to 8.0 bar

Reynolds number

8 x 106 to 60 x 106 per metre,

Model incidence

-15° to 30° continuous and step mode.

Test duration

60 seconds (typical)

Special controls

Transonic Mach number control, Transonic Mach number and pressure sweep.


Special feature

Automatic nozzle contour for supersonic Mach numbers using VMFN

Last updated on : 10-05-2018 03:52:05pm