0.6m Trisonic Wind Tunnel
Working section
0.6m x 0.6m
Operation
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