facilities S

Atmosphärischer Windkanal  
Atmospheric Wind Tunnel   

- Eiffel design
- max. size of test section:

  1800 x 1800 x 22000 mm³
- max. flow velocity: 45 m/s

Trisonischer Windkanal  
Trisonic Wind Tunnel

- Blow-Down Wind Tunnel
- cross sectional area of test section:

  675 x 300 mm²
- range of Mach number: 0,3 - 3,0

Shock Wave Tube  

Shock Wave Tube

- length of the low-pressure tube: 12000 mm
- shock Mach number: 5,5 - 7,0

 

Open Jet Tunnel  

Open Jet Wind Tunnel

- diameter of the nozzle: 370 mm, 170 mm
- max. flow velocity: 80 m/s