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

 

Stosswellenrohr
  Shock Wave Tube

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

 
 

Freistrahl Kanal
  Open Jet Wind Tunnel

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

Rheologie
  Rheology






Staubbeschleuniger
  Dust Accelerator







Vakuumkammer
  Vacuum Chamber