Supersonic Wind Tunnel With Schlieren Optics


Supersonic Wind Tunnel With Schlieren Optics .

Supersonic Wind Tunnel With Schlieren Optics

Specification Of Supersonic Wind Tunnel With Schlieren Optics

  • Investigation of pressure curves in supersonic flow
  • Visualisation of Mach lines and shock waves using Schlieren optics
  • Continuously operating, open supersonic wind tunnel, low pressure principle
  • Positive displacement fan with variable speed
  • Interchangeable walls in the measuring section produce velocities up to Mach 1,8
  • Drag bodies: rocket, projectile, double wedge and wedge
  • Manometer for displaying the pressure in the measurement point

Technical Data

  • Positive displacement fan, variable speed
  • Sound-dampened, max. 84dB(A)
  • Power consumption: 55kW

Supersonic wind tunnel

  • Cross-section of the measuring section:
  • 100x25mm
  • Interchangeable walls for measuring section
  • 1 x straight contour: Ma<1
  • 2 x Laval contours: Ma 1,4 and Ma 1,8

Schlieren optics

  • Halogen lamp with 50 and 100W
  • 2 adjustable parabolic mirrors
  • Adjustable slit diaphragm
  • Screen for Schlieren optics

Drag bodies

  • Wedge, double wedge, projectile, rocket
  • Recommended ambient conditions: 40% rel. humidity at 25°C

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