Supersonic Wind Tunnel With Schlieren Optics

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

Technical Data:
Positive displacement fan, variable speed
Power consumption: 55kW
Sound-dampened, max. 84dB(A)
Supersonic wind tunnel
Schlieren optics
Halogen lamp with 50 and 100W
Adjustable slit diaphragm
Screen for Schlieren optics
2 adjustable parabolic mirrors
Cross-section of the measuring section:
100x25mm
Interchangeable walls for measuring section
2 x Laval contours: Ma 1,4 and Ma 1,8
1 x straight contour: Ma<1
Drag bodies
Recommended ambient conditions: 40% rel. humidity at 25C
Wedge, double wedge, projectile, rocket.