Specification
[1] investigation of pressure curves in supersonic flow
[2] visualisation of Mach lines and shock waves using Schlieren optics
[3] continuously operating, open supersonic wind tunnel, low pressure principle
[4] positive displacement fan with variable speed
[5] interchangeable walls in the measuring section produce velocities up to Mach 1,8 [6] drag bodies: rocket, projectile, double wedge and wedge
[7] manometer for displaying the pressure in the measurement point
Technical Data
Positive displacement fan, variable speed
– sound-dampened, max. 84dB(A)
– power consumption: 45….70kW
Supersonic wind tunnel
– cross-section of the measuring section:
– 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 PC with Windows recommended
Dimensions
LxWxH: 3500x810x1720mm (wind tunnel)
LxWxH: 1420x1600x1750mm (fan)
LxWxH: 1710x580x1450mm (Schlieren optics)
software for data acquisition via Windows 10 and Pc is recomended
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