Supersonic Wind Tunnel
SPECIFICATION
1. Investigation of pressure curves in supersonic flow
2. Visualization 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.
8. Software for data acquisition via USB under windows 7, 8.1, 10
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