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.
