Supersonic Wind Tunnel- Engineering Lab Training Systems Description and Specifications for Lab Tenders
Technical Description Continuously operating supersonic wind tunnel with
a rectangular measuring section..
Transsonic and supersonic flows from
Ma 0.8 up to Ma 1.8 can be realized with interchangeable measuring
sections and nozzle profiles. Supersonic flow and the occurring shock
waves can be directly observed with the supplied Schlieren optic
apparatus. The continuous operation allows enough time to take
measurements and to observe the phenomena. Four aerofoil models are
supplied: a wedge, a double wedge, a bullet and a rocket. A flow
straightener at the inlet ensures a low degree of turbulence. The tunnel
is driven by a speed controlled vacuum pump. The pump is effectively
silenced so it can be placed in the same room as the wind tunnel Fluid
Mechanics Lab Equipments manufacturers