Wind Tunnels

Mach Number of 2.0, in-draft wind tunnel

M2.0-WindTunnel

This is our in-draft supersonic wind tunnel. Designed Mach number is 2.0. Test section has an 80mm×80mm square cross section. This experimental apparatus is used for the research about shock wave – low density babble interaction.

Mach Number of 3.5, blow down wind tunnel

M3.5-WindTunnel

This is our blow down supersonic wind tunnel. Designed Mach number is 3.5.  Test section has an 40mm×40mm square cross section. This experimental apparatus is used for the research about shock wave – low density babble interaction, currently we are working about wind tunnel testing.