Wind Tunnels

Wind Tunnel (7’ x 10’) Low Speed

Description Applications
7'x10' low speed wind tunnel capable of speeds up to Mach 0.37. Stability and control aircraft characteristics, propulsion testing, laminar flow testing.; Force and moment data aquired through a six component internal balance.; Static and dynamic pressure measurements (64 channels for high rate data collection); Flow visualization through a smoke wand Speed: Up to Mach 0.37; Angle of Attack Range: -14 to 90 deg; Angle of Sideslip Range: -24 to +24 deg
Specifications  
Wind Tunnel (7’ x 10’) Low Speed

Wind Tunnel (2’)

Description Applications
28" x 40" low speed wind tunnel capable of speeds up to Mach 0.22. Research for stability and control aircraft characteristics; Force and moment data acquired through an Integrated sting/balance. Speed: Up to Mach 0.22 AOA Range: -14 to 90 deg Angle of sideslip: -35 to +35 deg
Specifications  
Wind Tunnel (2’)