Low and High Speed Aerodynamics Laboratory
The low speed wind tunnel is a closed-circuit, continuous flow type with a 100 horsepower variable frequency drive. The test section flow area is 0.6 x 0.9 meters (2 x 3 feet). The tunnel is capable of a maximum flow velocity of 50 meters per second. The tunnel is also equipped with a 3-component force balance, a multiplexed data acquisition system, and equipment for smoke visualization.
To study various avionics system and their data transfer technique in aircraft