The Aerospace Engineering Sciences Department worked with the ITLL to upgrade the analog measurement and control system of the wind tunnel with a digital data acquisition system. This new system provides high-speed, high-accuracy data that is easy to import into data-analysis programs such as Excel and Matlab.

Aerolab Educational Wind Tunnel

• 12-in x 12-in test section
• Variable air speed from 0-145 mph
• Contraction ratio: 9.5:1
• Computer-controlled (LabVIEW)

For more information, including a list of accessories, please visit the wind-tunnel page in our Experiment Directory.