Test Section
Dedicated measurement area for mounting models, sensors, and supporting experimental hardware.
Experimental aerodynamics infrastructure for controlled measurements, propeller studies, spray work, and student research projects.
The low-speed wind tunnel supports hands-on research and teaching activities across the group, from aerodynamic model testing to instrumentation development and project-based learning.
Dedicated measurement area for mounting models, sensors, and supporting experimental hardware.
Supports repeatable test campaigns for propeller performance, wake interaction, and flow diagnostics.
These images show the core facility, test section hardware, supporting systems, and representative project hardware.

Overall view of the low-speed wind tunnel facility.

Measurement area where aerodynamic models and instrumentation can be mounted and evaluated.

Supporting infrastructure around the wind-tunnel test section.

Representative hardware tested in the wind tunnel.