Facilities / Wind Tunnel

Low-Speed Wind Tunnel.

Experimental aerodynamics infrastructure for controlled measurements, propeller studies, spray work, and student research projects.

Overview

Controlled testing for aerodynamics and flow diagnostics.

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.

Test Section

Dedicated measurement area for mounting models, sensors, and supporting experimental hardware.

Research Workflows

Supports repeatable test campaigns for propeller performance, wake interaction, and flow diagnostics.

Images

Wind tunnel facility and example projects.

These images show the core facility, test section hardware, supporting systems, and representative project hardware.