The tunnel is capable of continuous operation at velocities of over 150 mph. With a contraction ratio of 15:1 and the use of multiple diffusion screens, very low turbulence is achievable. The facility is a closed circuit, single return tunnel with a 7 ft wide by 5 ft high by 25 ft long test section. It is now fully owned by the University and is used for education, research and to serve local industry as a well equipped, affordable subsonic wind tunnel resource. It was initially designed to study the effects of gusts on aircraft but has since been upgraded to suit a variety of applications. The subsonic tunnel was built in 1956 in a joint effort with the US Air Force. The wind tunnel was used to demonstrate the powerful winds you find in tornadoes and the dangers that go along with them.) Subsonic Low Turbulence 5 ft x 7 ft Wind Tunnel (The University of Michigan Aerospace Engineering Wind tunnel was featured in a special report by on May 15, 2012. Subsonic 6 inch Wind Tunnels for Student Classroom Laboratories.Subsonic 2 ft x 2 ft Instructional Tunnel.Variable Mach Number Supersonic Wind Tunnel.Subsonic Low Turbulence 5 ft x 7 ft Wind Tunnel.Below is a list of the wind tunnel facilities that the department offers. The research interests of the group include a wide range of fluid dynamic, combustion and propulsion problems, much of which is based on wind tunnel experimentation. The function of this group is to conduct experimental and theoretical research, teach lecture and lab courses, and to guide PhD theses. These tunnels are run by the Aerodynamics and Propulsion, which consists of a closely integrated group of professors, technicians and students within the Aerospace Department.
The University of Michigan Department of Aerospace Engineering can boast among its many resources ten wind tunnels for instructional and research work. Sequential Undergraduate/Graduate Studies (SUGS) Program.Diversity, Equity & Inclusion Resources.
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