The Low Speed Aeroacoustics Wind Tunnel (LSAWT) simulates realistic flow conditions of commercial and military aircraft engine exhausts and focuses on developing noise reduction techniques and investigating complex flow interactions.
Transonic Dynamics Tunnel (TDT) The Transonic Dynamics Tunnel (TDT) provides a unique national testing capability for identifying, understanding, and developing solutions for complex aeroelastic and non-aeroelastic phenomena configurations. + Learn More
National Transonic Facility (NTF) The world’s largest pressurized cryogenic wind tunnel, the National Transonic Facility (NTF), possesses unique capabilities to duplicate actual flight conditions. + Learn More
0.3-Meter Transonic Cryogenic Tunnel (0.3-M TCT) Reynolds numbers up to 100 million per foot can be attained in the cryogenic mode of operation in the 0.3-Meter Transonic Cryogenic Tunnel (0.3-M TCT). + Learn More
at a Glance
Learn about the capabilities of our facilities and decide which facility best meets your needs + View PDF Document