Skip to main content

Inlet and Nozzle Test Facilities

Our inlets and nozzles researchers maintain and operate several test facilities, which are used to:

1'x1' Supersonic Wind Tunnel
1 x 1 Supersonic Wind Tunnel
8'x6' Supersonic Wind Tunnel
8 x 6 Supersonic Wind Tunnel
9'x15' Low Speed Wind Tunnel
9 x 15  Low Speed Wind Tunnel
10' x 10' Abe Silverstein Supersonic Wind Tunnel
10 x 10 Abe Silverstein Supersonic Wind Tunnel
15cm x 15cm Supersonic Wind Tunnel
15 x 15 Supersonic Wind Tunnel
20"x30" Low Speed Wind Tunnel
20 x 30  Low Speed Wind Tunnel
Advanced Nozzle Test Facility
Advanced Nozzle Test Facility
Aero-Acoustic Propulsion Laboratory (Nozzle Acoustic Test Rig)
Aero-Acoustic Propulsion Laboratory (Nozzle Acoustic Test Rig)
Free Jet Facility
Free Jet Facility
Hypersonic Tunnel Facility
Hypersonic Tunnel Facility
Internal Fluid Mechanics Facility
Internal Fluid Mechanics Facility
Propulsion Systems Laboratory
Propulsion Systems Laboratory
Provide feedback