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X-59 model inside the 8x6 supersonic wind tunnel.
1.79 percent scale model of a future concept supersonic aircraft built by The Boeing Company in the 8x6 wind tunnel.
Inside the 8x6 Supersonic Wind Tunnel, a female engineer is placing trip dots on the leading edge of the wing.

8- by 6-Foot Supersonic Wind Tunnel Facility

The 8′ x 6′ Supersonic Wind Tunnel operates either in an aerodynamic closed-loop cycle, testing aerodynamic performance, or in a propulsion open-loop cycle that tests live fuel burning engines and models.

Learn More About the 8- by 6-Foot Supersonic Wind Tunnel about 8- by 6-Foot Supersonic Wind Tunnel Facility

Focus Areas and Capabilities

Learn more about the specifications and capabilities of this facility.

Black and gold image showing a silhouette of a man inside a wind tunnel.

Characteristics

The test section is large enough to accommodate large-scale models and full-size aircraft components.

man silhouetted in a blue lit wind tunnel holding an aircraft model for setup

Quick Facts

The 10×10 SWT was specifically designed to test supersonic propulsion components such as inlets, nozzles, and full-scale jet and rocket engines.

Man with rocket model in wind tunnel.

Data Acquisition

Real-time remote access to data through secure network connections.

Virtual Tour

The 8 x 6 Supersonic Wind Tunnel is a world-class facility that provides researchers with the opportunity to explore higher speed regions of flight.

Learn More about Virtual Tour
Cutaway drawing of the 8x6 wind tunnel.

Contact Information

8’x6′ Supersonic Wind Tunnel
Facility Manager: Richard Bozak
(216) 433-5160

NASA Glenn Research Center
21000 Brookpark Rd.
Cleveland, Ohio 44135
(216) 433-4000

Fact Sheet

Actively involved in research and development testing for over 60 years, the 8- by 6-Foot Supersonic Wind Tunnel is NASA’s only transonic-propulsion wind tunnel, serving industry, academia, and NASA’s own community of aerospace researchers.

The facility operates either in an aerodynamic closed-loop cycle, testing aerodynamic performance models, or in a propulsion open-loop cycle that tests live fuel-burning engines and models.

Read the 8- by 6-Foot Supersonic Wind Tunnel Fact Sheet
Two men working on the Aero Acoustic test.
Aero Acoustic Test of Launch Abort Rocket System (LAS) for OrionInstallation into the 8×6 foot Supersonic Wind Tunnel (SWT).
NASA