Wind Tunnel Contacts

Aerial image of Wind Tunnels Nasa Ames

If you would like to do business with the Unitary Plan Wind Tunnel Division at Ames, please visit our contact page.

Other Wind Tunnels at Ames

National Full Scale Aerodynamic Complex: Operated by the U.S. Air Force. The 40-by 80-foot wind tunnel circuit is capable of providing test velocities up to 300 knots. The 80-by 120-foot test section is the world's largest wind tunnel and is capable of velocities up to 100 knots.

7-by 10-foot Wind Tunnel: Closed circuit wind tunnel operated by the U.S. Army. The constant cross-section test section measures 7 feet high by 10 feet wide by 15 feet long. The tunnel has a maximum speed of approximately 355 ft/s.

Image Gallery

Model of ISRP ERA UHB Semi-Span in 11-by 11-ft

Ultra-High Bypass (UHB) Semi-Span Wind Tunnel Model

Forward view of an Ultra-High Bypass (UHB) semi-span model in the Unitary Plan Wind Tunnel 11-by 11-foot test section.

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CEV/LAS 75 model in Unitary Plan Wind Tunnel 11-by 11-foot test section.

5% Scale CEV/LAS 75 Wind Tunnel Model

5% Scale Model of the CEV/LAS 75-AA ACM Jet Interference model in Unitary Plan Wind Tunnel 11-by 11-foot test section.

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Common Research Model in Unitary Plan Wind Tunnel 11-by 11-ft test section.

Common Research Wind Tunnel Model

Common research model in the Unitary Plan Wind Tunnel 11-by 11-foot wind tunnel test section.

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Common research model in the Unitary Plan Wind Tunnel 11-by 11-foot wind tunnel test section.

Common Research Wind Tunnel Model

Common research model in the Unitary Plan Wind Tunnel 11-by 11-foot wind tunnel test section.

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CEV 26 model in Unitary Plan Wind Tunnel 9-by 7-ft test section.

Modified 6% CEV Wind Tunnel Model

Modified 6% Crew Exploration Vehicle (CEV) model in Unitary Plan Wind Tunnel 9-by 7-foot test section.

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Model of TBC-1 in 9-by 7-foot Unitary Plan Wind Tunnel

0.65% Scale QEVC Wind Tunnel Model

0.65% scale quiet experimental validation concept (QEVC) model in the Unitary Plan Wind Tunnel 9-by 7-foot wind tunnel test section.

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Model of LM1 in 9-by 7-ft Supersonic Wind Tunnel at NASA Ames.

Ames Low Boom Wing Tail Wind Tunnel Model

Low boom wing tail model in the Unitary Plan Wind Tunnel 9-by 7-foot wind tunnel test section.

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NASA Ames Wind Tunnel Division

Welcome Message

    NASA Ames Research Center is pleased to offer the services of our premier wind tunnel facilities that have a broad range of proven testing capabilities to customers from industry, DOD, other government agencies, and academia.
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Documentation

Wind Tunnel Related Links

    Aeronautics at NASA: NASA's Aeronautics Research Mission Directorate works to solve challenges that still exist in our nation's air transportation system: air traffic congestion, safety and environmental impacts.

    Aeronautics Test Program (ATP): Created to set the strategic direction for NASA's versatile and comprehensive portfolio of ground and flight test aeronautics research capabilities.

    Ames Balance Calibration Laboratory: Operations at the lab include calibrating balances for the Ames wind tunnels as well as for approved outside projects.