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1×1 Supersonic Wind Tunnel

The 1- by 1-Foot Supersonic Wind Tunnel (1×1) specializes in conducting fundamental research in supersonic and hypersonic fluid mechanics, supersonic-vehicle-focused research and detailed benchmark quality experiments for computational fluid dynamics (CFD) code validation.

Facility Overview

Exhaust Nozzle Plume Effects on Sonic Boom Hardware
Advanced nozzle concepts at NASA’s Glenn Research Center, exhaust nozzle plume effects on sonic boom hardware in the 1- by 1-Foot Supersonic Wind Tunnel (1×1).

The 1×1 is a facility located in the Engine Research Building (ERB) at NASA’s Glenn Research Center in Cleveland, Ohio. This facility is used to conduct fundamental research in supersonic and hypersonic fluid mechanics, supersonic-vehicle-focused research and detailed benchmark quality experiments for CFD code validation.

The tunnel can provide continuous operation at 10 discrete airspeeds from Mach 1.3 to 6.0 by using an appropriate fixed-area contoured nozzle block upstream of the test section.

A number of specialized support systems are available to meet the research customer’s needs such as auxiliary bleed, model hydraulics, and probe actuation systems. Machine shop equipment is also available to accommodate model build-up and changes. The 1×1 uses several different types of experimental research tools that are invaluable to fundamental studies.

Inlet Mode Transition Mach 4
Inlet mode transition (IMX) Mach 4 inlet model mounted in the 1- by 1-Foot Supersonic Wind Tunnel (1×1).

The facility has qualitative and quantitative flow visualization capabilities such as Schlieren imaging system, particle image velocimetry (PIV), a sheet-laser system, blue Zyglo (Magnaflux) and black lights, two-component laser Doppler velocimetry (LDV), and trace gas detection.

The equipment in the 1×1 is complemented by staff experienced in supersonic test hardware and experimentation. With its capabilities, expert staff, and efficiency, the 1×1 offers the supersonic research community an excellent low-cost tool for fundamental small-scale research.

Quick Facts

The 1×1 is used to conduct fundamental research in supersonic and hypersonic fluid mechanics. It is also used for supersonic-vehicle-focused research and detailed benchmark quality experiments for CFD code validation.

Name: 1- by 1-Foot Supersonic Wind Tunnel (1×1 )
Mach no.: 1.3 to 6.0 (10 discrete airspeeds)
Test section: 1 foot high by 1 foot wide by 8 feet long

Capabilities

The 1×1 provides customers with a facility capable of conducting fundamental research in supersonic and hypersonic fluid mechanics.

Characteristics and Performance

Flow Visualization

Support Systems

Research Instrumentation and Data Systems

Contact

1×1 Supersonic Wind Tunnel (1×1)
Facility Manager: Gwynn Severt
216-433-8310
Gwynn.A.Severt@nasa.gov

Test Facility Management Branch
Branch Chief: Deborah L. Waters
216-433-5371
deborah.l.waters@nasa.gov

Using Our Facilities

NASA’s Glenn Research Center provides ground test facilities to industry, government, and academia. If you are considering testing in one of our facilities or would like further information about a specific facility or capability, please let us know.

Did you test in one of our facilities? Let us know about your experience by participating in our customer facility evaluation survey.

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