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Abe Silverstein Supersonic Wind Tunnel (10x10)
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Quick Facts
Capabilities
Testing Information
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Facility Fact

The 10x10 is specifically designed to test supersonic propulsion components such as
inlets and nozzles, propulsion system integration,and full-scale jet and rocket engines.


C-2000-674: Rocket Based Combined Cycle Rig in the 10x10 C-1994-1394: Bifurcated two-stage supersonic inlet in the 10x10
Facility Capabilities
The 10x10 SWT can be run in aerodynamic (closed-loop) mode or propulsion (open-loop) mode. It can also run at subsonic test conditions in aerodynamic and propulsion modes. Subsonic test conditions range from 5 to 240 kn and altitudes up to 50000 feet.

 
Aerodynamic Mode
Propulsion Mode
Altitude:
(supersonic operation)
50,000 - 154,000 ft
57,000 - 77,000 ft
Reynolds No./ft:
(supersonic operation)
0.12 - 3.4 x 106
2.2 - 2.7 x 106
Mach No.
0 - 0.36 & 2.0 - 3.5
0 - 0.36 & 2.0 - 3.5

Tunnel Support Systems

High Pressure Air
• High-Pressure Air (2600 psig) Storage: 981,000 scf
• Combustion Air: 450 psig at 12 lbm/s (300 °F max. temp)
• Service Air: 125 psig at 2 lbm/s
Hydraulics
• Model hydraulics: 3,000 psig at 75 gpm
Fuels
• Gaseous hydrogen: 1,200 psig at 2 lbm/s
• Gaseous oxygen: 1,500 psig at 23 lbm/s
• Liquid jet fuel: 40 psig 70 gpm
Vacuum/Exhaust
• Model exhaust: 20 lbm/s (2 lines at 10 lbm/s)

Model Support Systems:

  • Lower Strut Assembly: angle of attack range between
    -6.0 and 19.0°, height translation
  • Upper Strut Assembly: angle of attack range between
    -5.0 and 15.0°
  • Gust Plates: Extends local conditions down to Mach Number 1.5 or up to Mach Number 4.1

Model Data and Control System Capabilities

  • Pressure Systems
    ESP is an off the shelf electronically scanned pressure system. The system consists of numerous 32 port, rack mounted modules from +/-2.5 PSID to +500 PSID, located outside the test chamber. Each module has a check pressure to assure the module is performing correctly and can be calibrated in place using up to 5 highly accurate calibration pressures to maintain the overall system accuracy of +/-0.05% of range. This calibration is performed every 2 hours.
    For the 10x10, the following ranges are typically provided:
    • 768 ports +/- 15 PSID Barometric Ref
    • 192 ports +/- 30 PSID Barometric Ref

  • Data System - Escort
    Escort, the steady state data acquisition system, uses a DEC Alpha microprocessor to provide:
    • An X window based system
    • Real time on-line acquisition of analog signals
    • Conversion of raw 10Hz filtered digitized Neff data to engineering units
    • Computed performance calculations, which can be displayed in a variety of tabular and graphical formats.
    • Limit checking on all selected channels
    • 1 second update rate

    Escort can stand alone to meet all secure test requirements or it can be connected to a central processing cluster, which facilitates software application development, downloading of software, uploading and storage of facility tables, post processing of data and transmitting of data to a data collector for archival storage.
    For the 10x10, Escort provides the following:
    • Accuracy for the Neff 400 is +/- 0.05% of range, while the accuracy for the Neff 600 is +/- 0.02% of range +2µv
    • Off-site access to data
    • 240 channels of which 220 are available for the test article
    • 48 temperatures from type J
    • 48 temperatures from type T
    • 48 temperatures from type R
  • Dynamic Data System
    The transient data system provides multi-channel high speed digitized acquisition of rapidly changing cyclic on non-periodic impulse type events. The system consists of:
    • A front end Precision Filter amplifiers with elliptical (132 dB/oct) or linear phase (46 dB/oct) anti aliasing filters (132 dB per octave)
    • Off loading the data by FTPing, in near real time, to either our computer or yours for post processing
    • 16 Bit A/D per channel (sample and hold)
    • Throughput of 40 million samples per second

  • Flow Visualization
    • Pressure sensitive paint
    • Both conventional and focused Schlerien systems
    • Sheet laser
    • Oil flow visualization
    • High speed video - up to 1000 full screen frames/s

  • Test Article Controls
    • Digital model control system with graphical interface
    • Automated test article sequencing system

  • Remote Access Control Room
    • Real-time remote access to all data
    • Video conferencing in real time
    • Workstations supplied for remote site
    • Secure network connections provided
Further Information
Abe Silverstein Supersonic Wind Tunnel (10x10)
The largest and fastest wind tunnel at NASA Glenn
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Last Updated: November 5, 2007