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8- by 6-Foot Supersonic Wind Tunnel Data Acquisition

Man with rocket model in wind tunnel.
Mechanical engineer Sam Stein invented a novel fuel injector that changed the course of rocket propulsion. In this photo he works on a model of the Saturn rocket in the 8×6 tunnel in 1960, where he studied the eight engines of the rocket.

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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 8×6, the following ranges are typically provided:

  • 384 ports +/- 15 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 8×6, Escort provides the following:

  • Accuracy for the Neff 400 is +/- 0.05% of range
  • 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 E

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
  • Throughput of 40 million samples per second

Flow Visualization

  • Pressure sensitive paint
  • Conventional Schlieren systems
  • Sheet laser
  • Oil flow visualization
  • High speed video

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

8’x6′ Supersonic Wind Tunnel (8×6) Fact Sheet

GRC Research Facilities
Find out more about the research facilities at NASA’s Glenn Research Center

AETC Supersonic Facilities

AETC Ground Facilities

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Last Updated
Jul 25, 2023
Editor
Lillian Gipson
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