NASA - National Aeronautics and Space Administration
  Follow this link to skip to the main content + Contact NASA
Go

+ GRC Home
+ GRC Facilities Home
8'x6' Supersonic Wind Tunnel
8x6 Home
Quick Facts
Capabilities
Testing Information
Contact Information
Gallery
Layout diagram of the ERB View of the wind tunnel in SE-1
Facility Capabilities
Engine Research Building (ERB):
Turbine Facilities - SE-1
Supersonic/Subsonic Wind Tunnel Facility

SE-1 Facility Description
This facility contains 2 small wind tunnels capable of both subsonic and supersonic operation. The test sections are 36 in.2 and 48 in. long. Tunnel 1 uses atmospheric inlet while tunnel 2 uses 40-psig air that is filtered, heated, and flow conditioned. Both tunnels are equipped with a particle spray seeding system for laser anemometry. Typical instrumentation development projects include an open-beam laser fringe anemometry (LFA) system for unsteady supersonic flow compressor studies, novel heat flux measurement tests, and fiber optic LFA systems development. Tunnel 2 can be used as a supersonic calibration duct for LFA particle dynamics studies. Recent instrumentation development projects include curved diffuser experiments, and the dynamic response of pressure sensitive paint.

SE-1 Special Features
An auxiliary air supply and exhaust piping provides both test sections with suction, blowing, and crossflow capabilities. SE-1 has combustible gas, smoke, and IR flame detectors and a burn wire to allow experimentation with volatile seeding solutions. A focus schlieren system is available for flow-field visualization. A microcomputer is used for research data acquisition and analysis. There are multiple channels of scanivalve pressures and temperatures available.

SE-1
Facility Capabilities
Parameter Operating value
  Tunnel 1 Tunnel 2
Inlet air pressure Ambient 40 psig
Inlet air temperature Ambient 400 oF
Inlet airflow 5 lb/s 10 lb/s
Altitude exhaust 26 in. hg 26 in. hg
Mach no. (max) 2.5 3.0
Test section size 36 in.2 36 in.2

SE-1 System Instrumentation
System Number and Type
ESP 64 Ports of +/- 30 PSID
64 Ports of +/- 5 PSID
15 PSIA Ref
Escort 80 Channels
40 Available to the Customer
Thermocouples 48 Type K
Further Information
Engine Research Building
A large complex with 60 test rigs supporting engine research and development.
+ View the fact sheet (PDF)

Get Adobe Acrobat Reader
 








USA.gov - Your First Click to the US Government

+ Freedom of Information Act
+ NASA Web Privacy Policy and Important Notices

NASA - National Aeronautics and Space Administration
Editor: Sharon Maier, SGT Inc.
NASA Official: Susan Kevdzija
+ Web Curator
+ Contact NASA Glenn
+ Contact NASA
Last Updated: January 24, 2007