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 A view inside CE-5B-1
Facility Capabilities
Engine Research Building (ERB):
Combustor Facilities - CE-5B-1
Sector Combustor Studies Test Facility
(Laser Diagnostics)

CE-5B-1 Facility Description
Combustion studies are conducted in this two-test position facility specifically in support of the NOx reduction research for the HSR program and the AST program. CE-5B-1 is large enough to test sector arrangements of injector elements, to include interactions of the elements, and single larger elements. The facility receives filtered combustion air from the 450 psig system. The air is heated in a 1100 deg F non-vitiated heater at flows up to 20 lb/s, which can be valved to either test stand. The airflow passes through the test section, is water spray quenched and then discharged to the altitude exhaust system or the atmospheric exhaust system. The facility preheater consists of a heat exchanger fired by four J-47 burner cans using natural gas for a fuel and the 40 psig combustion air. The research hardware uses ASTM Jet-A, JP-5, or JP-8 as a fuel.

CE-5 Facility Graphic
CE-5 Facility Graphic (click for enlargement)

CE-5B-1 Special Features
In addition to inlet and exit rakes and standard instrumentation, water-cooled gas sampling rakes are in the downstream section. Particulate measurements are taken at the exit of the combustion section. Optical accessibility of the combustor section allows never before possible nonintrusive laser-based diagnostics of the reacting and non reacting flowfield. These include such techniques as planar laser-induced fluorescence (PLIF)imaging, Planar Mie scattering, Phase/Doppler particle analysis (PDPA), focussed Schlieren imaging and light sheet photography. Both rigs share the gas analysis, particulate analysis, and diagnostics equipment.

CE-5B Facility Capabilities
(typical of both rigs)
Parameter Operating Value
Inlet air supply pressure 450 psig
Inlet air temperature 100°F, preheated to 350-1350°F
Inlet airflow
   Stand 1
   Stand 2
20 lb/s (available)
0.5 to 12.0 pps
0.5 to 5.0 pps
Exhaust Atm or 20-26 in. Hg
Rig pressure without windows
   Stand 1
   Stand 2

275 psig
400 psig
Rig pressure with windows
   Stand 1
   Stand 2

250 psig
275 psig
Rig Fuel (JP-8) flow 7 gpm @ 400-900 psig
(three legs per stand)
Window cooling GN2 (4 legs) 0.125 to 0.5 pps (each leg)
Cooling water 150 gpm @ 460 psig
250 gpm @ 395 psig
50 gpm @ 350 psig
15 gpm @ 55 psig

CE-5B-1 System Instrumentation
System Number and Type
ESP 96 Ports of + 500 PSID
Barometric Ref
Escort 240 Channels
154 Available to the Customer
Thermocouples 156 Type K
24 Type B
12 Type W5
24 Type R
Gas Analyzers HC – 1000 ppm 1% & 5%
CO – 2000 ppm 5%
CO2 – 5%, 10%, 20%
O2 – 25%
NO – 100 ppm, 1000 ppm 1%
NOx –
Laser PLIF, Raman

CE-5B-2 System Instrumentation
System Number and Type
ESP 96 Ports of + 500 PSID
Barometric Ref
Escort 240 Channels
154 Available to the Customer
Thermocouples 148 Type K
24 Type B
48 Type R
Gas Analyzers HC – 1000 ppm 1% & 5%
CO – 2000 ppm 5%
CO2 – 5%, 10%, 20%
O2 – 25%
NO – 100 ppm, 1000 ppm 1%
NOx –
Laser PLIF, Raman
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: Linda C. Elonen-Wright
+ Web Curator
+ Contact NASA Glenn
+ Contact NASA
Last Updated: January 24, 2007