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Engine
Research Building (ERB):
Flow Physics Facilities - Duct Lab
4- by 10-in. Supersonic Wind Tunnel
Duct
Lab Facility Description
Typical programs being conducted in the Duct Lab include the development
and demonstration of supersonic injectors, artificial intelligence
schemes, new laser-based nonintrusive instrumentation systems, and
physical experiments to gain insight into continuous Mach 1.6 to
5.0 (with and without injection), flow physics and explore new technologies.
The facility receives air from atmospheric inlet or by the 40-psig
system, which can be heated by electric heaters. The inlet air is
filtered, enters a 48-in.-diameter plenum, passes through a 2-D
bellmouth, is flow straightened, and then enters the test section.
The walls and roof have interchangeable Plexiglas, optical-glass
(fuse silica/BK-7), or solid-metal windows with rows of pressure
taps. The airflow passes through a fixed diffuser before entering
the altitude exhaust system.
Duct
Lab Special Features
Flow visualization measurements are obtained by both Schlieren
and laser anemometry systems. A supplementary vacuum purge system,
for control of boundary layers, uses two 400-CFM blowers and two
150-CFM mechanical pumps. Data acquisition system is capable of
measuring 372 pressures and 48 temperatures.
Duct
Lab
Facility Capabilities |
| Parameter |
Operating Values |
| Inlet
pressure |
atm
or 40 psig |
| Inlet
airflow |
28
lb/s down to 1.0 lb/s |
| Inlet
air temperature |
400
°F |
| Tunnel
speed |
Mach 1.6,2.0,2.5,3.0,3.5,4.0,4.5, and 5.0 |
| Tunnel
size |
3.84
by 10 in. by 8 ft |
| Altitude
exhaust |
20
to 26 in. hg vac |
| Duct Lab System Instrumentation |
| System |
Number and Type |
| ESP |
384 Ports of +/- 30 PSID
32 Ports of +/- 100 PSID
30 PSIA Ref |
| Escort |
128 Channels
78 Available to the Customer |
| Thermocouples |
21 Type E
27 Type K |
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