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Engine
Research Building (ERB):
Flow Physics Facilities - CW-17
Free Jet Facility
CW-17
Facility Description
This facility is used to conduct experiments to develop fundamental
understanding of the jet mixing process and to increase jet mixing
efficiency. The mixing process between a jet and surrounding airflow
can be enhanced through use of aerodynamic excitation. CW-17 consists
of a plenum chamber, excitation spool piece, and a nozzle. The 3-ft
diameter by 5-ft long plenum is supplied with either 40- or 125-psig
combustion air. Each of several supply lines are controlled to automatically
set and maintain a desired plenum pressure. A 300-kW electric heater
is available to provide warm airflow. Using adaptor pieces, various
nozzles can be mounted off the plenum chamber. A swirl generator
section can also be installed as part of the plenum. The nozzle,
which exhausts into the room, has an exit diameter of 3.5 in. An
altitude exhaust scoop is available to catch the nozzle flow and
prevent recirculation within the test cell.
CW-17
Special Features
A microphone array can be mounted at the nozzle exit to determine
the output of the acoustic signal. Pitot tubes, hot wire probes,
and microphones can be mounted on an XYZ table in order to survey
the flow field downstream of the exit nozzle. ESCORT D data acquisition,
laser anemometry, and Schlieren systems are also available.
CW-17
Facility Capabilities |
| PARAMETER |
OPERATING
VALUES |
| Supply
airflow, and pressure |
30
lb/s at 40 psig
50
lb/s at 125 psig |
| Inlet
air temperature |
Primary
air 70 to 150 ¡F |
| Altitude
exhaust |
20
to 26 in. hg vacuum |
| CW-17 System Instrumentation |
| System |
Number and Type |
| ESP |
None |
| Escort |
No |
| Laser |
Rayleigh Scattering |
| Other Information |
National Instruments LabVIEW
Hot Wire
Automated Pressure Probe System
Microphones B&K |
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