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Engine
Research Building (ERB):
Heat Transfer Facilities - W-5A-3
3-D Subsonic Tunnel
W-5A-3
Facility Description
This
test rig is one of three in cell W-5A. The turbine vane cascade
is used to obtain aerodynamic and heat transfer data for turbine
van geometries. It is a three van -four passage high aspect ratio
cascade. Tests are conducted over a wide range of Reynolds and Mach
numbers. Inlet air is supplied by the 40 psig combustion air system.
Air exhausts to the low pressure altitude exhaust system at pressures
as low as 2 psia. Blown air turbulence grids are used to provide
high and uniform turbulence at the inlet. Survey slots are located
upstream and downstream of the vanes. Infrared (IR) camera access
is available from three access ports using IR transparent windows.
Escort-D (a data collection system) is used for low frequency data
acquisition. IR camera image data is acquired using a PC based system.
Hot wire data are also acquired using a PC based system.
W-5A-3
Facility Capabilities |
| Parameter |
Operating Value |
| Inlet
air pressure |
40
psig |
| Inlet
airflow |
60
lb/s
(Note: Vane cascade will not accommodate 60
LB/s. However, combustor simulator tests in the upstream section
have used 60 LB/s when the test vanes were removed) |
| Inlet
air temperature |
amb |
| Altitude
exhaust |
20-26
in. hg |
| W-5A-3 System Instrumentation |
| System |
Number and Type |
| ESP |
192 Ports of +/- 15 PSID, 17 PSIA Ref
32 Ports of +/- 5 PSID, Barometric Ref |
| Escort |
128 Channels
92 Available to the Customer |
| Thermocouples |
96 Type E
48 Type K |
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