Active Solicitation · DEPT OF DEFENSE
AI Summary
The Department of Defense is soliciting proposals for the procurement of a closed-circuit wind tunnel. The wind tunnel must meet specific operational requirements, including a maximum speed of 50 meters per second and specialized fittings for various instruments. Proposals must demonstrate compliance with air speed and turbulence specifications through quantitative analysis. Delivery is required at Redstone Arsenal, AL.
Purchase Description
Procurement of Closed-Circuit Wind Tunnel
Requirements:
• This wind tunnel must be a closed circuit, as the operation of an LDV system
requires seed particles to be added to the air stream – in this case, a substance
called Bis(2-ethylhexyl) subacute. The wind tunnel thus needs to be fitted with a
3/8-inch Swagelok bulkhead fitting placed upstream of the test and transitional
sections.
• This wind tunnel must have a maximum operating speed of approximately 50
meters per second (~9900 feet per minute). The test section walls must have 6.85
millimeter (0.27-inch)-thick grooves placed at approximately 75 percent of the total
length of the test section as measured from the entrance in which specialized
nozzle restriction plates can be affixed to adjust the operating range and achieve
an air speed of 0.15 meters per second (~30 feet per minute). The typical
turbulence intensity across this operating range must be less than 1 percent, where
turbulence intensity is defined as the root-mean-square of velocity fluctuations
divided by the average test section velocity.
• This wind tunnel must have a test section size of 101.6 millimeters by 101.6
millimeters (~4 inches by 4 inches). Test section length can vary if the design
meets the following requirements: The test section must have at least two sealable
ports or fittings for the insertion of instruments of various sizes, such as Pitot-static
tubes and hotwire anemometers. These ports or fittings must accommodate the
following instrument diameters: 4.3 mm (~0.188 in); 6.3 mm (0.25 in); 7.9 mm
(0.313 in); 9.5 mm (0.375 in); 10.1 mm (0.4 in); 12.7 mm (0.5 in); 15.9 mm (0.625
in). One port must be located 49.5 mm (1.95 in) from the inlet, centered into the
test section; the other port should be offset from this port by 37.5 mm (1.47 in).
Additionally, the test section sidewalls must be made of optical-quality glass to
minimize interference with laser propagation. The argon-ion continuous-wave laser
used in this application has a max wavelength of 532 nanometers and 500
milliwatts output power.
• The wind tunnel must have a centrifugal fan design. The fan should be isolated
from the rest of the tunnel system to minimize vibration. The fan must be controlled
by a variable-frequency drive (VFD) connected to a motor of appropriate size and
power to meet the air speed requirements listed above. The VFD must be
implemented such that an operator could use computer software or manual input to
control the drive and automate its function. The computer-VFD interface must not
rely on internet or wireless connections, such as Bluetooth or WiFi. This interface
must be programmable via National Instruments’ LabVIEW software.
• Any design submitted must be shown to meet the specific air speed and
turbulence requirements listed above through a quantitative analysis, such as by
computational fluid dynamics (CFD) simulations or other appropriate methods.
1.0 Delivery Requirements
Shipping Address: U.S. Army TMDE Activity, Attn: Michael Tyler, Building 5435,
Redstone Arsenal, AL 35898
CLOSED CIRCUIT WIND TUNNEL is a federal acquisition solicitation issued by DEPT OF DEFENSE. Review the full description, attachments, and submission requirements on SamSearch before the response deadline.
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