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This Solicitation opportunity from Department Of Defense was posted on May 1, 2026. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

Closed Circuit Wind Tunnel

Awarded
PANRSA26P0000033772Federal

Contract Overview

Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

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The U.S. Army TMDE Activity is seeking a closed-circuit wind tunnel designed for integration with a Laser Doppler Velocimetry system at the Primary Standards Laboratory in Redstone Arsenal, Alabama. The system must operate with a maximum airspeed of 50 meters per second and be capable of achieving a minimum speed of 0.15 meters per second via interchangeable nozzle plates inserted into 6.85-millimeter grooves located at 75 percent of the test section length. Turbulence intensity across the entire speed range must remain below 1 percent, defined as the root-mean-square of velocity fluctuations divided by the average velocity. The test section must measure 101.6 millimeters square and feature optical-quality glass sidewalls to ensure compatibility with a 532-nanometer, 500-milliwatt argon-ion continuous-wave laser. Two sealable instrument ports are required, accommodating tool diameters ranging from 4.3 to 15.9 millimeters, with one located 49.5 millimeters from the inlet and the other offset by 37.5 millimeters. A 3/8-inch Swagelok bulkhead fitting must be installed upstream of the test section to introduce Bis(2-ethylhexyl) sebacate seed particles into the airflow. The wind tunnel must utilize a centrifugal fan with vibration isolation, controlled by a variable-frequency drive programmable exclusively through National Instruments LabVIEW software without any internet, Bluetooth, or Wi-Fi connectivity. All design claims must be substantiated through quantitative analysis such as computational fluid dynamics simulations. The unit must be delivered to U.S. Army TMDE Activity, Building 5435, Redstone Arsenal, Alabama, with acceptance performed by government personnel at the site based on strict compliance with all technical specifications. No pricing, contract type, or cost data is provided in the solicitation, and no formal clauses, evaluation factors, or packaging requirements are included, suggesting a technical performance-based procurement likely evaluated under a lowest price technically acceptable approach. The solicitation was posted on May 1, 2026, with proposals due by May 18, 2026, under NAICS code 541715.

General Info

Procure closed-circuit wind tunnel with LDV support, low turbulence, precise speed control, and optical testing.

NAICS

541715 - Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)

Place of Performance

Redstone Arsenal, AL, 35898, USA

Set-Aside

NONE

Documents

2

Purchase Description for Closed-Circuit Wind Tunnel

PDF, High priority: read this firstpurchase-description
High

Justification and Approval for Closed-Circuit Wind Tunnel Purchase

PDF, Low priorityjustification-and-approval
Low

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Timeline

PhaseAwarded
Posted

Solicitation

Awarded

Contract was awarded

Submission Closed

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Organization & Contact Information

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AgencyDepartment Of Defense → W6QK Acc-Rsa
Contacts2 people available
OfficeREDSTONE ARSENAL, AL, 35898-5200, USA
Office AddressREDSTONE ARSENAL, AL, 35898-5200, USA

Full Description

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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 

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