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Solicitation Expired 1 notice 2 documents

Closed Circuit Wind Tunnel PANRSA26P0000033772

Solicitation PANRSA26P0000033772 Copied Notice ID ec3dfc7a63654960bc13915f1e8b9a25 Copied DEPT OF DEFENSE — W6QK ACC-RSA
SAM.gov
Posted
May 01, 2026
Deadline
May 18, 2026
Set-aside
None
NAICS
541715
PSC
6636

Summary

AI-generated · May 02, 2026

Procure a closed-circuit wind tunnel capable of seed-particle operation, using the specified seed substance Bis(2-ethylhexyl) subacute. It must include a 3/8-inch Swagelok bulkhead fitting upstream of the test and transitional sections, achieve up to ~50 m/s, and feature a 101.6 mm x 101.6 mm test section with grooves (6.85 mm thick) placed about 75% of the length from the entrance. The design must allow nozzle-restriction plates to adjust the range and reach an air speed of 0.15 m/s, with turbulence intensity under 1% (defined as the RMS velocity fluctuations divided by the average velocity). The test section must provide at least two sealable ports for instruments of various sizes (including Pitot-static tubes and hotwire anemometers) with specified diameters, with one port 49.5 mm from the inlet centered in the test section and the other offset by 37.5 mm. Sidewalls must be optical-quality glass to minimize laser interference, and the system must accommodate an argon-ion continuous-wave laser (532 nm, 500 mW). The wind tunnel must use a centrifugal fan isolated from the tunnel, driven by a VFD that the operator can control via computer software or manual input, with the interface not reliant on internet or wireless connections and programmable via National Instruments LabVIEW. Any design submitted must demonstrate compliance with the required air speed and turbulence levels through quantitative analysis (e.g., CFD). Delivery is to the indicated shipping address.

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

From Solicitation posted on May 01, 2026

Notice history

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  1. Solicitation LATEST Posted May 01, 2026 View

Details

Solicitation number PANRSA26P0000033772
Notice ID ec3dfc7a63654960bc13915f1e8b9a25
Notice type Solicitation
Product / Service (PSC) 6636
NAICS 541715
Place of performance Redstone Arsenal, Alabama
Archive date Jun 02, 2026

Award Information

Not yet awarded

Contacts

primary
Wanda Little

Email

Phone

secondary
Portia Sampson

Email

Phone

Agency

DEPT OF DEFENSE
DEPT OF THE ARMY
AMC
ACC
ACC-CTRS
ACC RSA
W6QK ACC-RSA

Place of Performance

Redstone Arsenal, Alabama 35898
USA

Dates

Posted May 01, 2026 3 months ago
Last Updated Aug 06, 2026 1 day ago
Due May 18, 2026 2 months ago