Active Solicitation · DEPT OF DEFENSE

    CLOSED CIRCUIT WIND TUNNEL

    Sol. PANRSA26P0000033772SolicitationREDSTONE ARSENAL, AL
    Open · 4d remaining
    DAYS TO CLOSE
    4
    closes May 18, 2026
    POSTED
    May 1, 2026
    Publication date
    NAICS CODE
    541715
    Primary industry classification
    PSC CODE
    6636
    Product & service classification

    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.

    Contract details

    Solicitation No.
    PANRSA26P0000033772
    Notice Type
    Solicitation
    Posted Date
    May 1, 2026
    Response Deadline
    May 18, 2026
    NAICS Code
    541715AI guide
    PSC / Class Code
    6636
    Issuing Office
    W6QK ACC-RSA
    Primary Contact
    Wanda Little
    State
    AL
    ZIP Code
    35898-5200
    AI Product/Service
    product

    Description

    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 

    Key dates

    1. May 1, 2026Posted Date
    2. May 18, 2026Proposals / Responses Due

    AI search tags

    Frequently asked questions

    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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