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ARC-1965-A-35705
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ARC-1965-A-35705

N-222; 2 x 2ft Transonic Wind Tunnel is a closed return, variable-density tunnel equipped with an adjustable flexible-wall nozzle and a slotted test section. Airflow is produced by a two-stage, axial-flow compressor powered by four, variable-speed induction motors mounted in tandem, delivering a total of 4,000 horsepower. For conventional, steady-state testing models are generally supported on a sting. Internal, strain-gage balances are used for measuring forces and moments. This facility is also used for panel-flutter testing (one test-section wall is replaced with another containing the test specimen.

Date
1965-10-22
Collection
ARC
Archive
NASA Image and Video Library
Type
photograph

Public domainsafest

Reason: a NASA work: not copyrighted in the United States.

Read from: NASA media usage guidelines: NASA material is not copyrighted in the US unless noted; no third-party credit or mark found.

Credit line

"ARC-1965-A-35705" (1965-10-22). NASA/ARC. Public domain. https://images.nasa.gov/details/ARC-1965-A-35705

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Need photos for a whole script? Add Find Any Photo to Claude and ask for this one by its id: 90218.

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