Public domain
ARC-1965-A-35705
From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.
About this work
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.
NASA Image and Video Library’s own descriptionSubjects
Credit lineARC-1965-A-35705. NASA/ARC, 1965-10-22. Public domain. ID: ARC-1965-A-35705.
