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Noise Suppression Addition to the 8- by 6-Foot Supersonic Wind Tunnel
Public domain

Noise Suppression Addition to the 8- by 6-Foot Supersonic Wind Tunnel

NASA / GRC · 1950-08-23 · photograph (digital archive)

From the collection of NASA Image and Video Library. Free to download, adapt and use — no permission needed.

About this work

The 8- by 6-Foot Supersonic Wind Tunnel at the National Advisory Committee for Aeronautics (NACA) Lewis Flight Propulsion Laboratory was the largest supersonic wind tunnel in the nation at the time and the only one able to test full-scale engines at supersonic speeds. The 8- by 6 was designed as a non-return and open-throat tunnel.

NASA Image and Video Library’s own description
Credit lineNoise Suppression Addition to the 8- by 6-Foot Supersonic Wind Tunnel. NASA/GRC, 1950-08-23. Public domain. ID: GRC-1950-C-26414.
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