Supersonic Wind Tunnel Test Section
8ft x 6ft Supersonic Wind Tunnel Test-Section showing changes made in Stainless Steel walls with 17 inch inlet model installation. The model is the ACN Nozzle model used for aircraft engines. The Supersonic Wind Tunnel is located in the Lewis Flight Propulsion Laboratory, now John H. Glenn Research Center.
Credit: NASA
Image Number: C-1957-45653
Date: July 31, 1957
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Uploaded on July 31, 2025
Taken on July 31, 1957
Supersonic Wind Tunnel Test Section
8ft x 6ft Supersonic Wind Tunnel Test-Section showing changes made in Stainless Steel walls with 17 inch inlet model installation. The model is the ACN Nozzle model used for aircraft engines. The Supersonic Wind Tunnel is located in the Lewis Flight Propulsion Laboratory, now John H. Glenn Research Center.
Credit: NASA
Image Number: C-1957-45653
Date: July 31, 1957
118,839
views
55
faves
0
comments
Uploaded on July 31, 2025
Taken on July 31, 1957