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Supersonic Wind Tunnel Test Section | by NASA on The Commons
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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.

 

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Date: August 31, 1957

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Taken on August 31, 1957