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Supersonic Wind Tunnel Test Section Main Content
NASA Center: Glenn Research Center
Image # : C1957-45653
Date : 07/31/1957

Title

Supersonic Wind Tunnel Test Section

Full Description

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

Keywords

Supersonic Wind Tunnel SWT Jet Engine Lewis Flight Propulsion Laboratory Lewis Research Center NACA

Subject Category

Aircraft Propulsion, NACA-GRC-LRC, Wind Tunnels-Interior,

Reference Numbers

  • Center: GRC
  • Center Number: C1957-45653
  • GRIN DataBase Number: GPN-2000-000624

Source Information

  • Creator/Photographer: GRC
  • Original Source: DIGITAL

Image Information ( Copyright Notification )

ResolutionFormatWidth
(Pixels)		Height
(Pixels)		Size
(KBytes)
Thumbnail .jpg 90 72 7
Small .jpg 640 512 165
Medium .jpg 1500 1200 712
Large .jpg 3000 2400 2,167

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