File:Inlet shock waves at Mach 2.jpg

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Inlet_shock_waves_at_Mach_2.jpg ‎(761 × 486 pixels, file size: 63 KB, MIME type: image/jpeg)

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English: Shock wave structure about a supersonic axisymmetric cone inlet. Left image shows unstarted flow. Right image shows started flow.
Date
Source NASA document ID: C-1955-37520 https://archive.org/details/C-1955-37520
Author NASA Glenn Research Center

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Public domain This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)
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Date/TimeThumbnailDimensionsUserComment
current19:00, 29 April 2020Thumbnail for version as of 19:00, 29 April 2020761 × 486 (63 KB)Hohum (talk | contribs)Cropped to subject
18:00, 6 February 2012Thumbnail for version as of 18:00, 6 February 2012960 × 720 (42 KB)Wikiflew (talk | contribs)

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