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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Summary
| Description |
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 |
Licensing
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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/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 19:00, 29 April 2020 | | 761 × 486 (63 KB) | Hohum | Cropped to subject |
| 18:00, 6 February 2012 |  | 960 × 720 (42 KB) | Wikiflew |
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