File:Inlet shock waves at Mach 2.jpg
No higher resolution available.
Inlet_shock_waves_at_Mach_2.jpg (761 × 486 pixels, file size: 63 KB, MIME type: image/jpeg)
 | This is a file from the Wikimedia Commons. Information from its description page there is shown below. Commons is a freely licensed media file repository. You can help. |
 |
This is a retouched picture, which means that it has been digitally altered from its original version.
|
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
|
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.) |  |
 |
Warnings:
|
File history
Click on a date/time to view the file as it appeared at that time.
| 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 |
File usage
The following 4 pages use this file:
Global file usage
The following other wikis use this file:
- Usage on he.wikipedia.org
- Usage on ro.wikipedia.org