| Display title | Physics:Normal shock tables |
| Default sort key | Normal shock tables |
| Page length (in bytes) | 29,228 |
| Namespace ID | 3020 |
| Namespace | Physics |
| Page ID | 405296 |
| Page content language | en - English |
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| Page creator | imported>Scavis2 |
| Date of page creation | 04:36, 5 February 2024 |
| Latest editor | imported>Scavis2 |
| Date of latest edit | 04:36, 5 February 2024 |
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Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | In aerodynamics, the normal shock tables are a series of tabulated data listing the various properties before and after the occurrence of a normal shock wave. With a given upstream Mach number, the post-shock Mach number can be calculated along with the pressure, density, temperature, and stagnation... |
