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Summary
| Description |
English: This figure shows the angle at which a shock will be formed in a 2D supersonic flowfield for various deflection angle. M1 is the upstream Mach number, M2 is the downstream Mach number. |
| Date | |
| Source | Own work (Original text: self-made) |
| Author | -- Myth (Talk) 05:29, 27 October 2007 (UTC) |
| Permission (Reusing this file) |
One is free to use this image. No tags attached. |
Licensing
|
This work has been released into the public domain by its author, Mythealias at English Wikipedia. This applies worldwide. In some countries this may not be legally possible; if so: Mythealias grants anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law. |
Original upload log
The original description page was here. All following user names refer to en.wikipedia.
| Date/Time | Dimensions | User | Comment |
|---|---|---|---|
| 2007-10-27 05:29 | 1078×815× (38726 bytes) | Mythealias | {{Information| |Description = This figure shows the angle at which a [[oblique shock|shock]] will be formed in a 2D supersonic flowfield for various deflection angle. M<sub>1</sub> is the upstream Mach number, M<sub>2</sub> is the downstream Mach number. |
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 18:46, 8 November 2016 | | 1,078 × 815 (38 KB) | Stevenliuyi | Transferred from en.wikipedia |
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