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Summary
| Description | Shock polar of pressure ratio against flow deflection angle for M = 1.8 and γ = 1.4. |
| Source | Own work |
| Author | Alphanumeric Sheep Pig |
Licensing
|
I, the copyright holder of this work, release this work into the public domain. This applies worldwide. In some countries this may not be legally possible; if so: I grant anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law. |
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 11:03, 7 June 2010 | | 392 × 421 (27 KB) | Alphanumeric Sheep Pig | Reduced size |
| 10:48, 7 June 2010 |  | 546 × 570 (27 KB) | Alphanumeric Sheep Pig | {{Information |Description= Shock polar of pressure ratio against flow deflection angle for M = 1.8 and γ = 1.4. |Source={{own}} |Date= |Author= Alphanumeric Sheep Pig |Permission= |other_versions= }} |
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