Image:Streamlines around a NACA 0012.svg
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Streamlines_around_a_NACA_0012.svg (SVG file, nominally 302 × 164 pixels, file size: 329 KB)
| This is a file from the Wikimedia Commons. The description on its description page there is shown below.
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[edit] Summary
| Description |
English: Potential-flow streamlines around a NACA 0012 airfoil at 11° angle of attack, with upper and lower streamtubes identified. Computed using the Wolfram Demonstrations Project Code Potential Flow over a NACA Four-Digit Airfoil by Richard L. Fearn and beautified in Adobe Illustrator CS3.
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| Source |
self-made |
| Date |
2008-04-23 |
| Author | |
| Permission (Reusing this image) |
see below |
[edit] Licensing
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I, the copyright holder of this work, hereby release it into the public domain. This applies worldwide. In case this is not legally possible: Afrikaans | Alemannisch | Aragonés | العربية | Asturianu | Български | Català | Česky | Cymraeg | Dansk | Deutsch | Eʋegbe | Ελληνικά | English | Español | Esperanto | Euskara | Estremeñu | فارسی | Français | Galego | 한국어 | हिन्दी | Hrvatski | Ido | Bahasa Indonesia | Íslenska | Italiano | עברית | Kurdî / كوردی | Latina | Lietuvių | Latviešu | Magyar | Македонски | Bahasa Melayu | Nederlands | Norsk (bokmål) | Norsk (nynorsk) | 日本語 | Polski | Português | Ripoarisch | Română | Русский | Shqip | Slovenčina | Slovenščina | Српски / Srpski | Svenska | ไทย | Tagalog | Türkçe | Українська | Tiếng Việt | Walon | 中文(简体) | 中文(繁體) | zh-yue-hant | +/- |
File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Dimensions | User | Comment | |
|---|---|---|---|---|
| current | 02:43, 24 April 2008 | 302×164 (329 KB) | Michael Belisle | (Reverted to version as of 02:21, 24 April 2008. Decided transparency is OK in the SVG file.) |
| 02:33, 24 April 2008 | 303×165 (329 KB) | Michael Belisle | (Added solid white background.) | |
| 02:21, 24 April 2008 | 302×164 (329 KB) | Michael Belisle | ({{Information |Description={{en|Streamlines around a NACA 0012 airfoil at 11° angle of attack. Computed using the Wolfram Demonstrations Project Code [[http://demonstrations.wolfram.com/PotentialFlowOverANACAFourDigitAirfoil Potential Flow over a NACA Fo) |
