File:Airfoil sym10.png
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| Description |
Deutsch: ideale Strömung um ein symmetrisches Profil bei Anstellwinkel 10°
English: ideal airflow around a symmetric airfoil with angle of attack 10° |
| Date | |
| Source | Own work |
| Author | Dfedra unter Verwendung der freien Software https://www.grc.nasa.gov/www/k-12/airplane/foil3.html |
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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. |
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 21:19, 26 December 2021 | | 582 × 422 (36 KB) | Dfedra (talk | contribs) | Stromlinien |
| 19:22, 26 December 2021 |  | 296 × 217 (11 KB) | Dfedra (talk | contribs) | {{Information |Description= berechnetes gepulstes Stromlinienbild um ein symmetrisches Profil bei Anstellwinkel 10° |Source={{own}} |Date= |Author= Dfedra unter Verwendung der freien Software [https://www.grc.nasa.gov/www/k-12/airplane/foil3.html] |Permission= |other_versions= }} |
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