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Summary
| Description |
English: Pressure coefficient of NACA 0012 at 11° angle of attack. |
| Date | |
| Source | Computed using Xfoil 6.96. |
| Author | Michael Belisle (talk) |
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 | 20:54, 21 January 2009 | | 765 × 581 (23 KB) | Michael Belisle | {{Information |Description=Pressure coefficient of NACA 0012 at 11° angle of attack. |Source=Computed using [XFoil http://web.mit.edu/drela/Public/web/xfoil/]. |Date= |Author=~~~ |other_versions= }} |
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