File:Streamlines around a NACA 0012.svg
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Size of this PNG preview of this SVG file: 302 × 164 pixels. Other resolutions: 320 × 174 pixels | 640 × 348 pixels | 1,024 × 556 pixels | 1,280 × 695 pixels | 2,560 × 1,390 pixels.
Original file (SVG file, nominally 302 × 164 pixels, file size: 329 KB)
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. |
| Date | |
| Source | Own work |
| Author | Michael Belisle |
| Other versions | Derivative works of this file: Streamlines around a NACA 0012-hu.svg |
This W3C-unspecified diagram was created with Mathematica.
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
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 04:43, 24 April 2008 | | 302 × 164 (329 KB) | wikimediacommons>Michael Belisle | Reverted to version as of 02:21, 24 April 2008. Decided transparency is OK in the SVG file. |
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