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679:{{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
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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
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Reverted to version as of 02:21, 24 April 2008. Decided transparency is OK in the SVG file.
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Click on a date/time to view the file as it appeared at that time.
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I, the copyright holder of this work, release this work into the
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copyrighted, dedicated to the public domain by copyright holder
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Théorie du déplacement d'un mobile à voile contre le vent
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by
Richard L. Fearn and beautified in Adobe Illustrator CS3.
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In some countries this may not be legally possible; if so:
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78:(SVG file, nominally 302 × 164 pixels, file size: 329 KB)
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released into the public domain by the copyright holder
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Add a one-line explanation of what this file represents
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Commons is a freely licensed media file repository.
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