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File:Streamlines around a NACA 0012.svg

Original file (SVG file, nominally 302 × 164 pixels, file size: 329 KB)


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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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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.

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Date/TimeThumbnailDimensionsUserComment
current02:43, 24 April 2008Thumbnail for version as of 02:43, 24 April 2008302 × 164 (329 KB)Michael BelisleReverted to version as of 02:21, 24 April 2008. Decided transparency is OK in the SVG file.
02:33, 24 April 2008Thumbnail for version as of 02:33, 24 April 2008303 × 165 (329 KB)Michael BelisleAdded solid white background.
02:21, 24 April 2008Thumbnail for version as of 02:21, 24 April 2008302 × 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

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