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Deskripsyon
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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Gigikanan Kaugalingong trabaho
Tagsulat 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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Public domain 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:
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23 Abril 2008

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Petsa/TaknaThumbnailMga dimensyonTiggamitKomento
kasamtangan02:43, 24 Abril 2008Thumbnail sa bersyon sa 02:43, 24 Abril 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 Abril 2008Thumbnail sa bersyon sa 02:33, 24 Abril 2008303 × 165 (329 KB)Michael BelisleAdded solid white background.
02:21, 24 Abril 2008Thumbnail sa bersyon sa 02:21, 24 Abril 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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