File:Streamlines around a NACA 0012.svg
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![File:Streamlines around a NACA 0012.svg](/w/images/thumb/b/b3/Streamlines_around_a_NACA_0012.svg/302px-Streamlines_around_a_NACA_0012.svg.png)
Size of this PNG preview of this SVG file: 302 × 164 pixels. Other resolution: 320 × 174 pixels.
Original file (SVG file, nominally 302 × 164 pixels, file size: 329 KB)
Summary
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 <a rel="nofollow" class="external text" href="http://demonstrations.wolfram.com/PotentialFlowOverANACAFourDigitAirfoil">Potential Flow over a NACA Four-Digit Airfoil</a> by Richard L. Fearn and beautified in Adobe Illustrator CS3.
Licensing
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File history
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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current | 01:04, 5 January 2017 | ![]() | 302 × 164 (329 KB) | 127.0.0.1 (talk) | 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 <a rel="nofollow" class="external text" href="http://demonstrations.wolfram.com/PotentialFlowOverANACAFourDigitAirfoil">Potential Flow over a NACA Four-Digit Airfoil</a> by Richard L. Fearn and beautified in Adobe Illustrator CS3. |
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