File:Streamlines around a NACA 0012.svg

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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/TimeThumbnailDimensionsUserComment
current01:04, 5 January 2017Thumbnail for version as of 01:04, 5 January 2017302 × 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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