File:Streamlines around a NACA 0012.svg

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

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Summary

Description
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.
Date
Source Own work
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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23 April 2008

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Date/TimeDimensionsUserComment
current19:43, 23 April 2008302 × 164 (329 KB)Michael BelisleReverted to version as of 02:21, 24 April 2008. Decided transparency is OK in the SVG file.

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