Summary edit

DescriptionStreamlines around a NACA 0012-hu.svg	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	4 February 2012, 11:28 (UTC)
Source	This file was derived from: Streamlines around a NACA 0012.svg:
Author	Streamlines_around_a_NACA_0012.svg: Kaboldy derivative work: Kaboldy (talk)

This is a retouched picture, which means that it has been digitally altered from its original version. Modifications: Szöveg cseréje magyarra. The original can be viewed here: Streamlines around a NACA 0012.svg: . Modifications made by Kaboldy.

Licensing edit

I, the copyright holder of this work, hereby publish it under the following license:

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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: I grant anyone the right to use this work for any purpose, without any conditions, unless such conditions are required by law.

Original upload log edit

This image is a derivative work of the following images:

• File:Streamlines_around_a_NACA_0012.svg licensed with PD-self
  • 2008-04-24T02:43:25Z Michael Belisle 302x164 (336740 Bytes) Reverted to version as of 02:21, 24 April 2008. Decided transparency is OK in the SVG file.
  • 2008-04-24T02:33:39Z Michael Belisle 303x165 (336851 Bytes) Added solid white background.
  • 2008-04-24T02:21:38Z Michael Belisle 302x164 (336740 Bytes) {{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

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