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File:Streamlines around a NACA 0012.svg

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38: 202: 249: 90: 662: 632: 602: 679:{{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 147:
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
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Théorie du déplacement d'un mobile à voile contre le vent
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File:Streamlines around a NACA 0012.svg
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Potential Flow over a NACA Four-Digit Airfoil
Michael Belisle
Streamlines around a NACA 0012-hu.svg

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