Streamlines_around_a_NACA_0012.svg
Size of this PNG preview of this SVG file:
302 × 164 pixels
.
Other resolutions:
320 × 174 pixels
|
640 × 348 pixels
|
1,024 × 556 pixels
|
1,280 × 695 pixels
|
2,560 × 1,390 pixels
.
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
.
Licensing
|
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. |