Voxel

a Human Engine Labs project
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Presets

NACA Airfoil

NACA 2412
6°
-18°22°
M 0.78
subsonicsupersonic

Flow Parameters

0.10 m/s
0.512.00
0.55
01.00

Visualization

Streamlines
Particles
Pressure Contours
Mach Waves

Simulation

1.00x
0.25x4x

Statistics

FPS
Reynolds Number
Grid200 × 100
Iterations0
airfoil Geometry
SPEED (m/s)
0.100.080.050.030.00
Left click = draw obstacle | Right click = erase | Space = play / pause
T = 0.00 s
Step 0
Live Insights
Paused · 0 fps

Avg. Velocity

0.04 m/s

Max. Velocity

0.10 m/s

Pressure Drop

0.0 Pa

Drag Coefficient

0.00

Speed Distribution

0.00.51.0

Speed (m/s)

Layers

Velocity Field
⋮⋮
Streamlines
Particles
Pressure Contours
Mach Waves