NACA Airfoil Flow Simulator

Controls

NACA 4-digit Code

Enter a 4-digit NACA code (e.g., 2412, 0012)

Angle of Attack: 5°

Wind Speed: 10 m/s

Flow Visualization

Performance Metrics

Lift Coefficient (C_L):

0.75

Drag Coefficient (C_D):

0.02

Reynolds Number:

6.7×10⁵

FPS:

Pressure Gradient

Low High

About NACA Airfoils

The NACA 4-digit series defines airfoil geometry using 4 digits (e.g., 2412): [?] First digit: maximum camber (% of chord)
Second digit: camber position (tenths of chord)
Last two digits: maximum thickness (% of chord)

Controls

Performance Metrics

About NACA Airfoils

Lift Coefficient vs Angle of Attack