Airfoil Aerodynamics Simulator

See how angle of attack and configuration affect lift and drag. As AOA increases, both lift and drag increase — but beyond a critical angle, the wing stalls and lift drops sharply. Drag up or down on the airfoil to explore.

Flow Status

Boundary Layer
Attached Flow
NORMAL

Configuration

Slats
Icing
Flap Setting

Aircraft Type

Aerodynamic Data

AOA
0.0°
Cl
0.00
Cd
0.000
L/D Ratio
0.0
L/D Max
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