INTERACTIVE AIRFOIL ANALYSIS

Interactive airfoil
aerodynamics.

Explore how airfoil shape, angle of attack, and Reynolds number change pressure, skin friction, lift, drag, and flow separation.

02Airfoil Geometry & FlowNACA 2412

MAX CAMBER 2.0%POSITION 40% cTHICKNESS 12%

03Surface Pressure Distribution Upper Lower

C_p

x / c

04Signed Skin-Friction DistributionCƒ ≤ 0 indicates separation Upper Lower

C_f

x / c

Interactive airfoilaerodynamics.