🪂 Laboratori d'envol - 🦈 Shark Nose Airfoil Mofification

Convert any standard .dat airfoil into a shark-nose profile using two generic parabolas.

(no file loaded)

🔴 First modification (0 → mod1)

🟡 Inlet (mod1 → mod2)

(inlet section is not modified directly)

🔵 Second modification (mod1 → mod3)

(1.0 = original thickness)

Modified airfoil preview

Upper surface First modification Inlet Second modification Unmodified Interpolated points 🖱 Wheel zoom · Drag to pan
k0 (nose): - k1: - k2: - k3: - Total points: - Interpolated: -
100%

Generated airfoil-sn.dat