# 🪂 Laboratori d'envol - 🦈 Shark Nose Airfoil Mofification

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

Choose airfoil.dat: (no file loaded)

#### 🔴 First modification (0 → mod1)

mod1 (%)
deflection1 (%)
n1

#### 🟡 Inlet (mod1 → mod2)

mod2 (%)
(inlet section is not modified directly)

#### 🔵 Second modification (mod1 → mod3)

mod3 (%)
deflection3 (%)
n3
Thickness scale (xcale):
(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`