🪂 Laboratori d'envol - 🦈 Shark Nose Airfoil Modification ASN v0.1

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

Choose airfoil.dat: (no file loaded)

x1 (%)

deflection1 (%)

exponent n1

y=k1*x^n1 k1=deflection/(x1^n1)

x2 (%)

(inlet section is modified by second mod)

x3 (%)

deflection3 (%)

exponent n3

y=k3*(x3-x)^n3 k3=deflection/((x3-x1)^n3)

Thickness scale (xcale):

(1.0 = original thickness)

Upper surface First modification Inlet Second modification Unmodified Interpolated points 🖱 Wheel zoom · Drag to pan

Points count → k0 (nose): - k1: - k2: - k3: - Total points: - Interpolated: -

100%