Vibefoil

An interactive airfoil explorer based on XFOIL.

Airfoil Source

NACA Database Custom

Series

4-digit 5-digit 6-series

Max camber (M) 2%

Camber position (P) 40%

Thickness (T) 12%

Boundary Layer Viscous mode

Mach

Re

N_cr

Advanced mode

Angle-of-attack 0°

Start End Inc

Flap

Deflection (+ down) 0.0°

Hinge x/c 0.75

Hinge y/t 0.50

Run case

—

Re—

α—

C_L—

C_M—

C_D—

L/D—

N_cr—