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Credit goes to webxfoil.com
Example WebXFOIL
Run XFOIL v6.996 in the browser.
Inputs
Airfoil source
NACA 4-digit
Upload points
NACA (4-digit)
Airfoil file
Alpha (deg)
Mach
Reynolds (VISC)
Ncr
Iterations
Viscous
Run XFOIL
Results
CL
--
CD
--
Cm
--
L/D
--
Mode: --
Re: --
Ncr: --
Source: --