RustFoil vs XFOIL Inviscid Solver Comparison
3 NACA airfoils × 8 angles of attack (-4° to +10°)
Lift Polars
Cp - NACA0012
Cp - NACA2412
Cp - NACA4412
Gamma - NACA0012
Gamma - NACA2412
Gamma - NACA4412
Error Analysis