EMX 07 LA 2573a NLF 1015 NACA 63412

Airfoil Aerodynamic comparison

AirfoilEMX 07LA 2573aNACA 63412NLF 1015

Thickness (%)9.9113.71215

Camber (%)2.543.22.24.8

Trailling edge angle (%)789.6

Lower Surface flatness (%)56.163.365.7

Leading edge radius (%)3.21.52.2

Max CL1.1051.341.311.096

Max CL angle (deg)10121312

Max L/D66.6969.2087.4380.78

Max L/D angle (deg)71065

Stall Angle (deg)1012612

x_max thickness (%)29.628.734.939.8

x_max chamber (%)20.726.15058.3