Comparing Airfoils

AH 95-160

AH 94-145

AH 95-160 AH 94-145
Thickness (%) 15.971 14.546
Camber (%) 5.495 5.495
Trailing Edge Angle (%) 15.107 11.125
Lower Surface Flatness 12.717 17.118
Leading Edge Radius (%) 3.003 2.708
Maximum Lift (CL) 1.860 1.774
Maximum Lift Angle-of-Attack (deg) 15.000 13.500
Maximum Lift-to-drag (L/D) 36.960 40.456
Lift at Maximum Lift-to-drag 0.639 0.668
Angle-of-Attack for Maximum Lift-to-drag (L/D) -0.500 -0.500