Comparing Airfoils

NASA/LANGLEY RC08-64C AIRFOIL

GIII BL126 AIRFOIL

NASA/LANGLEY RC08-64C AIRFOIL GIII BL126 AIRFOIL
Thickness (%) 8.000 8.758
Camber (%) 1.000 1.184
Trailing Edge Angle (%) 17.558 12.236
Lower Surface Flatness 10.814 10.128
Leading Edge Radius (%) 1.804 1.854
Maximum Lift (CL) 0.711 0.757
Maximum Lift Angle-of-Attack (deg) 12.000 11.500
Maximum Lift-to-drag (L/D) 18.841 37.508
Lift at Maximum Lift-to-drag 0.273 0.551
Angle-of-Attack for Maximum Lift-to-drag (L/D) 1.500 4.000