Comparing Airfoils

FX 84-W-127

BOEING 106 AIRFOIL

FX 84-W-127 BOEING 106 AIRFOIL
Thickness (%) 12.747 13.030
Camber (%) 3.740 3.316
Trailing Edge Angle (%) 6.085 17.663
Lower Surface Flatness 12.530 13.315
Leading Edge Radius (%) 2.417 3.206
Maximum Lift (CL) 1.324 1.413
Maximum Lift Angle-of-Attack (deg) 10.000 12.000
Maximum Lift-to-drag (L/D) 50.843 61.001
Lift at Maximum Lift-to-drag 1.090 0.733
Angle-of-Attack for Maximum Lift-to-drag (L/D) 7.000 3.000