where:

..\Images\INFO1102_wmf.gif

is the wing sectional lift curve slope at the wing mean geometric chord at zero-Mach and Re = 6.0x10^6.

..\Images\INFO1103_wmf.gif

is the Y-distance between the wing mean geometric chord and the wing root chord in terms of wing half span.

..\Images\INFO1104_wmf.gif

is the wing root airfoil lift curve slope.

..\Images\INFO1105_wmf.gif

is the wing tip airfoil lift curve slope.