where:

..\Images\INFO1351_wmf.gif

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

..\Images\INFO1352_wmf.gif

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

..\Images\INFO1353_wmf.gif

is the V-Tail root airfoil lift curve slope.

..\Images\INFO1354_wmf.gif

is the V-Tail tip airfoil lift curve slope.