where:

..\Images\INFO1060_wmf.gif

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

..\Images\INFO1061_wmf.gif

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

..\Images\INFO1062_wmf.gif

is the canard root airfoil lift curve slope.

..\Images\INFO1063_wmf.gif

is the canard tip airfoil lift curve slope.