Lateral Acceleration Imparted to the Aircraft as a Result of a Unit Change in Vertical Tail Incidence

..\Images\INFO1457_wmf.gif

where:

..\Images\INFO1458_wmf.gif

is the dynamic pressure.

..\Images\INFO1459_wmf.gif

is the reference area.

..\Images\INFO1460_wmf.gif

is the reference span.

..\Images\INFO1461_wmf.gif

is the mass.

..\Images\INFO1462_wmf.gif

is the rolling moment of inertia.

..\Images\INFO1463_wmf.gif

is the yawing moment of inertia.