Vertical Acceleration Imparted to the Aircraft as a Result of a Unit Change in V-Tail Incidence Angle

..\Images\INFO1333_wmf.gif

where:

..\Images\INFO1334_wmf.gif

is the dynamic pressure.

..\Images\INFO1335_wmf.gif

is the reference area.

..\Images\INFO1336_wmf.gif

is the reference span.

..\Images\INFO1337_wmf.gif

is the mass.

..\Images\INFO1338_wmf.gif

is the rolling moment of inertia.

..\Images\INFO1339_wmf.gif

is the yawing moment of inertia.