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

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where:

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is the dynamic pressure.

..\Images\INFO1342_wmf.gif

is the reference area.

..\Images\INFO1343_wmf.gif

is the reference span.

..\Images\INFO1344_wmf.gif

is the pitching moment of inertia.