Aerospace Engineering > GATE 2009 > Longitudinal Stability
The contribution of the horizontal tail to the pitching moment coefficient about the center of gravity
(CmCG) of an aircraft is given by Cmtalt=0.2-0.0215 α where α is the angle of attack of the
aircraft. The contribution of the tail to the aircraft longitudinal stability
(CmCG) of an aircraft is given by Cmtalt=0.2-0.0215 α where α is the angle of attack of the
aircraft. The contribution of the tail to the aircraft longitudinal stability
Correct : a
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