Aerospace Engineering > GATE 2010 > Longitudinal Stability
The Irim curves of an aircraft are of the form Cm,...=(0.05-0.2δ)-0.1Ct where the elevator
deflection angle, δr, is in radians. The static margin of the aircraft is:
deflection angle, δr, is in radians. The static margin of the aircraft is:
Correct : c
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