Aerospace Engineering > GATE 2018 > Aircraft Performance
A statically-stable aircraft has a CLα=5 (where the angle of attack, α, is measured in radians). The coefficient of moment of the aircraft about the center of gravity is given as CM,c.g=0.05−4α The mean aerodynamic chord of the aircraft wing is 1 m. The location (positive towards the nose) of the neutral point of the aircraft from the center of gravity is ________ (in m, accurate to two decimal places).
Correct : -0.81 to -0.79
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