Q. A statically-stable aircraft has a ๐ถ๐ฟ๐ผ= 5 (where the angle of attack, ฮฑ, is measured in radians). The coefficient of moment of the aircraft about the center of gravity is given as ๐ถ๐,๐.๐ = 0.05 โ 4๐ผ. 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
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