Q. 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
