Airplane Performance & Stability

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).