A typical longitudinal Stability quadratic for an aircraft having a mass of 20,000 kg and wing area 50 m2. Aircraft is flying at 240 m/s where the relative density is 0.5. The Characteristic equation is λ4+ 4.5λ3 +8.3 λ2 +0.5λ+0.06+0. Determine the roots of the equation, Time period of the phugoid motion and write comments on the modes of motion.
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