The 30-Mg aircraft is climbing at the angle under θ = 15o a jet thrust T of 180 kN. At the instant represented, its speed is 300 km/h and is increasing at the rate of 1.96 m/s2. Also θ is decreasing as the aircraft begins to level off. If the radius of curvature of the path at this instant is 20 km, compute the lift L and drag D. (Lift L and drag D are the aerodynamic forces normal to and opposite to the flight direction, respectively.)
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