Solution of the D1 16. The aircraft mass m = 103 kg flying horizontally under the force of the thrust developed by the engine, which is equal to the horizontal component of F = 3,82 kN. Drag force depends on the speed of the aircraft, and is R = 0,05v2. Determine the distance traveled by the aircraft at the time when its speed changed from 100 m / s to 200 m / s.

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