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Engineering, 28.09.2019 01:10 jessica94866

A30-seat turboprop airliner whose mass is 14,000 kg takes off from an airport and eventually achieves its cruising speed of 620 km/h at an altitude of 10,000 m. for g = 9.78 m/s^2, determine the change in kinetic energy and the change in gravitational potential energy of the airliner, each in kj.

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