Engineering, 17.07.2019 21:10, spinshot13

Ajet airplane, with a wing area of 20 m', moves through still air at a constant velocity of 225 m/s. the plane is at an altitude of 5000 m and is climbing at an angle of 20 degrees horizon. under the given conditions, the plane has a lift coefficient of 0.2, and with the a drag coefficient of 0.075. answer the following a)-what thrust force, in n, must the jet engine produce? b)-what power, in kw, must the jet engine produce?

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Ajet airplane, with a wing area of 20 m', moves through still air at a constant velocity of 225 m/s....