Calculate the thrust of the turbojet.

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Calculate the thrust of the turbojet.

Consider a turbojet-powered airplane flying at a standard altitude of 40,000 at a velocity of 530 . The turbojet engine has inlet and exit areas of 13 and I 0 ft2, respectively. The velocity and pressure of the exhaust gas at the exit are 1500 ftls and 450 lb/ft2, respectively. Calculate the thrust of the turbojet.

 

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