gabbynambo9680 gabbynambo9680 29-05-2024 Engineering Answered Calculate the thrust of the turbojet engine in Example 7.1 at M0 1/4 0.8, 9-m altitude, reduced throttle ( Tt4 1/4 1100K ) , and P0/P9 1/4 1 for a reference air mass flow rate of 50 / at a reference altitude of 12 m.