Answer to Question #347676 in Mechanical Engineering for huda

Question

A turbojet aircraft flies at an altitude of 10000 m at a speed of 300 m/s. Compression ratio 10,

turbines inlet section is 1000°C and the mass flow rate of the air is 30 kg/s, from this engine

Calculate the maximum possible thrust. In addition, the heating value of the fuel is assumed to be 8400 kJ/kg.

fuel calculation.