To apply the thermodynamic equations and analyse the performance of a Turbojet Engine with variation in the Speed and Altitude
An Engine is a source of power for an aircraft, to evaluate the aircraft performance we need to evaluate the engine performance first.
Apply the thermodynamic equations to analyse the performance of a Turbojet Engine using the Python Code.
Generate the Plots of Variation of Jet Engine Performance with Altitude and Velocity.
An airplane powered with the turbojet engine with the Inlet diameter is 0.75 m flying at standard sea level with a velocity of 305 m/s with the fuel-air ratio 0.05. (Use the Data Given Below)
Plot the Variation of Thrust Produced by the Engine Varying with the Velocity at the Altitude of 5 km from Mean Sea Level Under ISA.
Plot the variation of Thrust Produced by varying the altitude at the Velocity of 305 m/s