Exercise 4: Turbojet Engine Performance
Objective : What I want you to learn?
To apply the thermodynamic equations and analyse the performance of a Turbojet Engine with variation in the Speed and Altitude
Rationale : Why this is useful to you?
An Engine is a source of power for an aircraft, to evaluate the aircraft performance we need to evaluate the engine performance first.
Learning Outcomes : What I want you to do after completing this topic?
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.
Turbo Jet Engine Performance
Assignment 4:
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