2. Analysis of Thrust Equation for Ideal Turbo Jet Engine P M V Subbarao Professor Mechanical Engineering Department Understanding the Features of A True Flying Machine Muscles ….

3. Ideal Turbo Jet Cycle T0T0 1,2 3 4 5,6 s

4. p0p0 s 1,2 3 4 5,6 Ideal Turbo Jet Cycle

5. Thrust

7. Isentropic Expansion in an Active Turbine

8. Theory of Jet Propulsion : Jet Enough Work The power input to the compressor = The power output of the turbine

11. Isentropic Expansion in a Passive Turbine (Nozzle)

12. Thermodynamic SSSF model for Nozzle

13. Limit of Utilization: Open Cycle Engine: Just to Ambient Pressure!!!

16. Maximum Obtainable Jet Kinetic Energy:

22. Generation of Thrust : The Capacity

23. Specific Thrust S

24. Propulsive Power or Thrust Power: Thrust Specific Fuel Consumption TSFC

25. Aviation Appreciation Propulsion Efficiency

27. Thermodynamic Appreciation Thermodynamic Efficiency

30. Jet engine Performance Parameters