| Learning Outcomes | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 | 11 |
|---|
| Explain the physical principles of thrust generation in aircraft propulsion systems. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Classify air-breathing propulsion systems according to operating principle and application. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Apply conservation of mass, momentum, and energy to basic propulsion-system problems. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Calculate and interpret thrust, specific thrust, fuel consumption, and propulsion efficiencies using theoretical relations and basic experimental data. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Analyze ideal and real turbojet and turbofan engine cycles. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Compare turbojet, turbofan, turboprop, and turboshaft engines for different flight missions. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Describe the function and performance role of inlets, compressors, combustors, turbines, and nozzles. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Evaluate the effects of flight Mach number, pressure ratio, bypass ratio, turbine inlet temperature, and component efficiency on engine performance. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |
| Interpret propulsion-system selection for subsonic, supersonic, and special-purpose aircraft. | 3 | 3 | 3 | 3 | 3 | 2 | 2 | 3 | 1 | 0 | 0 |