Akademik Dersler - İçerik

0 : Does not support 1 : Low-level support 2 : Mid-level support 3 : Top level support

Learning Outcomes	1	2	3	4	5	6	7	8	9
Explain the physical principles of thrust generation in aircraft propulsion systems.	3	3	3	3	3	2	2	3	1
Classify air-breathing propulsion systems according to operating principle and application.	3	3	3	3	3	2	2	3	1
Apply conservation of mass, momentum, and energy to basic propulsion-system problems.	3	3	3	3	3	2	2	3	1
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
Analyze ideal and real turbojet and turbofan engine cycles.	3	3	3	3	3	2	2	3	1
Compare turbojet, turbofan, turboprop, and turboshaft engines for different flight missions.	3	3	3	3	3	2	2	3	1
Describe the function and performance role of inlets, compressors, combustors, turbines, and nozzles.	3	3	3	3	3	2	2	3	1
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
Interpret propulsion-system selection for subsonic, supersonic, and special-purpose aircraft.	3	3	3	3	3	2	2	3	1