PROPULSION SYSTEMS COURSE IDENTIFICATION AND APPLICATION INFORMATION
| Code |
Name of the Course Unit |
Semester |
In-Class Hours (T+P) |
Credit |
ECTS Credit |
| UCK306 |
PROPULSION SYSTEMS |
6 |
3 |
3 |
4 |
KEY LEARNING OUTCOMES OF THE COURSE UNIT (On successful completion of this course unit, students/learners will or will be able to) |
| To understand the basics of recognizing and classifying aircraft engines. To understand how reaction is created with aircraft engines. To understand the basic performance parameters in aircraft engines. To understand the use of thermodynamic cycles in performance analysis in aircraft engines. To understand the reaction heat, adiabatic flame temperature and their effects on general performance in aircraft engine combustion chambers. To be able to calculate the ideal performance of aircraft engines and their components under design conditions. To understand the internal and effects of aircraft engine component losses on general performance analysis. To be able to calculate and examine aircraft engine performance values in real situations where losses occur. To be able to perform and interpret aircraft engine performance analysis. |