PROPULSION SYSTEMS IN AIRCRAFT II COURSE IDENTIFICATION AND APPLICATION INFORMATION
| Code |
Name of the Course Unit |
Semester |
In-Class Hours (T+P) |
Credit |
ECTS Credit |
| HEE406 |
PROPULSION SYSTEMS IN AIRCRAFT II |
8 |
5 |
4 |
4 |
KEY LEARNING OUTCOMES OF THE COURSE UNIT (On successful completion of this course unit, students/learners will or will be able to) |
| Students who successfully complete this course;
Will be able to compare gas turbine types and design processes.
Will be able to discuss the principles of combustion.
Will be able to define the basic principles of turbomachinery.
Will be able to explain the basic components of gas turbine.
Will be able to determine wing profile and geometry on the basis of aerodynamics.
Will be able to define turbine performance. |