AERODYNAMICS II COURSE IDENTIFICATION AND APPLICATION INFORMATION
| Code |
Name of the Course Unit |
Semester |
In-Class Hours (T+P) |
Credit |
ECTS Credit |
| UCK302 |
AERODYNAMICS II |
6 |
4 |
3 |
4 |
KEY LEARNING OUTCOMES OF THE COURSE UNIT (On successful completion of this course unit, students/learners will or will be able to) |
| He/she can apply correction formulas for high subsonic speeds. He/she knows the calculations of normal-shock, oblique shock and expansion waves for supersonic flows. He/she knows how to calculate with linearized potential theory for supersonic flows. He/she knows how to calculate with characteristic method for supersonic flows. |