AERODYNAMICS II COURSE IDENTIFICATION AND APPLICATION INFORMATION
| Code |
Name of the Course Unit |
Semester |
In-Class Hours (T+P) |
Credit |
ECTS Credit |
| UCK302E |
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) |
| Explains fundamentals of isentropic flow in a Laval nozzle |
| Solves problems involving normal shock waves in one-dimensional supersonic flow |
| Solve problems involving oblique shock waves and expansion waves in two-dimensional supersonic flow |
| Applies the linearized theory to solve subsonic and supersonic two-dimensional problems |
| Applies the method of characteristics to flow in a Laval nozzle |