| Code | Name of the Course Unit | Semester | In-Class Hours (T+P) | Credit | ECTS Credit |
|---|---|---|---|---|---|
| UCK446 | COMPUTATIONAL AERODYNAMICS | 5 | 3 | 3 | 5 |
Objectives and Contents |
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|---|---|
| Objectives: | 1. Calculation of two-dimensional incompressible potential flow around airfoils by panel methods. 2. Calculation of three-dimensional incompressible potential flow around finite wings by panel methods. 3. Calculation of three-dimensional incompressible potential flow around aircraft fuselages by panel methods. |
| Content: | Fundamentals of frictionless incompressible flow, general solutions of incompressible potential flow equations, panel methods, singularity elements and influence coefficients, two-dimensional numerical solutions, three-dimensional numerical solutions, time-dependent incompressible potential flow, refinements applied to the potential flow model |