| Code |
10372
|
| Year |
3
|
| Semester |
S2
|
| ECTS Credits |
6
|
| Workload |
TP(60H)
|
| Scientific area |
Aeronautics and Astronautics
|
|
Entry requirements |
Knowledge of Physics, Mathematics, Differential Analysis, Numerical Analysis, Statistical Methods, Algebra, Applied Continuum Mechanics, Experimental and Computational Methods, Elementary Fluid Mechanics.
|
|
Mode of delivery |
Face to face.
|
|
Work placements |
None.
|
|
Learning outcomes |
Capacity for analysis and control of boundary layers. Capacity analysis and design of airfoils. Capacity analysis and design of wings. Capacity for analysis and design of blunt bodies.
|
|
Syllabus |
Governing equations. Laminar boundary layers. Transition. Airfoils. Wings. Blunt bodies.
|
|
Main Bibliography |
Anderson, J.D., Jr. “Fundamentals of Aerodynamics”. McGraw-Hill.
|
|
Teaching Methodologies and Assessment Criteria |
Theoretical-practical classes and laboratory.
|
|
Language |
Portuguese. Tutorial support is available in English.
|