Branch Details
Aircraft Design
FSIAbbreviation: M-STLAcad. year: 2020/2021
Programme: Mechanical Engineering
Length of Study: 2 years
Tuition Fees: 3000 EUR/academic year for EU students, 3000 EUR/academic year for non-EU students
Accredited from: Accredited until: 31.12.2024
Profile
Graduates in Aircraft Design specialization obtain knowledge of Aerodynamics and Mechanics of Flight, theory of Strength of Aircraft Structure and Aircraft Design. They will be made familiar with structure materials and their processing, and design of weight-saving structure. They will acquire principles of aircraft design from the point of view of technology of production and operating. They will familiarize themselves with basics of theory of aircraft reliability and aircraft structure life.
Key learning outcomes
Graduates in Aircraft Design branch obtain knowledge of Aerodynamics and Mechanics of Flight, theory of Strength of Aircraft Structure and Aircraft Design. They will be made familiar with structure materials and their processing, and design of weight-saving structure. They will acquire principles of aircraft design from the point of view of technology of production and operating. They will familiarize themselves with basics of theory of aircraft reliability and aircraft structure life.
Occupational profiles of graduates with examples
Graduates of Aircraft Design branch find opportunity for application at projection, constructionally developmental and research workplaces of state or private aircraft industry. Gained knowledge also allows them to find application at any engineering area dealing with flow problems.
Graduates of Aircraft Design branch can continue their studies in Doctoral study programme Design and Process Engineering.
Guarantor
Course structure diagram with ECTS credits
| Abbreviation | Title | L. | Cr. | Com. | Compl. | Hr. range | Gr. | Op. |
|---|---|---|---|---|---|---|---|---|
| OAE-A | Aeroelasticity | en | 4 | Compulsory | Cr,Ex | P - 26 / L - 1 / C1 - 12 | yes | |
| OK2-A | Aircraft Design II | en | 3 | Compulsory | Cr,Ex | P - 26 / C1 - 13 | yes | |
| OZ0-A | Space Flight Mechanics | en | 3 | Compulsory | GCr | P - 26 | yes | |
| OML-A | Flight Mechanics II | en | 5 | Compulsory | Cr,Ex | P - 39 / C1 - 13 | yes | |
| OPZ-A | Aircraft On-Board Systems I | en | 4 | Compulsory | Cr,Ex | P - 52 / L - 2 / C1 - 11 | yes | |
| OSD-A | Reliability and Maintainability of Aircraft | en | 3 | Compulsory | GCr | P - 26 / C1 - 13 | yes | |
| OT2-A | Aircraft Manufacture II | en | 4 | Compulsory | Cr,Ex | P - 26 / L - 2 / C1 - 11 | yes | |
| OAA-A | Aeroacoustics | en | 4 | Compulsory-optional | GCr | P - 26 | 1 | yes |
| OZK-A | Aircraft Testing | en | 4 | Compulsory-optional | GCr | P - 26 / L - 8 / C1 - 5 | 1 | yes |
| Abbreviation | Title | L. | Cr. | Com. | Compl. | Hr. range | Gr. | Op. |
|---|---|---|---|---|---|---|---|---|
| 7AZM | English - Exam B1 for MS | en | 0 | Compulsory | Ex | Z - 1 | yes | |
| OD5-A | Diploma Project (M-STL) | en | 12 | Compulsory | Cr | VD - 156 | yes | |
| OK3-A | Aircraft Design III | en | 5 | Compulsory | Cr,Ex | P - 26 / C1 - 13 | yes | |
| OLP-A | Aviation Law and Regulations | en | 2 | Compulsory | Cr | P - 13 | yes | |
| OPL-A | Aircraft On-Board Systems II | en | 5 | Compulsory | Cr,Ex | P - 26 / L - 1 / C1 - 12 | yes | |
| ODS-A | Diploma Seminar (M-STL) | en | 2 | Compulsory | Cr | C1 - 26 | yes | |
| OUZ-A | Fatigue of Aircraft Structures | en | 4 | Compulsory | GCr | P - 26 / C1 - 13 | yes |
| All the groups of optional courses | ||
|---|---|---|
| Gr. | Number of courses | Courses |
| 1 | 1 | OAA-A, OZK-A |