Information about the module
General data about the module
Study program |
M.Sc. Aerospace Engineering |
Module number | 3000 |
Trimester | Autumn trimester |
ECTS | 3 |
Work load |
90h total, thereof 36h presence time 54h self-study |
Typ/TWS |
3 TWS lecture |
Qualification goals
- The students can name the regulations and explain the procedure for determining the stresses of the overall structure and apply them to simple examples.
- Students will be able to name the different theories of plane structures and point out their differences.
- Students will be able to name the stresses on the overall structure and explain the differences in the calculation methods.
- Upon completion of the module, students will be able to name the major structural assemblies of the aircraft and their essential functions and design criteria.
Content
- Regulations and stresses
- Introduction
- Development of an aircraft
- Regulations and safety
- Aircraft stress
- Aeroelastic effects
- Structures of planes, stability and loading of the whole structure
- Sheet structures
- Stability
- Determination of stress for overall structures
- Calculation of assemblies
- Introduction
- Large assemblies
- Wing and tailplane calculation
- Fuselage calculation
- Calculation of doors and gates
- Stress in riveted and bolted connections
- Bonded joints