Numerical simulation of bonded cfk aircraft structures
Damage tolerance evaluation
Fe-models with coarser resolution
The structural bonding of fiber composite materials is a key technology in aviation for building lighter and more economical structures
Job Summary
The structural bonding of fiber composite materials is a key technology in aviation for building lighter and more economical structures.
In the scope of the Master's thesis, representative CFK aircraft structures in bonded design are to be investigated and evaluated for damage tolerance using numerical simulation.
Attractive remuneration and balanced work-life balance with a 35-hour week (flexible working hours).
Matching Summary
The structural bonding of fiber composite materials is a key technology in aviation for building lighter and more economical structures.
Skills & Requirements
Must-have
Numerical simulation of bonded CFK aircraft structures
Damage tolerance evaluation
FE-models with coarser resolution
Static and dynamic loading
Nice-to-have
International environment
Modern/varied technologies
Generation Airbus Community
Key Requirements
Master's degree in Aerospace Engineering, Mechanical Engineering or similar
Finite Element Simulation and Fiber Composite Technology courses