Numerical simulation of bonded cfk aircraft structures
Damage tolerance assessment
Fe-models with coarser resolution
The Master's thesis will investigate representative CFK aircraft structures in bonded design and evaluate them for damage tolerance using numerical simulation
Job Summary
The Master's thesis will investigate representative CFK aircraft structures in bonded design and evaluate them for damage tolerance using numerical simulation.
Tasks include literature research, developing and implementing a scaling approach for predicting adhesive layer failure through nonlinear FE analyses, and validation through test-FEM correlation.
Benefits include attractive compensation, a 35-hour work week with flexible hours, and an international environment with opportunities to build global contacts.
Matching Summary
The Master's thesis will investigate representative CFK aircraft structures in bonded design and evaluate them for damage tolerance using numerical simulation.
Skills & Requirements
Must-have
Numerical simulation of bonded CFK aircraft structures
Damage tolerance assessment
FE-models with coarser resolution
Static and dynamic load
Nonlinear FE-analyses
Nice-to-have
International environment
Modern/varied technologies
Team member
Generation Airbus Community
Key Requirements
Master's degree in Aerospace Engineering, Mechanical Engineering or similar
Finite Element Simulation and Fiber Composite Technology courses