Numerical simulation of bonded cfrp aircraft structures
Damage tolerance evaluation
Non-linear fe analyses
The Master's thesis will focus on the numerical simulation of bonded CFRP aircraft structures to evaluate damage tolerance
Job Summary
The Master's thesis will focus on the numerical simulation of bonded CFRP aircraft structures to evaluate damage tolerance.
Key responsibilities include literature research, developing and implementing a scaling approach for predicting adhesive failure, and validation through test-FEM correlation.
Benefits include attractive compensation, a 35-hour work week with flexible hours, and an international environment with opportunities for networking.
Matching Summary
The Master's thesis will focus on the numerical simulation of bonded CFRP aircraft structures to evaluate damage tolerance.
Skills & Requirements
Must-have
Numerical simulation of bonded CFRP aircraft structures
Damage tolerance evaluation
Non-linear FE analyses
Test-FEM correlation
Nice-to-have
International environment
Modern/diverse technologies
Team player
Network expansion
Key Requirements
Master's degree in Aerospace Engineering, Mechanical Engineering, or similar
Finite Element Simulation and Fiber Composite Technology coursework
Practical FEM simulation experience
Experience with Altair Hyperworks and Optistruct (optional)
Experience with fiber composite structures (optional)