The role involves performing comprehensive stress analysis on metallic and composite aircraft structures using advanced numerical and classical methods
Job Summary
The role involves performing comprehensive stress analysis on metallic and composite aircraft structures using advanced numerical and classical methods.
Candidates will be responsible for creating Finite Element Models, conducting detailed joint analysis, and calculating Reserve Factors for various failure modes.
The position requires preparing stress certification dossiers including ACD4 and SSR reports while collaborating with cross-functional teams to ensure regulatory compliance.
Matching Summary
The role involves performing comprehensive stress analysis on metallic and composite aircraft structures using advanced numerical and classical methods.
Skills & Requirements
Must-have
Static stress analysis of aircraft structures
Finite Element Modeling (FEM) creation
Classical methods and ISAMI/GFEM/DFEM
Reserve Factor calculation for failure modes
Fastener joint analysis and sizing
Nice-to-have
Collaboration with design and certification teams
Experience with ACD4 and SSR reports
Commitment to integrity and compliance risks
Key Requirements
5-7 years of professional experience
Knowledge of standard references for static design values
Ability to identify and implement low RF mitigations