The role involves performing comprehensive static stress analysis on metallic and composite aircraft structures using advanced numerical methods
Job Summary
The role involves performing comprehensive static stress analysis on metallic and composite aircraft structures using advanced numerical methods.
Candidates will be responsible for creating Finite Element Models, conducting detailed joint analyses, and preparing stress certification dossiers including ACD4 and SSR reports.
This position requires collaboration with design, loads, and certification teams to ensure full compliance with regulatory requirements.
Matching Summary
The role involves performing comprehensive static stress analysis on metallic and composite aircraft structures using advanced numerical 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 load extraction and joint analysis
ACD4 and SSR report preparation
Nice-to-have
Collaboration with design and certification teams
Awareness of compliance risks and integrity
Experience in primary and secondary structure sizing
Key Requirements
5-7 years of experience
Knowledge of standard references for static design values