The role involves performing comprehensive stress analysis of aircraft structures using advanced methods like ISAMI, GFEM, and DFEM
Job Summary
The role involves performing comprehensive stress analysis of aircraft structures using advanced methods like ISAMI, GFEM, and DFEM.
Candidates will be responsible for creating Finite Element Models, sizing primary and secondary structures, and calculating Reserve Factors for various failure modes.
The position requires preparing stress certification dossiers including ACD4 and SSR reports while collaborating with loads and certification teams.
Matching Summary
The role involves performing comprehensive stress analysis of aircraft structures using advanced methods like ISAMI, GFEM, and DFEM.
Skills & Requirements
Must-have
Static stress analysis experience
Finite Element Modeling (FEM)
Composite and metallic structure sizing
Fastener joint analysis
Reserve Factor calculation
Nice-to-have
Collaboration with design teams
Regulatory compliance awareness
Commitment to integrity
Key Requirements
5-7 years of professional experience
Knowledge of standard references for static design values
Experience with buckling and shear panel failure analysis