Finite element modeling (fem) using isami gfem dfem
Classical methods for structural sizing
The role involves performing comprehensive static stress analysis on metallic and composite aircraft structures using classical methods and advanced FEM techniques
Job Summary
The role involves performing comprehensive static stress analysis on metallic and composite aircraft structures using classical methods and advanced FEM techniques.
Candidates will be responsible for creating detailed Finite Element Models, sizing structures, and calculating Reserve Factors to ensure compliance with regulatory requirements.
The position requires preparing stress certification dossiers including ACD4 and SSR reports while collaborating closely with design, loads, and certification teams.
Matching Summary
The role involves performing comprehensive static stress analysis on metallic and composite aircraft structures using classical methods and advanced FEM techniques.
Skills & Requirements
Must-have
Static stress analysis of aircraft structures
Finite Element Modeling (FEM) using ISAMI GFEM DFEM
Classical methods for structural sizing
Fastener load extraction and joint analysis
Reserve Factor calculation for failure modes
ACD4 and SSR report preparation
Nice-to-have
Collaboration with design loads teams
Regulatory compliance awareness
Commitment to integrity and safety
Flexible working arrangements
Key Requirements
5-7 years of experience in structural analysis
Proficiency in ISAMI, GFEM, and DFEM tools
Knowledge of standard references for static design values