Stress – Static Composite, Fuselage - EFR
•Knowledge of aircraft Fuselage structure and aircraft loads
• Experienced in the static calculations of Airbus aircrafts (fuselage section)
• Knowledge and experience on composites and sandwich structures
• Sizing and stress analysis of the fuselage Structure and interfaces by means of hand calculations, numerical simulations (FEM)
• Well versed in ISAMI static modules and ISAMI template preparation for metallic and composite modules
• Experience in numerical modeling, post-processing (metallic & composite), extraction & reporting of the results
• Very well-versed in stress dossier writing
• Good in excel macros
B.E/B.Tech - Mechanical Engineering
• ISAMI
• Hyper view (Post processing knowledge)
• Catia V5, ZAMIZ/AIRENA (Basic knowledge)
• Excel & VBA
• Nastran/Patran
• Python Scripting (Desirable)
5 – 10 Years