Stress – Static Composite, Fuselage - EFR
Responsibilities
•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
Qualifications
B.E/B.Tech - Mechanical Engineering
Skills
• ISAMI • Hyper view (Post processing knowledge) • Catia V5, ZAMIZ/AIRENA (Basic knowledge) • Excel & VBA • Nastran/Patran • Python Scripting (Desirable)
Experience
5 – 10 Years
Permanent