Stress – Static Composite
Knowledge of aircraft Fuselage structure and aircraft load
Experienced in the static calculations of Airbus aircrafts (wing 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
Experience in numerical modeling, post-processing (metallic and composite), extraction & reporting of the results
Very well-versed in stress dossier writing
Good in excel macros
B.E(Mechanical-Aero)
: 8-10 Yrs