Knowledge of aircraft Fuselage structure and aircraft load
Experienced in the static calculations of Airbus aircrafts (wing section)
- 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, extraction & reporting of the results
- Very well-versed in stress dossier writing
- Good in excel macros
- Knowledge and experience on composite and sandwich structures (Desirable)
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
- Knowledge of aircraft and understanding the functions of various aerospace wing components
- Expert in Finite element modeling using Hypermesh (1D, 2D, 3D ) and should be capable of idealizing the structure both GFEM and DFEM
- Experience on using connections like MPCs, Stuck nodes, Glue elements, CFAST etc
- Experience in submitting and debugging issues with Nastran Runs
- Well versed in post-processing FE results and capable of presenting the FEM results
- Experience in FE Validations per Airbus methodology
- Experienced in the static calculations of Airbus aircrafts (wing section)
- Well versed in ISAMI static modules and ISAMI template preparation
- Sizing and stress analysis of the Wing Structure and interfaces by means of hand calculations, numerical simulations (FEM)
- Very well-versed in stress dossier writing
- Good in excel macros, Tcl/Tk, PCL
F&DT- Fuselage - 1 Opening
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