Stress - Static Composite, Wing - Euk

3 days ago


Bengaluru, India Expleo Full time

Overview:
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

**Skills**:

- ISAMI
- Hyper view (Post processing knowledge)
- Catia V5, ZAMIZ/AIRENA (Basic knowledge)
- Excel & VBA
- Nastran/Patran
- Python Scripting (Desirable)

**Experience**:
8 - 10 Years - 2 Openings



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