
Stress - Static Metallic, Wing - Euk
4 days ago
Overview:
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)
**Skills**:
- ISAMI
- Hyper view (Post processing knowledge)
- Catia V5, ZAMIZ/AIRENA (Basic knowledge)
- Excel & VBA
- Nastran/Patran
- Python Scripting (Desirable)
**Experience**:
5 - 10 Years - 5 Openings
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