Stress - Static Composite, Fuselage - Efr
6 months ago
Overview:
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
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