
Stress - Fem, Static, Wing - Euk
11 hours ago
Overview:
- 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
**Skills**:
- Pre Processing: Hypermesh and Patran
- Solver: Nastran and Optistruct (optional)
- Post Processing: Hyperview and Patran
- Catia V5, AIRENA (Basic knowledge)
- Excel & VBA, Tcl/Tk, PCL
- ISAMI
- Python Scripting (Desirable)
**Experience**:
8 - 10 Years - 2 Openings
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