- Own GFEM updates, FEM validation, and DMU optimization.Define mesh strategies for complex stress/F&DT; analyses.
- Lead load extraction, hand calcs, and crack growth assessments.
- Conduct fatigue life predictions (rainflow/Miner) and damage tolerance evaluations.
- Validate composite/metallic material performance in ISAMI.
- Manage complex static and fatigue analysis, including crack growth and DTA for metallic and composite structures.
- Ensure compliance with Airbus structural analysis methods and tools.
- Develop Excel VBA tools for process automation.
- Drive and ensure Airframe certification requirements and resolve critical structural issues.
- Guide junior engineers and review analysis reports.
- Review technical reports, Liaise with Technical committee for design verification and changes.
- conduct technical audits, and support management decisions.
Qualifications:
- Master’s in Aerospace/Mechanical Engineering (PhD a plus).
- 9+ years in airframe stress/F&DT; (fuselage sub-assemblies: frames, panels, junctions).
- Expert in Airbus methods, ISAMI, HyperWorks, Nastran/Patran.
- Deep knowledge of composite/metallic fatigue and crack growth.
- Advanced Excel/VBA/Python for analytical automation.
- Positive Communication skills