Structural Stress Engineer (Aerospace)

Conduct independent structural analysis (static & F&DT) on fuselage primary structures (PSE). Validate FEMs, extract loads, and ensure compliance with Airbus methods.
Perform DMU cleaning, GFEM updates, and FEM validations.
Apply mesh refinement rules for stress analyses (0D/1D/2D/3D).
Extract & apply loads using Airbus in-house tools.
Conduct hand calculations, Static Stress,
Perform fatigue life calculations and crack growth
Analyze composite/metallic materials for damage tolerance.
Use ISAMI, HyperWorks suite (Hypermesh/View), MSC Nastran/Patran.
Develop Excel VBA macros for automation.
Contribute to Airframe certification tasks as needed.
Requirements:
bachelors/masters in Aerospace/Mechanical Engineering.
1-3 years of structural analysis experience (aircraft fuselage preferred).
Proficiency in F&DT, FEM validation, and stress hand calcs.
Strong skills in ISAMI, Hypermesh, MSC-NASTRAN/PATRAN, Airbus load tools.
Experience with composite and metallic material behavior.
Advanced Excel/VBA for data processing.
Familiar with Aerospace certification requirements and processes.
Preferred:
A350XWB certification experience.
Knowledge of Airbus design practices and PSE requirements