Role & responsibilities :
Extraction of material data, geometry details and fastener specifications from part and assembly drawings.
Extraction of loads, stresses from GFEM.
Generate detailed finite element models
Static stress analysis of primary and secondary Aircraft structural components
Sizing of primary and secondary structural parts for static, fatigue & DT requirements
Mitigation techniques for low margins of safety
Preparation of stress certification reports

Preferred candidate profile:
Candidate should have positive working experience on Static, Fatigue & Damage tolerance analysis of Aircraft structural components.
Should have positive working experience on plant engineering concessions of Aircraft structural (Primary and Secondary) components.
Profound knowledge on Stress analysis, aircraft loads and aircraft structures are expected.



Should be aware of certification requirements and should have experience with static & fatigue stress certification reports.
Candidate should be able to co-ordinate with design and stress teams. Sound knowledge of structural design principles, aircraft loads and aircraft structures are expected
Must have experience in static analysis & sizing of Aircraft structural components for metallic and composites
Must have experience in the preparation of stress certification reports
Working experience in concessions
Must have experience in the preparation of stress reports.
Having experience in Fatigue & damage tolerance analysis is an added advantage

📌 Aerospace Stress Analysis Engineer Bengaluru
🏢 Infosys
📍 Bengaluru