Aerospace Stress Analysis Engineer

• 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 good working experience on Static, Fatigue & Damage tolerance analysis of Aircraft structural components.
• Should have good 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