Extraction of material data, geometry details and fastener specifications from part and assembly drawings.Extraction of loads, stresses from GFEM.Generate detailed finite element modelsStatic stress analysis of primary and secondary Aircraft structural componentsSizing of primary and secondary structural parts for static, fatigue & DT requirementsMitigation techniques for low margins of safetyPreparation of stress certification reportsPreferred 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
Skills Required
Aerospace Stress Analysis Engineer, GFEM