1160 Stress Lead Static

Contract type : Permanent

Job description

Job Description: Job scope (core activities):

• Stress analysis of metallic and composite aircraft structures using hand calculations, ISAMI, GFEM and DFEMs

• Extraction of loads, stresses, generation of spectra and mission files

• Extraction of material data, geometry details and fastener specifications from part & assembly drawings

• Application of appropriate static, fatigue and damage tolerance design values from standard references

• Creation of FEMs using geometric data from part & assembly drawings

• Sizing of primary and secondary parts for static and fatigue requirements

• Fastener load extraction and joint analysis

• RF calculation for different failure modes such as strength, buckling, shear panel failure, damage tolerance etc.

• Low RF mitigations using classical or numerical methods

• Preparation of stress certification dossiers, ACD4 and ACD6

Profile

5 - 9 years of experience in static analysis

Graduate / Post Graduate Engineer (Aerospace Engineering / Mechanical Engineering).
Experience working with Aerospace OEM / Tier / Suppliers on Specific Design activities.
• Minimum 3 years’ experience in leading team.
Tools : Patran/Nastran, Hypermesh, ISAMI (preferred)
• Sound knowledge of structural design principles, aircraft loads and aircraft structures
• Experience in static, fatigue and damage tolerance analysis of aircraft structural components
(Airbus methods and tools would be preferable)
• Background in design and sizing of aircraft primary structure components and parts
• Ability to liaise/negotiate with design, stress, EU teams and customer services
• Certification requirements and experience with stress dossiers
• Finite element method / finite element analysis (FEM / FEA)
• Very good analytical and reasoning skills