Stress Static Lead (M/F)

Type d'emploi : CDI / Permanent

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

Profil souhaité

Qualification : B.E / M. E. in Mechanical / Aeronautical Engineering

Graduate / Post Graduate Engineer (Aerospace Engineering / Mechanical Engineering).

Experience Range : 6 - 9 years of experience in static analysis

Experience working with Aerospace OEM / Tier / Suppliers on Specific Design activities

Minimum 3 years’ experience in leading team.

Experience in High Lift is an advantage

Keyskills :

• Tools : Patran/Nastran, Hypermesh, ISAMI (preferred)
• Advanced Knowledge of Microsoft Office Software
• Sound knowledge of structural design principles, aircraft loads and aircraft structures
• Experience in static, fatigue and damage tolerance analysis of aircraft structural components
• Knowledge of Airbus internal Static manuals, methods and policies mandatory
• Advanced knowledge of hand and classic calculation methods (e.g. HSB, Bruhn…)
• 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)
• Knowledge in Metallic / CFRP aircraft structure
• Very good analytical and reasoning skills

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