Static Stress Engineer

Job Description

Analysis and Validation of metallic structures for static & fatigue strength.

Ensure safe operation of the Product with respect to structural integrity and operational effectiveness.

Experience Range : 3-15 Years Only

• Perform stress analysis of metallic and composite aircraft structures using classical methods, ISAMI, GFEM, and DFEM.
• Extract loads, stresses, material data, geometry details, and fastener specifications from part and assembly drawings.
• Apply appropriate static design values from standard references.
• Create and refine Finite Element Models (FEMs) using geometric data.
• Conduct sizing of primary and secondary structures to meet static requirements.
• Extract fastener loads and perform detailed joint analysis. Calculate Reserve Factors (RF) for various failure modes, including:
• Strength
• Buckling (Column & Panel)
• Shear panel failure
• Identify and implement low RF mitigations using classical or numerical methods.
• Prepare stress certification dossiers, including ACD4 and SSR reports.
• Collaborate with design, loads, and certification teams to ensure compliance with regulatory requirements.