Static Stress Engineer

1w1 week ago

Airbus

Bengaluru, IN · Full-time · INR 2,500,000 – INR 4,000,000

About this role

The Static Stress Engineer role at Airbus involves performing stress analysis on metallic and composite aircraft structures using classical methods, ISAMI, GFEM, and DFEM. Responsibilities include extracting loads, stresses, material data, geometry details, and fastener specifications from part and assembly drawings. This ensures structural integrity meets aviation standards.

Daily tasks encompass applying static design values from standard references and creating, refining Finite Element Models using geometric data. Engineers conduct sizing of primary and secondary structures to satisfy static requirements, extract fastener loads, and perform detailed joint analysis. Reserve Factors are calculated for failure modes like strength, buckling, and shear panel failure.

Collaboration with design, loads, and certification teams is essential to ensure compliance with regulatory requirements. Professionals identify low Reserve Factor mitigations using classical or numerical methods and prepare stress certification dossiers, including ACD4 and SSR reports. This team-oriented environment supports Airbus India's engineering efforts.

The position demands 5-7 years of experience and awareness of compliance risks with a commitment to integrity for company success. Airbus fosters flexible working arrangements to enable innovative thinking and connection. An inclusive environment welcomes diverse applications for sustainable growth.

Requirements

5-7 years of experience in stress analysis
Proficiency in classical stress analysis methods for aircraft structures
Experience with ISAMI, GFEM, and DFEM tools
Knowledge of metallic and composite materials in aerospace
Familiarity with Finite Element Modeling and joint analysis
Ability to calculate Reserve Factors for various failure modes
Understanding of regulatory compliance for aircraft certification
Awareness of compliance risks and commitment to act with integrity

Responsibilities

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 failure modes including strength, buckling (column & panel), and shear panel failure
Prepare stress certification dossiers, including ACD4 and SSR reports

Benefits

Permanent employment
Flexible working arrangements to stimulate innovative thinking
Commitment to workforce diversity and inclusive working environment
Equal opportunities irrespective of social and cultural background, age, gender, disability, sexual orientation, or religious belief