Engineer - Aircraft Component Analysis - Static

6 months ago


Bengaluru, India airbus Full time
Job Description:
  • 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 & amp; assembly drawings
  • Application of appropriate static, fatigue and damage tolerance design values from standard references
  • Creation of FEMs using geometric data from part & amp; 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

This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.

Company:

Airbus Group India Private Limited

Employment Type:

Permanent

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Experience Level:

Professional

Job Family:

Structure & Dynamic Systems Analysis



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