Engineer - Aircraft Component Analysis - Static
6 months ago
- 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 LimitedEmployment Type:
Permanent-------
Experience Level:
ProfessionalJob Family:
Structure & Dynamic Systems Analysis-
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