Bayt.com
https://bayt.page.link/C1swJsM3jKXcrFWi6
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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 & 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 requirement
  • 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
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