Fatigue and Damage Tolerance Analysis was completed considering both Primary & Secondary Crack Growth using Airbus methods and toolsets on Rib Posts 4 and 7 attached to the Rear Spar on A350. 

Deliverables

  • Stress Reports

Toolset

  • NASTRAN
  • PATRAN
  • ISAMI Static
  • ISAMI Fatigue
  • CATIA

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