A combination of finite element modelling (FEM) and classical hand calculation methods were used to ascertain load distribution and strength when subjected to the loads and requirements defined by the customer.

A Stress Report was delivered to enable certification of the aircraft. Support was provided throughout the qualification process, including test support and certification support.

Deliverables

  • Design and Analysis
  • Certification Stress Report
  • Qualification Support

Toolset

  • NASTRAN
  • PATRAN
  • CATIA
  • ACSA
  • SAFE

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