Aeronautics

A380

PROJECT DATA

  • Client: AIRBUS MILITARY, CT Ingenieros
  • Data: 2010 – 2012
  • Technologies: Static Structural Analyses and Fatigue and Damage Tolerance

PROJECTS

  • A380e – Belly Fairing: Structural Analysis and Justification of components. Airbus Military, 2010-2011
  • A380 – Wing Booms: Booms Resizing – Fatigue and Damage tolerance. CT Ingenieros. 2012

A380

ACTIVITIES:

  • A380e – Belly Fairing
    • Loads from FEM model (NASTRAN) in Patran.
    • Comparison between loads from A380-e FEM model with loads from A380_ALS08-S3i2 FEM model.
    • Analytic calculation.
    • Verification of the results with Airbus Military applications.
    • Comparison of the RF between models.
    • Design-stress communications.