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