Stress engineer

Project : EMA DS FLAADS missile program (Client MBDA
   - Review of mechanical specifications of missile launcher a nd systems according to DEF STAN and MIL STN
regulations.
   - Missile launcher computer aided design (CAD)
   - Launcher finite element modelling . GDFEM validation and description
   - Static and dynamic FE analyses Nastran SOL 101 , 103 112 , 400 oriented to verify the fulfillment of the
mechanical requirements of the structure.

Project: A380 Belly Fairing (Client AIRBUS).
   - Programming python script for automatic sandwich panel strength calculations for a given DFEM.

Project: BELUGA XL WP230 (Client AIRBUS).
   - HTP elevator functional test: hinge line defle ct ions compliance with specifications.
   - Loads evolution control and impact estimation in structure

Project: A380 Outer Flap ISAMI PS3 Module Benchmark (Client AIRBUS).
   - This activity falls in the frame of legacy tools replacing by ISAMI tool.

Project: ISAMI Fatigue & Damage Tolerance utilities development (Client AIRBUS).
- Fatigue spectra translators.

Project: BELUGA XL HTP & Auxiliary Fin (Client AIRBUS).
   - HTP lateral box finite element modeling according to AIRBUS design principles
   - HTP lateral box extensi o n box joints strength analysis and validation
- Normalized Stress Intensity Factor calculation

Project: A380 Belly Fairing (Client AIRBUS).
   - FEM update to model better the pa nels bending stiffness and impact evaluation
   - FEM update to model the p anels floatability and impact evaluation

Project: A350 900 Main Landing Gear Door (MLGD) (Client AIRBUS). Full Scale Test.
   - Test actuator loads calculation
   - Correlation between numerical predictions and test gauges measures.
   - Door hinges repair stress anal y sis

Project: A350XWB Belly Fairing (Client AIRBUS).
   - GFEM updates and control of the FEM evolution (IFs and structure loads).
   - GFEM validation according to the Airbus specifications (AM2036).
   - Trade off studies (carbonization, multi load path, tight zones redistribution, etc).
   - Hybrid structure strength analysis and validation. Certification documents.

Project: A30X Rear Fuselage (Client AIRBUS).
   - GFEM Validation and description according to Airbus specifications (AM2036).

Project: A350XWB ( 900, 1000) HTP, S19 and S19.1 GFEM loading support (Client AIRBUS).
   - HTP: static and fatigue load cases creation with Mapper (SimXpert).
      * Loads mapping from aerodynamic model to finite element model.
      * FEM loading according to the Airbus policy.
   - S19, S19.1: static and fatigue load cases creation with Airbus tool LMOD.

Project: A320 Neo HTP (Client AIRBUS).
   - GFEM Validation and description according to Airbus specifications
   - GFEM updating according to drawings HTP Box, Leading Edge and Elevator (simplification of real geometry
and properties of metallic, composite and sandwich structures to GFEM standards).

Project: Sizing of an endovascular filter of cobalt chromium alloy using the Finite Element Method.
   - Characterization of the materials of filter and auxiliary tube (needed to int roduce the filter in the vein). Research
on the vein behavior.
   - Finite e lement m odeling of auxiliary tube, filter and vein.
   - Simulation of the filter implant process (non linear ity due to complex geometry, contact s, etc ). Trade off studies
to check the mesh size, tube diameter and contact methods influence in the analysis convergence and in the
pressure on the vein’s wall obtained from the analysis

Master de especialización en mecánica y cálculo de estructuras mediante método de elementos finitos.