Cassandre FADEL

En résumé

Entreprises

• Assystem - Ingénieur Calcul

  Courbevoie 2012 - maintenant

• Assystem - Stress & Design Engineering

  Courbevoie 2012 - maintenant • Stress & Design Engineering in Aerospace & Aeronautics.
  -Finite Element Analysis on Nastran (Femap 10) for SABENA and DASSAULT aviation (Static, linear buckling, modal, fatigue and damage tolerance analysis) Electronic benches & Specifics equipments
  -Finite Element Analysis on Patran 2005 (Static linear analysis) - Small parts
  -Achievement of justification files
  -Predimensioning by analytical calculations
  -3D modelling on Catia V5 (Part Design, Assembly Design, Generative shape design), finite element analysis on Nastran (Femap 10) for Amphibian Aircraft (Assystem project) and project monitoring on MS Project - composite landing gear.
  - Preliminary design and costing - composite cylindrical shell for Astrium
  - Internal traineeship on Patran/Nastran for AIRBUS - (Static linear analysis Sol 101 , Static Non Linear Analysis Sol 106, Buckling Sol 105,Modal Analysis Sol 103, Condensed modeling ,Composites modeling , ISAMI)
  
  • Stress & Design Engineering of tooling in Aerospace & Aeronautics.
  -3D modelling on Catia V5, Specific tools for SAFRAN Herakles(Vibration Frame, measuring instruments)
  -Finite Element Analysis on Nastran (Femap 10.3) for SAFRAN Herakles (Static & Modal Analysis) - Vibration frame
  -Manufacturing monitoring for SAFRAN-Herakles
  -Finite Element Analysis on Nastran (Femap 10.3) for THALES Alenia Space (Static, Modal, Stiffness analysis, displacements "method of least squares") - Vibration frame for satellite Iridium
  -3D modelling on Catia V5 - Assembly frames for DASSAULT
  -Finite Element Analysis on Nastran (Patran 2005) for DASSAULT Aviation (Static & Modal Analysis) - Assembly Frames for SMS & Rafale aircrafts
  -Finite Element Analysis on Nastran (Femap 10.3/Hyperworks) for THALES Alenia Space (Static & Modal/thermal Analysis) - positioning jig, specific trolley, Simulator of focal plan for scientific and military satellite, handling spreaders.
  
  • Stress Engineering for AIRBUS – A350XWB – Keel Beam/Center Wingbox
  -Technical Support (STECO) in AIRBUS Toulouse offices
  -Analysed and validated the Finite Element Analysis results on Patran of the Composite Center Wingbox section using nonlinear, linear and buckling analysis
  -Correlated virtual and real test results for each manufacturing steps Batch2&3
  -Created and analysed ISAMI methods for post-processing
  -Worked in team with other stress engineers
  -PowerPoint presentations and reported weekly to the client
  -Organised and prioritised work within the overall project schedule
  

• Rivoyre ingénierie - Stress & Design

  2011 - 2012 • Stress & Design Engineering for Composite Yacht parts
  -Finite Element Analysis on Femap 10 (Static linear and non-linear analysis - general training with the company Nesys engineering).
  Buckling and modal analysis on Composite parts for sailing boats and yachts.
  -Simulayt (Composites Modeling - advanced fiber simulation and ply modelling)
  -Non-linear static analysis for carbon masts
  -Production monitoring with the customers
  -Drafting on Autocad (manufacturing layouts and lamination layouts)
  -3D modelling on Catia V5 (Part Design, Assembly Design, Generative Shape Design, Generative structural analysis)
  -Training in the LORIMA manufacturing of prepreg carbon masts
  -Pre-calculations on Excel
  
  

Formations

• University Of Science And Technology

  Lille 2009 - 2011 Masters Degree

• University Of Science And Technology

  Lille 2006 - 2009 B.A.

Réseau

• Aurelien GENEST

• Bentouti SAMIR

• Cédric GESLIN

• David HENRION

• Eloi SERGENT

• Gauwin DEMULLIER

• Jérémy GABARROT

• Julien COMBRET

• Léo DEBLONDE

• Loic DUPUIS