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CV: Structural analysis consultant
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Date Submitted: Last Modified: Current job: Employment Term: Relocation: Date available: Industry: KeywordsSUMMARY:
An extremely well qualified Engineer with a wide variety of structural analysis experience on both Spacecraft and Aircraft including also thermal analysis experience. Particularly recognized for his pro active ability to work independently and effectively, always concerned with both reliability and tight time schedules. Looking for challenging technical work covering all structural disciplines.
SKILLS:
Mathematical: Excel, Mathcad, Mapple, Matlab, MS Office
Finite Element Analysis: NASTRAN, PATRAN, Femap, IDEAS, SAMCEF
Hand Stressing: ESDU, Bruhn, Roark
Thermal: Gaetan, Esatan, Thermica
Programming:
ACHIEVEMENTS:
- Has performed a wide variety of structural analysis including Finite Element Analysis and Hand calculations
- Management experience at different levels from team leader to project manager
- Developed and programmed several in-house routines to optimize analysis process under several languages (Excel/Visual Basic, Patran Command Language, FEMAP scripts)
- Extensive knowledge of composite and metallic structures under static linear/non linear, dynamic, thermal, fatigue and damage tolerance behaviours
EDUCATION:
1998 – 2002 : Master of Science in Aeronautic and Space Engineering
(French Ingénieur, ENSICA)
1995 – 1998 : Preparatory classes for “Grandes Ecoles”
1995 : French Scientific Baccalaureate (Mathematics & Technology options)
OTHER DETAILS:
Languages:
Fluent : English, French, Italian
Intermediate : German
Notion : Finnish, Dutch
Personal details:
French National
British Security Clearance held
WORK EXPERIENCE:
2008 – Present Atkins Aerospace,
Stress dossiers check stressing , giving recommendations to customer/suppliers to re-perform work when quality and methods were not reliable.
2006 - 2007 Patria, Finland Structural consultant
A400M Fin TIP.
- Composite and metallic static, fatigue and thermal sizing
- Development of analysis tools in Patran Command Language, Visual Basic and Excel
2005 - 2005 Stork/Fokker,
A380 J-Nose
- Tool development of a Nastran parameter model using Excel as a Pre and Post Processor in order to detail load paths in a composite/metallic bolt joint integrating fastener non linear behaviour
- Load redistribution between global and local FEM approaches on riblets fasteners using mathematical correlation matrix
2002 - 2005 Assystem Etudes,
- Structural analysis on A380 fuselage, nose fairing, ailerons and landing gear bay related to static/fatigue on metallic and composite materials
- Project manager: fatigue test tool for a new generation pylon rib
- Satellite: thermal specification on satellite panels
2000 - 2001 Alenia Spazio,
Sizing and validation of satellite RADARSAT 2 bus structure (PDR and CDR phases)
- Dynamic sizing of secondary structures
- Static thermo elastic non-linear analysis on Launch Vehicle Adapter
- Cleats development (stress, rigidity and test correlation)
| 1 month - Discovery | 350 euros | convert |
| 3 months - Bronze | 850 euros | convert |
| 6 months - Silver | 1450 euros | convert |
| 12 months - Gold | 2500 euros | convert |
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