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Work Background
BETA TECHNOLOGIESFinite Element Analyst
Apr. 2022Montreal, Quebec, CanadaINDEPENDANT CONSULTANT ππππ πππ πππππ & πππππ πππππ
β
Development of the complete aircraft Global Finite Element Models (GFEM).
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Development of High Definition Finite Element Models (between 2 and 10 million DOF's).
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Finite Element Analysis using MSC-NASTRAN for Linear & Non-Linear Static (SOL101 & SOL400), Buckling (SOL105), Modal (SOL103) Analysis of metallic and composite structure
FEA AcademyFounder - Director - Publisher - Trainer - Book Author - Speaker - Analyst
Jul. 2020Canadaβ
FEA Consulting in Solid Mechanics & Structural Analysis β
Online FEA trainer for students and professionals in basic and advanced FEA courses.
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Author of the book "Practical Finite Element Analysis for Mechanical Engineers".
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Self-publishing
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Broadcast the FEA Academy webinars
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Ambassador of the Hexagon/MSC Technology Partner Programme "ππ«ππππ’πππ₯ π
π’π§π’ππ ππ₯ππ¦ππ§π ππ§ππ₯π²π¬π’π¬ ππ¨π« ππππ‘ππ§π’πππ₯ ππ§π π’π§πππ«π¬" is a book which offers the best practical methods and guidelines for the development and validation of finite element models. Its objective is to give mechanical structural engineers the keys to developing accurate and reliable finite element models by avoiding the most frequent errors. "ππ«ππππ’πππ₯ πππ¬π’π π
ππ" & "ππ«ππππ’πππ₯ ππ¨π§π₯π’π§πππ« π
ππ" are online courses which permit beginners and experimented engineers learning FEA.
Pratt & Whitney CanadaFinite Element Analyst & Stress Analyst
Jun. 2016 - Mar. 2022Longueuil, QC, CanadaINDEPENDANT CONSULTANT π
πππππ πππππππππ - ππππ
ππππ & ππππππ ππππππ
β
Development of Pylons & Nacelles for the Flight Test Bed Aircraft Boeing 747SP
β
Finite Element analysis (Static & Dynamic) for development of Nacelles for PW800 program
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Finite Element Analysis using MSC-NASTRAN for Linear & Non-Linear Static (SOL101-106-400), Buckling (SOL105), Modal (SOL103) & Dynamic (SOL111-129) problems
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Development of detailed FEM for metallic and composite parts
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Dynamic Analysis in Frequency Response (SOL111) for EBU systems
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Dynamic Analysis in Transient (SOL129) for Fan Blade Off events
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Substantiation of special installations on the Flight Test Bed Aircraft Boeing 747SP by FEA
BOMBARDIERFinite Element Analyst & Stress Analyst
Sep. 2006 - May. 2016Montreal, QC, CanadaINDEPENDANT CONSULTANT April 2013 - May 2016
π-ππππππ πππππ & πππππ
πππ & ππππ π
πππππππ
β
Finite element modeling (2D & 3D) with MSC-NASTRAN
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Linear & Non-Linear Static Analysis (SOL101, 106 & 400), Buckling (SOL105) and Modal Analysis (SOL103)
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Global FEM condensation
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Global FEM creation & management
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Detailed FEM creation & validation (between 2.5 & 10 millions D.O.F.βs)
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Modeling of complex joints with DFEMs using the Rutman methodology
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Assembling of high definition FEMs into GFEM
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FEM verification & validation
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Loads Generation (pressure & thermal mappingsβ¦)
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Rotor Burst Analysis
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Wheels-Up Landing & Ditching analysis
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Frequency Response Analysis by FEM (SOL111) on fuel lines
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Review of supplier data (FEMs and Stress Reports)
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Preparation of certification reports March 2010 - March 2013
ππππππππ πππ πππππππ ππ
πππππππππ ππππππππ π
πππππππ
β
Structural Analysis by FEM having a large amount of degrees of freedom (up to 5 millions)
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Sizing of the composite skin (honeycomb co-cured skin)
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FEA of the composite skin : static linear (SOL101) and non-linear (SOL106), buckling (SOL105)
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Transient analysis with MSC-NASTRAN (SOL129) to validate dynamic effects on Nose Panel
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Development of an optimized layup for the Flight Test Aircraft by FEM Sept 2006 - Feb 2010
ππππππππ ππππ ππππππ & πππππππ
πππππ
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Static and fatigue analysis
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Detailed FEMs with MSC-PATRAN-NASTRAN (linear & non-linear SOL101 - 106)
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Correlation between FEM and Durability & Damage Tolerance Test
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Definition of solutions in order to improve the life of parts
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Transient analyses with MSC-NASTRAN (Non-Linear Transient solution SOL129) on flaps
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Management of the MSC-NASTRAN Global FEM of the CRJ1000 aircraft
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Acoustic Fatigue Analysis by hand calculation (ESDU)
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Preparation of certification reports
Bell HelicopterFinite Element Analyst & Stress Analyst
Jan. 2006 - Aug. 2006Mirabel, QC, CanadaINDEPENDANT CONSULTANT ππππ πππ - ππππ πππππ
β
Design definition of the metallic and composite parts of the Bell 429 airframe
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Static analysis of the airframe by hand calculation using the Bell Helicopter methods
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Finite element analysis (static linear and non-linear, buckling) with MSC-PATRAN/NASTRAN (2D and 3D models) on metallic and composite parts
LATECOERE GROUPStress Analyst
Jul. 2001 - May. 2005Toulouse, Franceππππππ ππππ-πππ β ππππ π
ππ π
πππππππ & πππππππ ππππ πππ
β
Stress analysis by FEA using MSC/PATRAN-NASTRAN (linear and non linear).
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Static stress analysis for the definition, substantiation and certification of the structure.
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Sizing and optimization of design principles in collaboration with a design team.
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Hand calculation using Airbus and standard literature methods. ππππππππ π
πππππ π
ππ β ππππ π
πππππππ & πππππππ ππππππ πππππ π-ππππ
β
Stress analysis by FEA using MSC/PATRAN-NASTRAN (linear and non linear).
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Carrying out of a FEM for non-linear buckling analysis in SOL106 under MSC-NASTRAN on the Inlet-Sduct assembly for pressure and thermal loadings.
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Static stress analysis by hand calculation using Dassault and standard literature methods.
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Sizing and optimization of design principles in collaboration with a design team. ππππππ ππππ-πππ πππ β πππ πππππππππππ ππππ
β
Development and validation of a local FEM of the passenger surrounding door with MSC/PATRAN-NASTRAN (Linear Static SOL101).
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Hand calculation using Airbus methods and standard literature methods.
HISPANO-SUIZAStress Engineer
Dec. 1999 - Jun. 2001Le Havre, Franceππππππ ππππ β ππππππ ππππππππ
β
Development and validation of FEM's with MSC/PATRAN-NASTRAN : Linear Static SOL101, Non Linear Static SOL106, Non Linear Buckling SOL106, Modal Analysis SOL103, Linear Buckling SOL105.
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Stress analysis of metallic and composite parts of thrust reverser by hand calculation and FEA.
AIRBUSStress Analyst
Apr. 1998 - Nov. 1999Toulouse, Franceππππππ ππππ-πππ πππ β ππππππ π
πππππππ & ππππ πππππππ ππππ
β
Static stress analysis for the definition, substantiation and certification of the structure.
β
Sizing and optimization of design principles in collaboration with a design team.
β
Hand calculation using Airbus and standard literature methods.
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