ULiege - Aerospace & Mechanical Engineering

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team:gdeliege [2015/08/11 09:14] geoffreyteam:gdeliege [2015/08/13 19:11] – [Education and Training] geoffrey
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-{{ :team:geoffrey_deliege.jpg?cache=120|Geoffrey}} 
 ====== Geoffrey DELIEGE ====== ====== Geoffrey DELIEGE ======
-Research engineer  
 ===== Contact ===== ===== Contact =====
-//E-mail// [[]] \\ +<WRAP left> 
-//Phone// : +32 (0)4 366 95 91 \\ +{{ :team:geoffrey_deliege.jpg?cache=120|Geoffrey}} 
-//Address// Université de Liège - Aerospace and Mechanics \\ +</WRAP> 
-Quartier Polytech 1 - B52/3 (office +2/541) \\ + 
-Allée de la Découverte 13 A \\ +<code> 
-B-4000 Liège, BELGIUM  \\+Email : 
 +Phone : +32 (0)4 366 95 91 
 +Mail  : Aerospace and Mechanics 
 +        Quartier Polytech 1 
 +        Allée de la Découverte 13 A 
 +        B-4000 Liège, BELGIUM 
 ===== Research activities ===== ===== Research activities =====
-==== Composite materials ====+<WRAP group> 
 +<WRAP third column> 
 +<WRAP center box 100% centeralign> 
 +**[[team:gdeliege:composite|Composite materials]]** 
 +<WRAP third column> 
 +<WRAP center box 150 centeralign> 
 +<WRAP third column> 
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 +**[[team:gdeliege:espaint|Electrostatic painting]]** 
 +<WRAP group> 
 +<WRAP third column> 
 +<WRAP center box 100% centeralign> 
 +**[[team:gdeliege:mems|Microelectromechanical systems]]** 
 +<WRAP third column> 
 +<WRAP center box 150 centeralign> 
 +**[[team:gdeliege:nnm|Nonlinear normal modes]]** 
 +<WRAP third column> 
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-Carbon-Fibre-Reinforced Polymers (CFRP) are now widely used in aerospace industry +===== Education and training =====
-thanks to their high strength-to-weight ratio. +
-However, the numerical simulation of CFRP laminates up to failure is not trivial: +
-laminates have anisotropic mechanical properties and +
-laminate damage results from a combination of microscopic mechanisms +
-(fibre brittle failure, fibre-matrix debonding, matrix ductile failure and delamination) +
-that are not easily described at a macroscopic level.+
-My objective was to implement a material model for composite plies with woven fibre +**M.Sc., 1997 Physics Engineering, Université de Liège, Belgium** \\ 
-reinforcement in Metafor. +Graduate Thesis title: //Raffinement adaptatif de types h et p pour le calcul des champs électromagnétiques.// \\ 
-This model is inspired by the meso-model +Supervisor: ProfWilly Legros.\\
-proposed by PLadevèze and O. Allix [1-2] for unidirectional +
-composites as well as the 2D model for woven composites proposed by CHochard [3].+
-The idea is to describe the laminate as a stack of 3D orthotropic plies separated by 2D interfaces. +**Ph.D., 2003 - Electrotechnics, Katholieke Universiteit Leuven, Belgium** \\ 
-In a direction parallel to the fibres+Title: //Flexible Implementation of the Finite Element Method Applied to 3D Coupled Problems Considering Convective Effects.// \\ 
-the plies are elastic and subject to brittle fracture; +Supervisors: Prof. Kay HameyerProfStefan Vandewalle.
-in shearan elastoplastic behaviour is assumed and progressive damage is introduced. +
-The 2D interfaces between the plies are elastic with progressive damage. +
-Practical information on the +
-[[doc:user:elements:volumes:ortho_hypo_materials|orthotropic materials]] +
-and +
-[[doc:user:elements:volumes:ortho_continuousdamage|damage evolution laws]] +
-is available on the Metafor web page.+
-One interesting feature of Ladevèze and Allix's work is that most parameters of the constitutive laws +===== Skills and competences =====
-can be linked to physical quantities. +
-Therefore, these parameters can be identified with suitable experimental tests.+
-{{ :team:gdeliege:stiffener2d.png?direct |Finite element simulation (Metaforof an impacted stiffener made of woven carbon fibre laminate}}+**Languages** 
 +  * French (mother tongue) 
 +  * English (advanced) 
 +  * Dutch (advanced)
-== References ==+**IT** 
 +  * software development : knowledge of C/C++, Python, Matlab, parallel programming tools (MPI), version control tools (Subversion) 
 +  * finite element software (university code ; Samcef ; marginal use of MagNet, ANSYS, LS-DYNA) 
 +  * Linux system management
-[1] P. Ladevèze, E. Le Dantec. //Damage modelling of the elementary ply for laminated composites.// Composites Science and Technology, Vol. 43, pp. 257-267, 1992 \\ 
-[2] O. Allix, P. Ladevèze. //Interlaminar interface modeling for the prediction of laminate delamination.// Composite Structures, Vol. 22, pp. 235-242, 1992 \\ 
-[3] C. Hochard, P.-A. Aubourg, J.-P. Charles. //Modelling of the mechanical behaviour of woven-fabric CFRP laminates up to failure//. Composites Science and Technology, Vol. 61, pp. 221–230, 2001 \\ 
 ===== Publications ===== ===== Publications =====
team/gdeliege.txt · Last modified: 2016/03/30 15:23 by

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