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team:gdeliege [2015/08/11 09:14] geoffreyteam:gdeliege [2016/03/30 15:23] (current) – external edit 127.0.0.1
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-{{ :team:geoffrey_deliege.jpg?cache=120|Geoffrey}} 
- 
 ====== Geoffrey DELIEGE ====== ====== Geoffrey DELIEGE ======
- 
-Research engineer  
  
 ===== Contact ===== ===== Contact =====
  
-//E-mail// : [[geoffrey.deliege@ulg.ac.be]] \\ +<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 \\ +
-B-4000 Liège, BELGIUM  \\+
  
-===== Research activities =====+<code> 
 +Email : geoffrey.deliege@ulg.ac.be 
 +Phone : +32 (0)4 366 95 91 
 +Mail  : Aerospace and Mechanics 
 +        Quartier Polytech 1 
 +        Allée de la Découverte 13 A 
 +        B-4000 Liège, BELGIUM 
 +</code>
  
-==== Composite materials ====+===== Education and training =====
  
-Carbon-Fibre-Reinforced Polymers (CFRP) are now widely used in aerospace industry +**M.Sc., 1997 Physics Engineering, Université de Liège, Belgium** \\ 
-thanks to their high strength-to-weight ratio+Graduate Thesis title: //Raffinement adaptatif de types h et p pour le calcul des champs électromagnétiques.// \\ 
-However, the numerical simulation of CFRP laminates up to failure is not trivial+SupervisorProf. Willy Legros.\\ 
-laminates have anisotropic mechanical properties and + 
-laminate damage results from a combination of microscopic mechanisms +**Ph.D.2003 ElectrotechnicsKatholieke Universiteit Leuven, Belgium** \\ 
-(fibre brittle failurefibre-matrix debondingmatrix ductile failure and delamination) +Title: //Flexible Implementation of the Finite Element Method Applied to 3D Coupled Problems Considering Convective Effects.// \\ 
-that are not easily described at a macroscopic level.+Supervisors: Prof. Kay Hameyer, Prof. Stefan Vandewalle. 
 + 
 +===== Research activities =====
  
-My objective was to implement a material model for composite plies with woven fibre +<WRAP group> 
-reinforcement in Metafor. +<WRAP third column> 
-This model is inspired by the meso-model +<WRAP center box 100% centeralign> 
-proposed by PLadevèze and O. Allix [1-2for unidirectional +[[team:gdeliege:composite|{{:team:gdeliege:labelcomposite.png}}]]\\ 
-composites as well as the 2D model for woven composites proposed by CHochard [3].+**[[team:gdeliege:composite|Composite materials]]** 
 +</WRAP> 
 +</WRAP> 
 +<WRAP third column> 
 +<WRAP center box 150 centeralign> 
 +[[team:gdeliege:shearo|{{:team:gdeliege:labelshearo.png}}]]\\ 
 +**[[team:gdeliege:shearo|Shearography]]** 
 +</WRAP> 
 +</WRAP> 
 +<WRAP third column> 
 +<WRAP center box 150 centeralign> 
 +[[team:gdeliege:espaint|{{:team:gdeliege:labelesp.png}}]]\\ 
 +**[[team:gdeliege:espaint|Electrostatic painting]]** 
 +</WRAP> 
 +</WRAP> 
 +</WRAP>
  
-The idea is to describe the laminate as a stack of 3D orthotropic plies separated by 2D interfaces. +<WRAP group> 
-In a direction parallel to the fibres, +<WRAP third column> 
-the plies are elastic and subject to brittle fracture; +<WRAP center box 100% centeralign> 
-in shear, an elastoplastic behaviour is assumed and progressive damage is introduced. +[[team:gdeliege:mems|{{:team:gdeliege:labelmems.png}}]]\\ 
-The 2D interfaces between the plies are elastic with progressive damage. +**[[team:gdeliege:mems|Microelectromechanical systems]]** 
-Practical information on the +</WRAP> 
-[[doc:user:elements:volumes:ortho_hypo_materials|orthotropic materials]] +</WRAP> 
-and +<WRAP third column> 
-[[doc:user:elements:volumes:ortho_continuousdamage|damage evolution laws]] +<WRAP center box 150 centeralign> 
-is available on the Metafor web page.+[[team:gdeliege:nnm|{{:team:gdeliege:labelnnm.png}}]]\\ 
 +**[[team:gdeliege:nnm|Nonlinear normal modes]]** 
 +</WRAP> 
 +</WRAP> 
 +<WRAP third column> 
 +<WRAP center box 150 centeralign> 
 +</WRAP> 
 +</WRAP> 
 +</WRAP>
  
-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 127.0.0.1

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