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team:gdeliege [2015/08/10 17:21] – [Composite materials] geoffreyteam:gdeliege [2015/08/13 19:07] geoffrey
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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 \\ +<code> 
-B-4000 Liège, BELGIUM  \\+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>
  
 ===== Research activities ===== ===== Research activities =====
  
-==== Composite materials ==== +<WRAP group> 
- +<WRAP third column> 
-Carbon-Fibre-Reinforced Polymers (CFRP) are now widely used in aerospace industry +<WRAP center box 100% centeralign> 
-thanks to their high strength-to-weight ratio+[[team:gdeliege:composite|{{:team:gdeliege:labelcomposite.png}}]]\\ 
-However, the numerical simulation of CFRP laminates up to failure is not trivial+**[[team:gdeliege:composite|Composite materials]]** 
-laminates have anisotropic mechanical properties and +</WRAP> 
-damage results from a combination of microscopic mechanisms +</WRAP> 
-(fibre brittle failure, fibre-matrix debonding, matrix ductile failure and delamination) +<WRAP third column> 
-that are not easily described at a macroscopic level.+<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>
  
-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 P. Ladevèze and OAllix [1-2for unidirectional +[[team:gdeliege:mems|{{:team:gdeliege:labelmems.png}}]]\\ 
-composites as well as the 2D model for woven composites proposed by CHochard [3].+**[[team:gdeliege:mems|Microelectromechanical systems]]** 
 +</WRAP> 
 +</WRAP> 
 +<WRAP third column> 
 +<WRAP center box 150 centeralign> 
 +[[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>
  
-The idea is to describe the laminate as +===== Skills and competences =====
-a stack of 3D homogeneous plies separated by 2D interfaces. +
-The plies are orthotropic with an elastic behaviour and brittle failure +
-along the fibres +
-and an elastoplastic behaviour with progressive damage in shear. +
-The 2D interfaces between the plies are elastic with progressive damage.+
  
-One interesting feature of Ladevèze and Allix's work is that the parameters +**Languages** 
-of the constitutive laws can be linked to physical quantities, +  * French (mother tongue) 
-which allows their identification with suitable experimental tests.+  * English (advanced) 
 +  * Dutch (advanced)
  
-== Bibliography == +**IT** 
-[1] P. Ladevèze, E. Le Dantec. //Damage modelling of the elementary ply for laminated composites.// Composites Science and TechnologyVol. 43pp. 257-2671992 \\ +  * software development : C/C++PythonMatlab, parallel programming tools (MPI)version control tools (Subversion) 
-[2] O. Allix, P. Ladevèze. //Interlaminar interface modeling for the prediction of laminate delamination.// Composite StructuresVol. 22pp. 235-242, 1992 \\ +  * finite element software (university code ; Samcef ; marginal use of MagNetANSYSLS-DYNA) 
-[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 \\+  * Linux system management
  
-{{ :team:gdeliege:metafor_300dpi.jpg?400 |Stiffener}} 
  
 ===== Publications ===== ===== Publications =====
team/gdeliege.txt · Last modified: 2024/02/26 14:09 by boman

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