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       <dc:date>2026-04-10T09:22:29+00:00</dc:date>
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        <dc:date>2016-03-30T13:23:04+00:00</dc:date>
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        <title>Composite materials</title>
        <link>http://metafor.ltas.ulg.ac.be/dokuwiki/team/gdeliege/composite?rev=1459344184&amp;do=diff</link>
        <description>Composite materials

Background

Carbon-Fibre-Reinforced Polymers (CFRP) are now widely used in aerospace industry
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 macroscopi…</description>
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        <dc:date>2016-03-30T13:23:04+00:00</dc:date>
        <dc:creator>Anonymous (anonymous@undisclosed.example.com)</dc:creator>
        <title>Electrostatic painting</title>
        <link>http://metafor.ltas.ulg.ac.be/dokuwiki/team/gdeliege/espaint?rev=1459344184&amp;do=diff</link>
        <description>Electrostatic painting

Problem description

Electrostatic painting is one of the applications I studied during my PhD.
I started from a mathematical model by François Henrotte [1]
and used this nice coupled problem to test different potential and mixed formulations
of electrostatic equations.$$
\begin{eqnarray*}
\nabla\cdot\vec{d} &amp;=&amp; \rho_i \\
\nabla\times\vec{e} &amp;=&amp; 0 \\
\vec{d} &amp;=&amp; \varepsilon_0\vec{e} \\
\partial_t \rho_i +\nabla\cdot( \mu_i\vec{e}\rho_i) &amp;=&amp; 0
\end{eqnarray*}$
where $$\vec…</description>
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        <dc:date>2016-03-30T13:23:04+00:00</dc:date>
        <dc:creator>Anonymous (anonymous@undisclosed.example.com)</dc:creator>
        <title>Microelectromechanical systems</title>
        <link>http://metafor.ltas.ulg.ac.be/dokuwiki/team/gdeliege/mems?rev=1459344184&amp;do=diff</link>
        <description>Microelectromechanical systems

Background

I worked on a research project over microelectromechanical systems (MEMS)
in the Aerodynamics group of Prof. Essers.
This project was a collaboration between several research groups of the Université de Liège:
Aerodynamics, Mechanical Vibrations (Prof. Golinval) and Applied and Computational Electromagnetics
(W. Legros).
My objective in this project was to simulate the deformation of microactuators
taking into account the damping effect of air.
These m…</description>
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        <dc:date>2016-03-30T13:23:04+00:00</dc:date>
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        <title>Nonlinear normal modes</title>
        <link>http://metafor.ltas.ulg.ac.be/dokuwiki/team/gdeliege/nnm?rev=1459344184&amp;do=diff</link>
        <description>Nonlinear normal modes

Background

Nonlinear normal modes (NNMs) are an extension of linear normal modes to nonlinear systems.
This is one of the research topics of the 
Space Structures &amp; Systems Lab. (Prof. Kerschen).
Actually, I knew nothing of the subject until Ludovic Renson
told me about it
and about the nonlinear equations he wanted to solve with finite elements.
The idea to be faced with
an unusual set of PDEs was too much of a temptation
and I decided to implement a simple case in my o…</description>
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        <dc:date>2016-03-30T13:23:04+00:00</dc:date>
        <dc:creator>Anonymous (anonymous@undisclosed.example.com)</dc:creator>
        <title>Shearography</title>
        <link>http://metafor.ltas.ulg.ac.be/dokuwiki/team/gdeliege/shearo?rev=1459344184&amp;do=diff</link>
        <description>Shearography

Introduction

I am no shearography expert, so I will quote J.-F. Vandenrijt [1] for a proper definition:
Shearography records the interference pattern between a speckle object wavefront
and itself laterally displaced through an optical shearing device.
Such interference patterns, so-called shearograms, are recorded at different instants
between which the inspected object undergoes a certain stress
(thermal, mechanical, pressure variation, vibration).
The numerical difference betwee…</description>
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