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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS

Numerical and Experimental Study of an Omnidirectional Vibro-Impact Nonlinear Energy Sink ISAE-SUPMECA

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Lami, Souhaïl ULiège
Promotor(s) : Salles, Loïc ULiège
Date of defense : 29-Jun-2026/30-Jun-2026 • Permalink : http://hdl.handle.net/2268.2/26090
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Title : Numerical and Experimental Study of an Omnidirectional Vibro-Impact Nonlinear Energy Sink ISAE-SUPMECA
Translated title : [fr] Étude numérique et expérimentale d’un absorbeur d’énergie non linéaire vibro-impact omnidirectionnel
Author : Lami, Souhaïl ULiège
Date of defense  : 29-Jun-2026/30-Jun-2026
Advisor(s) : Salles, Loïc ULiège
Committee's member(s) : Raze, Ghislain ULiège
Lo Feudo, Stefania 
Job, Stéphane 
Language : English
Number of pages : 88
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Institution(s) : Université de Liège, Liège, Belgique
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[en] The objective of this work was to study an omnidirectional vibro-impact non-
linear energy sink composed of an internal cylindrical mass moving inside a circular
Host. The work was divided into two main parts: the development of numerical
models and the experimental study of several OVINES configurations.
First, a numerical OVINES model was developed in Python. The gravitational
force was taken into account for the NES in order to perform different validation
tests, including energy conservation and comparisons of rebound heights with the-
oretical values. Friction was then added to the model, and a new configuration
with springs and dampers between the Host and the ground was also studied. This
model shows that successive impacts transfer part of the energy from the Host to
the NES and redistribute the motion among the translational and rotational degrees
of freedom.
The second part of the work focused on the experimental study. A two-camera
measurement setup was used to reconstruct the three-dimensional motion of the
system. Several OVINES configurations were tested in order to reconstruct the
relative trajectory of the NES, estimate its angular position and rotational velocity,
detect impacts, and perform a first identification of the impact parameters.
A preliminary parameter identification was performed using selected impacts.
The normal restitution coefficient was identified from five impacts, giving a mean
value of approximately 0.72 and a standard deviation of 0.12. The collision friction
coefficient and the tangential restitution coefficient were estimated from two selected
impacts, giving indicative mean values of approximately μc = 0.129 and β0 = 0.494.
These values should be considered as preliminary estimates due to the limited num-
ber of analysed impacts and the experimental limitations related to marker tracking,
geometry reconstruction and measurement accuracy.


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Author

  • Lami, Souhaïl ULiège Université de Liège > Master ing. civ. aéro., fin. spéc. aer. eng.

Promotor(s)

Committee's member(s)

  • Raze, Ghislain ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire de structures et systèmes spatiaux
    ORBi View his publications on ORBi
  • Lo Feudo, Stefania
  • Job, Stéphane








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