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Faculté des Sciences appliquées
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Master thesis and internship[BR]- Master's thesis : The validation process of virtual crash testing of vehicle restraint system[BR]- Integration Internship

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Orabi, Tarek ULiège
Promotor(s) : Duysinx, Pierre ULiège
Date of defense : 27-Jun-2022/28-Jun-2022 • Permalink : http://hdl.handle.net/2268.2/14498
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Title : Master thesis and internship[BR]- Master's thesis : The validation process of virtual crash testing of vehicle restraint system[BR]- Integration Internship
Translated title : [fr] MODÈLES DE VÉHICULES POUR LES SIMULATIONS DE CRASH
Author : Orabi, Tarek ULiège
Date of defense  : 27-Jun-2022/28-Jun-2022
Advisor(s) : Duysinx, Pierre ULiège
Committee's member(s) : Himpe, Jeffrey 
Noels, Ludovic ULiège
Bruls, Olivier ULiège
Language : English
Number of pages : 73
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Funders : GDTech
Name of the research project : The validation process of virtual crash testing of vehicle restraint system
Target public : Student
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

[fr] The main objective of this work is to validate and verify the virtual crash test of the vehicle restraint system by using Hyper-mesh software to generate the mesh and LS-Dyna
software for pre and post-processing. The test was conducted in compliance with European standard EN 1317. These standards are the impact severity index level for the vehicle,
the deformation of the system which is expressed as working width and vehicle intrusion
including the normalized values, and the containment level of the vehicle. The barrier that
has been used in this test is 3N.TU-BPL.71 and two types of vehicles TB11 and TB61 were
tested. First, the model is built up followed by meshing each part separately using the hyper mesh software then assembling the parts and setting the parameters, constitutive law,
and the boundary condition using LS-Dyna software. Then, three tests were performed the
first one is just the barrier with applied gravity to check the numerical stability, the second
test is the barrier with vehicle TB11, and the last test is the barrier with vehicle TB61. The
results were validated in accordance with the European standard properly whereas the deformation of some parts of the barrier against TB61 was not as same as the physical one
whereas for TB11 the deformation was almost the same. To conclude, the virtual test and
the physical test have similarities and differences as it is impossible to reproduce the same
deformation as in reality, taking into account that the virtual test is a numerical way aimed
to have approximation results not the same results since the numerical way based on many
assumptions. For example, the discretization in space is the first error produced in the software, and the time discretization by using an explicit scheme is the second error produced
in the software.


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Author

  • Orabi, Tarek ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promotor(s)

Committee's member(s)

  • Himpe, Jeffrey GDTech
  • Noels, Ludovic ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Computational & Multiscale Mechanics of Materials (CM3)
    ORBi View his publications on ORBi
  • Bruls, Olivier ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Laboratoire des Systèmes Multicorps et Mécatroniques
    ORBi View his publications on ORBi
  • Total number of views 45
  • Total number of downloads 2










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