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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS
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Numerical simulations of non-destructive testing procedure by shearography and thermography

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Saint-Mard, Nicolas ULiège
Promotor(s) : Noels, Ludovic ULiège
Date of defense : 24-Jun-2021/25-Jun-2021 • Permalink : http://hdl.handle.net/2268.2/11520
Details
Title : Numerical simulations of non-destructive testing procedure by shearography and thermography
Translated title : [fr] Simulations numériques des procédures de tests non-destructifs par shearographie et thermographie
Author : Saint-Mard, Nicolas ULiège
Date of defense  : 24-Jun-2021/25-Jun-2021
Advisor(s) : Noels, Ludovic ULiège
Committee's member(s) : HOFFAIT, Sébastien 
Bruyneel, Michaël ULiège
Georges, Marc ULiège
Language : English
Number of pages : 87
Keywords : [en] Numerical Simulations
[en] Shearography
[en] Thermography
[en] Delamination models
[en] Porosity models
[en] Experimental validation
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Target public : Researchers
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 intrinsic structure of composites can lead to defects decreasing their reliability and their
in-mission security. Numerical simulations aiming to improve and support defect detection are envisaged in this work. More precisely, shearography and thermography as non-destructive detection methods are being modeled here. Two defect types are considered: delamination and porosity.

Detection is investigated with external thermal excitation, leading to thermal and mechanical
analysis in simulations. Firstly, an overview of composites, their defects and non-destructive techniques is addressed. Secondly, prerequisites for simulations like governing equations and assumptions made, the heater characterization, and the numerical scheme used for the transient thermal problem resolution are exposed. Then, defect numerical models are constructed and studied. Delamination and porosity are the two types of defects considered. Numerical models for the delamination covered true delamination and artificial delamination like the physic insert and flat bottom hole models. The porosity model is represented by a few flat bottom holes localized in a small region. Finally, an experimental approach compared with numerical results is used as a validation method.

Different delamination models are developed and they show pretty well concordances between
them, except for the Teflon layer (type of physic insert) model for which the mechanical response
was not expected or at least, suggests a further study to determine its validity. The porosity model showed difficulties in this kind of defect detection. Finally, the experimental approach enabled to see that numerical and experimental results were similar but that some efforts on parameter updating remain to be made. Mainly the characterization of the lamp that irradiates a highly non-homogeneous flux.


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Author

  • Saint-Mard, Nicolas ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promotor(s)

Committee's member(s)

  • HOFFAIT, Sébastien V2i
  • Bruyneel, Michaël ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Modél. num. du comport. des struct. en matériaux composites
    ORBi View his publications on ORBi
  • Georges, Marc ULiège Université de Liège - ULiège > CSL (Centre Spatial de Liège)
    ORBi View his publications on ORBi
  • Total number of views 42
  • Total number of downloads 37










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