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Advanced approach for mixed mode crack propagation

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Rajaraman, Dhanraj ULiège
Promotor(s) : Ponthot, Jean-Philippe ULiège
Date of defense : 26-Jun-2017/27-Jun-2017 • Permalink : http://hdl.handle.net/2268.2/2570
Details
Title : Advanced approach for mixed mode crack propagation
Author : Rajaraman, Dhanraj ULiège
Date of defense  : 26-Jun-2017/27-Jun-2017
Advisor(s) : Ponthot, Jean-Philippe ULiège
Committee's member(s) : Noels, Ludovic ULiège
Chary, Charles 
Canales Cardenas, Cristian ULiège
Language : English
Number of pages : 100
Keywords : [en] Crack propagation, Mixed mode loading, Crack box technique, Fatigue loading, Static loading, Bifurcation angle
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Commentary : This Document is restricted for all users and is accessible only to the member committee and the Company persons
Funders : KTH Royal institute of technology,Sweden
Research unit : SONACA Group, Gosselies, Belgium
Name of the research project : Fracture mechanics in stress department
Target public : Researchers
Professionals of domain
Student
Institution(s) : Université de Liège, Liège, Belgique
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "turbomachinery aeromechanics (THRUST)"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[en] In practical cases, manufacturing of components are not always perfect. The influence of cracks on structures are of interest here. In SONACA, Extended Finite Element Method (XFEM) was used earlier for the prediction of crack propagation and bifurcation angle. But due to some difficulties, we have developed a technique called Crack Box Technique (CBT) which had some difficulty in implementing into the model and is overcome by a new technique. In this thesis work, our objective is to confront the crack box approach for different models and analyse the results. A single edge notched specimen under tension of Steel materials is selected for static load cases. The results are successfully confronted using the crack box approach, analytical calculation and compared with the literature results.
Then, we wanted to use the Crack Box Technique to determine the behaviour of crack propagation by fatigue load and the propagation path of the crack. The Compact Tension Shear (CTS) specimen under mixed mode loading is considered. The bifurcation angle is determined using the various available bifurcation criteria. The equivalent stress intensity factor is determined and crack propagation is studied using various approaches and compared with the crack box results.


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Author

  • Rajaraman, Dhanraj ULiège Université de Liège > Master ingé. civ. aérospat., à fin. (THRUST)

Promotor(s)

Committee's member(s)

  • Noels, Ludovic ULiège Université de Liège - ULg > Département d'aérospatiale et mécanique > Computational & Multiscale Mechanics of Materials (CM3)
    ORBi View his publications on ORBi
  • Chary, Charles
  • Canales Cardenas, Cristian ULiège Université de Liège - ULg > Département d'aérospatiale et mécanique > LTAS-Mécanique numérique non linéaire
    ORBi View his publications on ORBi
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