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Blasting plays a crucial role in several engineering applications, from mining and tunneling to demolition projects. One of the remaining challenges of this process is that it can significantly affect the integrity of the rock mass by inducing damage in the form of cracks. Broadening the understanding of the behavior of the blast-induced cracks is essential for predicting the damage. One way of investigating this issue is through small-scale blasting experiments focused on crack propagation behavior. Controlled blasting experiments were conducted on rock-like cylindrical samples charged with Pentaerythritol tetranitrate (PETN) cords. Different blast designs were tested and a method for integrating a Digital Image Correlation (DIC) technique in the analysis was developed. The DIC system was composed of an Ultra High-Speed Camera (UHSC), a light system, and a data acquisition system. The setup was tested in a laboratory and underwent different calibrations before implementing it in the mine, where using explosives during the tests is allowed. The UHSC captured the blasting process regarding crack propagation. To analyze the development of the cracks, DIC technique was employed and results in terms of displacement versus time were measured from the sample surface. The described experiments integrate a novel analysis approach to the results from the DIC technique and propose a way of interpreting the outcomes regarding crack development in terms of velocity. While developing the methodology, the pre-processing of the data (UHSC images) was shown to enhance the DIC analysis and affect the further post-processing of the results. The presented methodology proposes a human-independent procedure of analysis that can help to differentiate the displacement of the crack along its time. Nevertheless, a visual analysis of the results was performed to complement the results and try to broaden the understanding of the crack development process. The DIC results indicated a nonconstant crack propagation velocity while the development patterns were interpreted to match previous literature. The experimental studies confirmed the radial propagation behavior surrounding the blasthole in the single borehole test, while the two borehole configurations show to influence the crack propagation direction and interconnection. This work describes small-scale experiments that provide meaningful insights in crack propagation and how the different blast design parameters can affect their development. The findings of this study could be useful as an input of a predictive tool to assess blast-induced crack initiation and development. / BeFo (Rock Engineering Research Foundation, Sweden) project number 427, “Experimental and Numerical modeling of blast-induced damage around rock tunnel using LS-DYNA”

L’optimisation du dimensionnement des structures passe par une meilleure connaissance de leur mode d’endommagement. Cette étude se focalise donc sur la caractérisation de l’endommagement du contact aube/disque des moteurs aéronautique. Cet assemblage mécanique est soumis a une combinaison d’un effort normal (force centrifuge) et tangentiel (dynamique de l’aube). La portée du disque en Ti-6Al-4V subi donc un chargement complexe de type fretting fatigue. Ce type de sollicitation entraine, entre autre dégradation, de la fissuration dont la modélisation expérimentale et numérique est rendue difficile par les limitations des moyens et des connaissances actuelles. Le premier objectif de ce travail de thèse est de développer un moyen d’essai et une instrumentation associée afin d’étudier de façon qualitative et quantitative la fissuration d’un contact Ti-6Al-4V/Ti-6Al-4V. Le second but est d’utiliser les données issues de ce moyen expérimental afin de proposer un modèle de prédiction des durées de vie de cet assemblage. Un montage inédit de fretting fatigue double vérin mono-contact a été mis en place avec une instrumentation nouvelle pour ce type d’essai : suivi de fissuration par suivi de potentiel et par émission acoustique. Une attention particulière a été apportée aux calibrations et aux méthodologies expérimentales. Ce banc d’essai permet notamment de simuler des efforts de fretting applique en phase ou alors de telle manière a simuler un vrai cycle de vol. Cet outil a permis de décrire quantitativement les premières courbes de Wohler en fretting à amorçage (Effort de fretting vs Nombre de cycles à amorçage) pour deux configurations de contact (cylindre/plan et plan/plan). Les impacts des différents paramètres de fretting sur l’amorcage ont pu être quantifies. Les paramètres influant sont : la configuration du contact, les niveaux des efforts appliques et leur mode de combinaison (cycles en phase ou cycles de type vol). De plus des courbes de cinétique de propagation des fissures ont pu être extraites des différents essais, montrant un fort impact du fretting sur les vitesses de propagation des fissures. Une analyse qualitative via l’émission acoustique a montré un mécanisme d’amorçage et de propagation en 3 étapes suivant la perte d’influence du contact. Un modèle de prédiction de l’amorçage et de simulation de la propagation des fissures a été mis en place. Bien que limite dans la prise en compte des effets gradients (approches non locales), ce modèle se montre très performant surtout dans sa capacité à utiliser les données expérimentales dans l’identification des lois d’amorçage ou de propagation. Ce travail a donc permis d’importantes avancées dans la compréhension des mécanismes de fissuration et dans leur modélisation ouvrant ainsi la porte vers une prédiction fiable de l’endommagement des contacts aube/disque. / Optimization of structures design requires a better understanding of their damage process. This study focuses on the characterisation of the blade/disk contact damaging process on aircraft engines. That mechanical structure is subjected to a normal load (centrifugal forces) combined with a tangential force (blade dynamic). Thus the Ti-6Al-4V disk seat sees a complex fretting fatigue loading. This type of solicitation can generate a series of degradations like cracking. Experimental and numerical simulation of this damaging is very difficult considering the present state of arts. The first aim of this work is to develop a new experimental set-up with the appropriate instrumentation in order to conduct a qualitative and a quantitative analysis of the cracking in a Ti-6Al-4V/Ti6-Al-4V contact. The second goal is to build a life prediction numerical model that would be able to use the data obtain with the new experimental tests. The new dual-actuator fretting-fatigue set-up is now operational. It allows to run single contact test under different loading combinations: fretting and fatigue loads can be applied in phase or in a way to simulate the real ‘in flight’ conditions. New instrumentations have been added in order to follow the crack initiation and propagation: potential-drop technique and acoustic emission. Thanks to this new test procedure, the first fretting Wöhler curve to crack nucleation have been described (fretting load vs number of cycles to crack nucleation) for two contact geometries (cylinder on flat and flat on flat). The separate influences of fatigue and fretting parameters have been determined. The mains parameters are: the contact characteristics, the stress level and the force combination modes (‘in phase’ cycles or ‘in-flight’ cycles). Moreover, the very first crack propagation kinetics have been drowned. Also, a major influence of the fretting on the crack propagation has been exposed. The qualitative analysis conducted with the acoustic emission has revealed a three steps crack propagation process. The crack propagation process evolves with the decrease of the contact influence. A model has been developed in order to predict crack initiation and propagation lives. Even if the model suffers from a major limitation due to the difficult considerations of the stress gradient effects, it has shown very good results through its ability to directly include experimental data. This work has led to major breakthroughs in the understanding of the cracking mechanisms and their simulation. This forms solid foundations for future predictions of the blade/disk interface durability.

<p>Predmet ove doktorske disertacije je definisanje metoda i procedure<br />za procenu veka konstrukcije tornja postrojenja za istraživanje nafte<br />i gasa. Dati su rezultati eksperimentalnih istraživanja radi analize<br />otpornosti prema prslinama pri statičkom i pri promenljivom<br />opterećenju eksploatisanog i novog materijala konstrkcije tornja<br />postrojenja za istraživanje nafte i gasa.</p> / <p>The topic of this doctoral dissertation is definition methods and proceduries for an<br />analysis of an assessmen life of construction derrick plant for investigation oil<br />and gas. The results of experimental investigation performed for the analysis<br />of crack resistance under static and under variable loading eksploatacion<br />and new of materials of construction derrick plant for investigation oil and gas.</p>

Dans le contexte général lié aux économies d’énergie, l’amélioration sensible du rendement des turbines à gaz (aéronautiques ou terrestres), nécessitera d’augmenter notablement la température des gaz de combustion. Cela implique l’emploi de matériaux stables au-delà de 1 500°C. Les céramiques eutectiques préparées par solidification dirigée, à partir des systèmes Al2O3 - Ln2O3 (où Ln représente un élément lanthanide ou l’yttrium) sont une solution envisageable. En effet, leur microstructure, constituée d’un réseau interpénétré 3D de deux phases monocristallines, et exempte de pores, de colonies et de joints de grains, confère à ces systèmes eutectiques des propriétés mécaniques d’un bon niveau, et quasi-constantes jusqu’à des températures proches de leur température eutectique (> 1 700°C). Nos travaux ont consisté à élaborer plusieurs systèmes eutectiques binaires et ternaires, par ajout d’une phase ZrO2 renforçante. Les six systèmes présentant les microstructures les plus prometteuses (3 binaires : Al2O3 - Y3Al5O12, Al2O3 - Er3Al5O12, Al2O3 - GdAlO3, et 3 ternaires : Al2O3 - Y3Al5O12 - ZrO2, Al2O3 - Er3Al5O12 - ZrO2, Al2O3 - GdAlO3 - ZrO2) ont été retenus pour étudier certaines de leurs propriétés mécaniques. Plusieurs modes de fissuration, allant dans le sens de l’augmentation de ténacité détectée dans ces systèmes, ont été décelés après des essais de flexion biaxiale. Ces modes de fissuration ont été corrélés aux caractéristiques microstructurales et à la distribution des contraintes résiduelles, déterminées par le calcul et mesurées par une méthode piézo-spectroscopique. Enfin, l’étude du comportement en fluage à haute température a permis de mettre en évidence une évolution des mécanismes de déformation en fonction des conditions de sollicitation. L’étude MET post mortem a également souligné l’influence marquée du caractère interconnecté de la microstructure sur le comportement en fluage. / In the general context of energy savings at a global scale, the improvement of the thermal efficiency of both terrestrial and aeronautical gas turbines will require to increase the turbine inlet gas temperature. The development of new materials, stable up to 1 500°C, is thus necessary. In this context, Directionally Solidified Eutectic Ceramics (DSEC), prepared from Al2O3 and Ln2O3-based systems, could be a potential solution. Their microstructure consists of two single-crystal phases continuously entangled in a threedimensional interpenetrating network without grain boundaries, pores or colonies. The outstanding stability of these microstructures gives rise to a high strength and creep resistance at high temperature. Our research consisted first in obtaining, by directional solidification, several eutectic systems, either binary or ternary (with addition of a toughening third ZrO2 phase). The six most promising DSEC (3 binary systems: Al2O3 - Y3Al5O12, Al2O3 - Er3Al5O12, Al2O3 - GdAlO3, and 3 ternary systems: Al2O3 - Y3Al5O12 - ZrO2, Al2O3 - Er3Al5O12 - ZrO2, Al2O3 - GdAlO3 - ZrO2) have then been selected to study some of their mechanical properties. Several crack propagation patterns have been detected after biaxial flexure testing, and partially explain the toughening which has been proven for DSEC. Attention has been paid to the possibility of crack deflection in the various phases and in the phase boundaries, a phenomenon which may markedly improve the toughness of these eutectic ceramics. These observations have been correlated to internal stress calculations and piezo-spectroscopic measurements. Finally, the study of the creep behavior showed that the deformation mechanisms evolve with the macroscopic solicitation (temperature and stress). microstructure. Moreover, post mortem TEM observations exhibited that creep mechanisms are strongly dependant on the entangled microstructure.

[pt] Neste trabalho são investigadas experimentalmente e numericamente as mudanças de geometria em trincas inicialmente passantes submetidas a carregamento remoto de flexão pura induzindo fechamento parcial das faces da trinca. Esse crescimento de trinca pode ocorrer numa variedade de estruturas com defeitos pré-existentes, tais como fuselagens de aviões, cascos de navios, vasos de pressões e pontes metálicas. O carregamento de flexão pura ocasiona regiões de tração e compressão na frente da trinca. É inquestionável que parte das faces da trinca sob compressão fecha independentemente de qualquer mecanismo de fechamento; e outra parte das faces da trinca, por outro lado, sob tração cresce mudando gradualmente de geometria. Após realizar ensaios em corpos-de-prova de aço ASTM A-36, foi observado que tais carregamentos geram uma quina na frente da trinca, que é a transição de uma geometria parcialmente passante e um trecho remanescente da geometria inicial. Para entender a distribuição do fator de intensidade de tensão em tais frentes de trinca, suas geometrias foram reproduzidas em um modelador tridimensional de mecânica da fratura linear elástica, o FRANC3D, acoplado a um programa de análise de elementos finitos (ABAQUS). Com este sistema acoplado, foram executadas análises considerando efeitos não lineares causados pelo contato das faces da trinca sob compressão. Verificou-se a necessidade de propor metodologias para tratamento dos resultados numéricos na quina, obtendo-se predições eficientes das mudanças na geometria da trinca. Contudo, a estimativa de vida, quando se compara taxas de crescimento da trinca obtidas em um corpo-de-prova sob tração cíclica e as taxas em um corpo-de-prova sob flexão com fechamento parcial da trinca, foi melhor reproduzida usando um fator de correção de fechamento da trinca. Adicionalmente, uma série de expressões empíricas normalizadas para geometrias da trinca e fatores de intensidade de tensão são propostas. / [en] This work investigates experimentally and numerically how the front of initially through edge cracks in plate changes after they pass to be remotely fatigue loaded under pure bending to induce partial closure of the crack faces. This type of crack growth problem can occur in a variety of structures with preexisting defects, such as aircraft fuselages, ship hulls, pressure vessels components, and steel bridges. The bending loads induce tension and compression regions along the crack front, with the part of the crack faces that work under compression undoubtedly closed by the load, independently of any other closure mechanism. The part of the crack faces that work under tension; on the other hand, crack grows by fatigue gradually changing its shape. After performing tests on ASTM A36 steel specimens, it was observed that the bending load induces a kink on the crack front, in the transition between the part through crack created on the tension side and initial crack geometry. To understand the distribution of the stress intensity factor along such crack fronts, the measured crack shapes were reproduced in a three-dimensional fracture mechanics modeler (FRANC3D) coupled to a finite element analysis program (ABAQUS). With this coupled system, linear elastic stress analysis simulations were performed considering the nonlinear effects caused by the crack face contact in the compressed region. In particular, methods had to be proposed to treat numerical noise around the kink. The proposed methodology efficiently predicts the observed crack front shape changes; although the observed fatigue lives were better reproduced using a crackclosure correction factor when compared to crack growth data obtained from standard compact tension specimens. In addition, a series of normalized empiric expressions for both crack front shapes and stress intensity factors are proposed.

Este trabalho apresenta um modelo numérico para a análise da propagação de fissuras em estruturas bidimensionais não-homogêneas. O comportamento mecânico é simulado a partir da formulação elastostática do Método dos Elementos de Contorno (MEC) aplicada a materiais isotrópicos. O MEC é uma eficiente e robusta técnica numérica para análises de propagação de fissuras. A não exigência de uma malha de domínio pelo método permite uma representação precisa da concentração de tensão nas pontas. Além disso, a redução da dimensionalidade proporcionada pelo MEC facilita o processo de remalhamento durante o crescimento das fissuras. A formulação dual do MEC é adotada, na qual as equações integrais singular e hipersingular são aplicadas. A modelagem de domínios não-homogêneos é realizada a partir da técnica de sub-regiões. A Mecânica da Fratura Elástico-Linear (MFEL) é aplicada para a análise da fratura em materiais frágeis. Os fatores de intensidade de tensão são determinados a partir da integral-J e a teoria da máxima tensão circunferencial é adotada para definir a direção de propagação das fissuras e o fator de intensidade de tensão equivalente. Problemas envolvendo fraturamento hidráulico também são investigados a partir da aplicação da MFEL. A integral-J é modificada para a consideração da pressão hidrostática atuante sobre as faces da fissura. Estruturas sujeitas à fadiga de alto ciclo também são avaliadas. A lei de Paris é utilizada para a estimativa da taxa de crescimento das fissuras. O último tipo de problema considerado é a fratura em materiais quase-frágeis. O modelo de fissura coesiva é empregado para a representação do comportamento não-linear físico próximo à ponta. O sistema de equações não-linear obtido é resolvido a partir de um algoritmo iterativo denominado operador constante. O estado de tensão na ponta, determinado por extrapolação, é utilizado para a verificação da estabilidade à propagação e o caminho de crescimento é definido a partir da formulação da MFEL. São observadas boas correspondências entre os resultados obtidos e as respostas encontradas na literatura, indicando a eficiência e a robustez do código computacional proposto. Melhorias do modelo numérico implementado também são discutidas. / This work presents a numerical approach for crack propagation modelling in non-homogeneous two-dimensional structures. The mechanical structural behaviour is simulated using the elastostatic formulation of the Boundary Element Method (BEM) applied to isotropic materials. The BEM is an efficient and robust numerical technique for crack propagation analyses. The non-requirement of a domain mesh enables the BEM for accurately quantifying the stresses concentration at the crack tip. Moreover, the mesh dimension reduction provided by the BEM makes the remeshing procedures during crack growth a less complex task. The dual BEM formulation is adopted, in which singular and hypersingular integral equations are applied. The non-homogeneous domains are modelled using the sub-region technique. The Linear Elastic Fracture Mechanics (LEFM) is applied to analyze the fracture in brittle materials. The stress intensity factors are evaluated through the J-integral and the maximum circumferential stress theory is adopted to define the crack propagation angle and the equivalent stress intensity factor. Problems involving hydraulic fracture (fracking) are also investigated applying the LEFM. A modified J-integral scheme is implemented to consider the hydrostatic pressure acting at the crack faces. Structures subjected to high-cycle fatigue are also addressed. The Paris law is used to estimate the crack growth rate. The last type of problem considered is the fracture in quasi-brittle materials. The cohesive crack model is used to represent the material nonlinear behaviour next to the crack tip. The nonlinear system of equations obtained is solved by an iterative algorithm named constant operator. The state of stress at the tip, obtained by extrapolation, is used to verify crack growth stability and the crack path is defined by the LEFM formulation. Good agreement is observed among the results achieved by the BEM model and the responses available in literature, showing the efficiency and robustness of the proposed numerical scheme. Further improvements of the BEM code are also discussed.

Os tratamentos de cementação, têmpera, revenimento e jateamento por granalhas são muito utilizados na produção seriada de peças da indústria automobilística, como engrenagens e eixos. Variações destes processos podem influenciar a vida em fadiga por flexão dos componentes descritos. O objetivo deste trabalho foi estudar a influência de variações no tempo de jateamento por granalhas, variações na temperatura de revenimento e de diferentes profundidades de oxidação intergranular, no crescimento de trincas curtas por fadiga na camada cementada do aço DIN 20MnCr5. Para isso foram feitos ensaios de fadiga por flexão em quatro pontos, utilizando corpos de prova de seção retangular e sem entalhe. Para o acompanhamento do crescimento de trincas curtas foi utilizado o método de réplicas de acetato. Foram estudados seis níveis de jateamento, quatro níveis de revenimento e dois níveis de oxidação intergranular. Como resultados principais, foram obtidas curvas de comprimento de trinca por número de ciclos e taxa de crescimento de trinca por tamanho médio da trinca. Amostras jateadas entre trinta minutos e uma hora, revenidas à 160&#176C e com oxidação intergranular por volta de dez mícrons, apresentaram os melhores resultados em relação à vida em fadiga. / Carburizing, quenching, tempering and shot peening treatments are often used in mass production of automotive parts, such as gears and shafts. Changes in these treatments can influence the bending fatigue life of these parts. The purpose of this study was to measure the influence of different shot peening times, different tempering temperature and different internal oxidation depths, on the short fatigue crack growth in case carburized DIN 20MnCr5 steel. Four-point-bend fatigue tests were carried out in rectangular section specimens without notch. The surface short crack growth was monitored by means of acetate replication technique. Six levels of shot peening, four levels of tempering temperatures and two levels of internal oxidation were studied in this work. Crack length versus number of cycles and crack growth rate versus mean crack length were obtained as principal results. Shot peening from 30 minutes to one hour, tempering at 160#176C and a lO~m depth of internal oxidation showed the best results in fatigue life.

No presente trabalho desenvolve-se um modelo constitutivo baseado na mecânica do dano contínuo para representar o acúmulo da degradação do concreto produzido por cargas repetidas. O modelo de dano apresenta as condições necessárias exigidas na chamada aproximação de descontinuidades fortes proposta por Simó, Oliver e Armero e, conseqüentemente, pode ser empregado na formulação de elementos finitos com descontinuidade forte incorporada. Em decorrência de sua capacidade de descrever o comportamento do meio descontínuo independentemente da posição dos contornos do elemento finito, essa classe de formulação constitui uma alternativa valiosa para remediar a forte dependência da malha observada nos modelos de fissuras distribuídas, assim como para evitar as sofisticadas técnicas de reconstrução da malha exigidas nos modelos de fissura discreta, nos quais a fissura é introduzida na interface entre elementos. O trabalho traz contribuições no sentido de proporcionar uma ferramenta alternativa para a análise de propagação de fissuras por fadiga em elementos estruturais de concreto, dentro do contexto da mecânica do dano contínuo. Verifica-se a eficiência da formulação mediante análise numérica de problemas de fadiga em elementos estruturais de concreto. / A constitutive model based on the continuum damage mechanics is proposed to describe the accumulation of the degradation produced by repeated loads in concrete materials. The proposed damage model presents the necessary conditions required in the strong discontinuity approach advocated by Simó, Oliver and Armero and, consequently, it can be used in the embedded strong discontinuity finite element approach. This class of approach has been recognized by its capability to model discontinuities independently on the element boundaries. In fracture mechanics, the embedded strong discontinuity element has been proved to be a efficient alternative to remedy the strong mesh dependence verified in smeared crack approaches, as well as to avoid the sophisticated remeshing techniques required in the discrete crack approaches, in which the crack is introduced in the element interfaces. This work provides an alternative tool for the analysis of crack propagation in concrete structures under fatigue in the context of the continuum damage mechanics. Numerical analysis of concrete elements under fatigue are performed to access the effectiveness of the proposed approach.