Atmospheric icing presents serious challenges to the development of wind power of the wind energy industry in cold regions. The potential detrimental impact on the safe operation of wind turbines and the energy harvest hasn't been fully understood and requires further investigation. This thesis presents the research on icing profiles under different weather conditions and their impact on natural frequency, fatigue life, and lift and drag of the wind turbine blade. The research aims to develop a further understanding of the effect of atmospheric ice accretion on the structural integrity and aerodynamic performance of wind turbine blades through numerical and aerodynamic investigations to address the challenges facing the industry. A 5-MW NREL (National Renewable Energy Laboratory) wind turbine blade was selected for this study, due to availability of required geometric design parameters and experimental data for verification. The turbine rotor and its three blades were modelled and numerically simulated with commercial finite element software ANSYS. Three icing scenarios were chosen according to the ISO Standard and the corresponding icing profiles were developed to investigate their influence on vibrational behaviours of the wind turbine blade and rotor under different weather conditions. Icing loads were applied on the leading edge of the blade and natural frequency results were compared between clean and iced blades. It was found that harsh icing weather drove the natural frequency down to the near resonance limit, which could lead to significant issue on structural integrity of the wind turbine. The effect of atmospheric ice accretion with additional load due to varying wind speeds on the fatigue life of the wind turbine blade has been investigated. Significant reduction of fatigue life was found due to the increase of the von Mises stresses. Finally, computational fluid dynamics (CFD) analysis was carried out to investigate the effect of atmospheric ice accretion on the aerodynamic performance of typical 1-MW and 5-MW wind turbine blades. Results of the drag and lift coefficients and power production under different icing scenarios were obtained for five angles of attack. Compared with the results of the clean aerofoil profile, remarkable reduction in the power generation was observed due to the accreted ice at various aerofoil sections in the spanwise direction of the blade, demonstrating the detrimental impact of atmospheric icing on energy harvest for the wind energy industry.

L’estimation de la durée de vie et de la rupture de structures composées par des matériaux quasi-fragiles nécessite le développement de nouveaux modèles théoriques et numériques. Dans ce travail, la modélisation de l’apparition des fissures et leur propagation en chargement monotone est d'abord étudiée. Un modèle d'effet de taille pour les structures fissurées et sa forme généralisée pour les structures présentant des défauts plus complexes qu’une fissure sont développés. Les prédictions du modèle de rupture sont comparées à des résultats expérimentaux de la littérature pour divers spécimens composés de différents matériaux et de différentes tailles. Des échantillons présentant des défauts initiaux en forme de V et en forme de trou illustrent les capacités de la formulation. Ensuite, l’endommagement et la fissuration induite par des chargements cycliques en fatigue sont discutés. Un modèle local en éléments discrets est développé, qui permet de coupler les deux mécanismes (endommagement et fissuration). Les prédictions numériques sont comparées aux résultats théoriques et expérimentaux. À la fin, les applications associées au comportement du béton bitumineux renforcé par des grilles en fibres de verres sont analysées en détail. / The prediction of the fatigue life and the rupture of structures made of quasi-brittle materials requires the development of new theoretical and numerical models. In this work, the modelling of the crack initiation and propagation under monotonic loading is firstly investigated. A size effect model for cracked structures and its generalized form for structures with defects more complex than a crack are developed. The predictions of the proposed model are compared with experimental results from the literature for various specimens of different materials and sizes. Samples with initial V-shaped and hole-shaped defects exemplify the formulation's capabilities. Then, the damage and cracking induced by cyclic fatigue loads is discussed. A local model using discrete elements is developed, that allows the coupling of two mechanisms (damage and fatigue cracking). The numerical results are compared to those of experimental bending fatigue tests. Finally, applications associated with the behavior of fiber glass reinforced asphalt concrete are analyzed in detail.

Atualmente, a exigência da indústria na construção de estruturas complexas é consequência da acirrada concorrência, principalmente, entre empresas dos segmentos rodoviários. Com o auxílio de ferramentas computacionais, baseadas no Método de Elementos Finitos, é possível dimensionar essas estruturas submetidas a solicitações aleatórias variando no tempo. Nesse caso, é comum a realização de simulações dinâmicas no domínio do tempo que se empregue um modelo de Elementos Finitos de placa ou viga e, assim, obter as tensões nos locais críticos de interesse. Porém, análises no domínio do tempo capturam tensões e deformações com boa precisão, mas costumam ser caras computacionalmente. Na maioria dos casos estudados, a vida em fadiga é fundamental para prever falhas estruturais de elevadas proporções, como o colapso da viga principal da estrutura chassi de um implemento rodoviário. Diante disso, são de interesse tecnológico e industrial as análises no domínio da frequência, a fim de diminuir o custo computacional de simulação dinâmica independente do modelo de Elementos Finitos. Com esse propósito, o presente trabalho propõe uma comparação entre metodologias capazes em estimar a vida em fadiga no domínio do tempo e da frequência, de um caso simples e um segundo caso, mais complexo, que é o da indústria. Os diferentes modelos de Elementos Finitos e métodos de cálculos da vida em fadiga no domínio da frequência são comparados e discutidos, usando-se como referência o método clássico de cálculo da vida em fadiga, domínio do tempo. A metodologia leva em conta os diferentes Elementos Finitos empregados, as simplificações dos modelos estruturais usados e potenciais restrições cinemáticas aplicadas ao modelo. A comparação é feita com a ajuda de ferramentas comerciais que executam as análises modais, harmônicas, transientes, espectrais e rotinas de cálculos. Assim, o analista pode selecionar malhas com quantidade viável de graus de liberdade tornando possível as simulações dinâmicas e, além disso, prever a vida em fadiga no domínio do tempo para modelos simples e complexos. A partir dos resultados, verificou-se que as análises de estimativa da vida em fadiga no domínio da frequência, para modelos complexos, ainda não apresentam resultados confiáveis e, assim, são sugeridas recomendações. / Currently, the industry demand for the construction of complex structures is a consequence of the fierce competition, mainly between companies from semi-trailers segments. With the support of computational tools, based on the Finite Element Method, it is possible to size these structures submitted to random requests varying in time. In this case, it is common to perform dynamic simulations in the time domain to use a Finite Element model of plate or beam and thus obtain the stresses at the critical sites of interest. However, time domain analyses capture tensions and deformations with good accuracy, but they are often computationally expensive. In most of the studied cases, fatigue life is fundamental to predict structural failures of high proportions, such as main beam collapse of the chassis structure of a semi-trailer. Therefore, the semi-trailer industry segments is interested in the frequency domain, in order to reduce the computational cost of dynamic simulation no matter of the Finite Element model. With this purpose, the present work proposes a comparison between methodologies which are able to estimate the fatigue life in time domain and frequency, of a simple and second case, more complex, that of the industry. The different Finite Element models and methods of calculating fatigue life in frequency domain are compared and discussed using the classic time domain fatigue life calculation method as reference. The methodology takes into account the different Finite Elements are used, the simplifications of the structural models used and potential kinematic constraints applied to the model. The comparison is made with not only the following analyses: modal, harmonic, transient, spectral, but also computational routines. Thus, the analyst can select meshes with a viable amount of degrees of freedom making dynamic simulations possible, in addition, to its predict the fatigue life in time domain for simple and complex models. Based on the results, it was verified that the fatigue life estimates in frequency domain, for complex models, do not present reliable results yet. Therefore, recommendations are suggested.

Atualmente, a exigência da indústria na construção de estruturas complexas é consequência da acirrada concorrência, principalmente, entre empresas dos segmentos rodoviários. Com o auxílio de ferramentas computacionais, baseadas no Método de Elementos Finitos, é possível dimensionar essas estruturas submetidas a solicitações aleatórias variando no tempo. Nesse caso, é comum a realização de simulações dinâmicas no domínio do tempo que se empregue um modelo de Elementos Finitos de placa ou viga e, assim, obter as tensões nos locais críticos de interesse. Porém, análises no domínio do tempo capturam tensões e deformações com boa precisão, mas costumam ser caras computacionalmente. Na maioria dos casos estudados, a vida em fadiga é fundamental para prever falhas estruturais de elevadas proporções, como o colapso da viga principal da estrutura chassi de um implemento rodoviário. Diante disso, são de interesse tecnológico e industrial as análises no domínio da frequência, a fim de diminuir o custo computacional de simulação dinâmica independente do modelo de Elementos Finitos. Com esse propósito, o presente trabalho propõe uma comparação entre metodologias capazes em estimar a vida em fadiga no domínio do tempo e da frequência, de um caso simples e um segundo caso, mais complexo, que é o da indústria. Os diferentes modelos de Elementos Finitos e métodos de cálculos da vida em fadiga no domínio da frequência são comparados e discutidos, usando-se como referência o método clássico de cálculo da vida em fadiga, domínio do tempo. A metodologia leva em conta os diferentes Elementos Finitos empregados, as simplificações dos modelos estruturais usados e potenciais restrições cinemáticas aplicadas ao modelo. A comparação é feita com a ajuda de ferramentas comerciais que executam as análises modais, harmônicas, transientes, espectrais e rotinas de cálculos. Assim, o analista pode selecionar malhas com quantidade viável de graus de liberdade tornando possível as simulações dinâmicas e, além disso, prever a vida em fadiga no domínio do tempo para modelos simples e complexos. A partir dos resultados, verificou-se que as análises de estimativa da vida em fadiga no domínio da frequência, para modelos complexos, ainda não apresentam resultados confiáveis e, assim, são sugeridas recomendações. / Currently, the industry demand for the construction of complex structures is a consequence of the fierce competition, mainly between companies from semi-trailers segments. With the support of computational tools, based on the Finite Element Method, it is possible to size these structures submitted to random requests varying in time. In this case, it is common to perform dynamic simulations in the time domain to use a Finite Element model of plate or beam and thus obtain the stresses at the critical sites of interest. However, time domain analyses capture tensions and deformations with good accuracy, but they are often computationally expensive. In most of the studied cases, fatigue life is fundamental to predict structural failures of high proportions, such as main beam collapse of the chassis structure of a semi-trailer. Therefore, the semi-trailer industry segments is interested in the frequency domain, in order to reduce the computational cost of dynamic simulation no matter of the Finite Element model. With this purpose, the present work proposes a comparison between methodologies which are able to estimate the fatigue life in time domain and frequency, of a simple and second case, more complex, that of the industry. The different Finite Element models and methods of calculating fatigue life in frequency domain are compared and discussed using the classic time domain fatigue life calculation method as reference. The methodology takes into account the different Finite Elements are used, the simplifications of the structural models used and potential kinematic constraints applied to the model. The comparison is made with not only the following analyses: modal, harmonic, transient, spectral, but also computational routines. Thus, the analyst can select meshes with a viable amount of degrees of freedom making dynamic simulations possible, in addition, to its predict the fatigue life in time domain for simple and complex models. Based on the results, it was verified that the fatigue life estimates in frequency domain, for complex models, do not present reliable results yet. Therefore, recommendations are suggested.

O aumento da vida em fadiga em peças submetidas a esforços cíclicos devido à aplicação de processos de tratamento mecânico superficial já é bastante conhecido, tanto no meio industrial quanto no meio acadêmico. Para molas, o processo de shot-peening se torna etapa essencial no processo de fabricação, porém um estudo sistemático do efeito do shot-peening na vida em fadiga se faz necessário. O objetivo deste trabalho é aprofundar o conhecimento nos processos de jateamento superficial do tipo shot-peening para molas em lâminas de veículos, através da análise de tensões residuais por difração de raios-x e ensaios de fadiga em uma série de amostras que sofreram dez diferentes receitas de processos de jateamento. Dos dez diferentes processos, o de jateamento com granalha esférica fundida de aço com 1,0mm de diâmetro seguido de um segundo jateamento com granalha esférica fundida de aço de 0,3mm de diâmetro levou a uma maior vida em fadiga das amostras. A análise por difração de raios-x comprovou que a importância das tensões residuais de compressão se dá até a uma profundidade de 0,05mm, influenciando diretamente no modo de nucleação de trincas de fadiga. Acima desta profundidade, as tensões residuais induzidas por shot-peening não têm influência no modo de propagação destas trincas, e por consequência na vida em fadiga das peças. Correlações entre os resultados e a alta dureza e diminuída ductilidade do material utilizado são discutidas. / The improvement of fatigue life in parts subjected to cyclic stresses by application of mechanical surface treatment processes is already well known, both in the industry and in the academy. Dealing with automotive springs, the shot peening process becomes an essential step in manufacturing these parts. In the case of leaf springs, however, a systematic investigation of the effect of shot peening on fatigue life is still required. The aim of this work is to improve the knowledge of shot peening on leaf springs for vehicles, through the analysis of residual stresses by x-ray diffraction and fatigue tests on a series of samples that were subjected to ten different peening schedules. Among the investigated processes, the usage of 1.0 mm diameter cast steel shot followed by a second peening with 0.3 mm diameter cast steel shot leads to better performance, regarding fatigue life. X-ray diffraction analysis shows that this improved performance may be attributed to residual compressive stress maintained until a depth of 0.05 mm below the surface, which directly influences the fatigue crack nucleation. Residual stresses induced by shot-peening in larger depths, have no influence on sample fatigue life, showing that crack propagation is not affected by the induced residual stresses. Consequently, the durability of parts is improved by shot-peening exclusively due to this influence on crack nucleation at samples surface. Correlations with the increased hardness and decreased ductility of the employed material are discussed.

Standard crystalline silicon photovoltaic (PV) modules are designed to continuously convert solar energy into electricity for 25 years. However, the continual generation of electricity by the PV modules throughout their designed service life has been a concern. The key challenge has been the untimely fatigue failure of solder interconnections of solar cells in the modules due to accelerated thermo-mechanical degradation. The goal of this research is to provide adequate information for proper design of solar cell solder joint against fatigue failure through the study of cyclic thermo-mechanical stresses and strains in the joint. This is carried-out through finite element analysis (FEA) using ANSYS software to develop the solar cell assembly geometric models followed by simulations. Appropriate material constitutive model for solder alloy is employed to predict number of cycles to failure of solder joint, hence predicting its fatigue life. The results obtained from this study indicate that intermetallic compound thickness (TIMC); solder joint thickness (TSJ) and width (WSJ) have significant impacts on fatigue life of solder joint. The impacts of TIMC and TSJ are such that as the thicknesses increases solder joint fatigue life decreases. Conversely, as solder joint width (WSJ) increases, fatigue life increases. Furthermore, optimization of the joint is carried-out towards thermo-mechanical reliability improvement. Analysis of results shows the design with optimal parameter setting to be: TIMC -2.5μm, TSJ -20μm and WSJ -1000μm. In addition, the optimized model has 16,264 cycles to failure which is 18.82% more than the expected 13,688 cycles to failure of a PV module designed to last for 25 years.

Articulated haulers are fundamental equipment to transport material. The load carrying structure on a hauler consists mainly of welded frames. During welding of the frames high residual stress will be introduced. These stresses may have a significant impact on the fatigue life of the frames. This is the reason for having good knowledge of the weld residual stresses. The finite element method was used to calculate the residual stress distributions in a butt weld and a T-join weld. Simulation of the welding process with thermal and mechanical analysis was prepared by means of welding GUI implemented in LS-PrePost. The welding simulation is a computer intensive operation with high CPU time. That is why it is important to investigate which process factors that have the largest impact on welding simulation results. The aim of this thesis is to investigate the correlation between designed models in FEA software with published results of weld residual stress measurements and conclude which parameters should be mainly taken into consideration.

This diploma thesis deals with frame of the two-point crank press LKDS800, which was designed by company ŽĎAS a.s. Frame is welded construction creating the base of the press which has mass approximately 90 tonnes. Aim of this study was to perform strain-stress analysis of the frame. From obtained results perform optimization of mass this frame leading to reduce material costs and machining. In the process is frame loaded by nominal forces from the shearing process, under its own weight and inertia forces caused by moving components. As a result of the dynamic loading in welded joints there are risks of fatigue fracture. The manufacturer of the press is required to find the most loaded welded joint and it to assess the fatigue life.

This thesis describes proposal of a methodology for evaluating fatigue life of riveted joints. The first section summarizes the theory used to evaluate fatigue life, description of the structure of operation load spectra and construction principles for the design joints for optimum durability. The second part of the thesis focuses on the proposal of a methodology enabling analytical solutions in closed form suitable for the initial structural design and also numerical solutions for use in detailed analyzes of the structure. The applicability of the methodology is demonstrated on an example of analysis of a real structural detail and subsequent comparison of the analysis with available test results.

Hlavním cílem této práce bylo vysvětlit únavové chování ocelí ODS Eurofer, 14Cr ODS feritické oceli vyráběné v CEA (Commissariat a l’énergie atomique, Saclay, France) a 14Cr ODS feritické oceli vyráběné v EPFL (École Polytechnique Fédérale de Laussane, Switzerland). Pokud to bylo možné byly získané výsledky porovnány s ocelí Eurofer 97. Tato práce je součástí široké spolupráce, která je zaměřena na vývoj konstrukčních materiálů pro fuzní reaktory. V průběhu práce byly provedeny následující experimenty: • Standardní únavové zkoušky za pokojové teploty, při 650 a při 750 , byly získány křivky cyklického zpevnění/změkčení, cyklické deformační křivky, Coffinovy–Mansonovy a Wöhlerovi křivky. Hysterezní smyčky byly detailně analyzovány. • Pozorování mikrostruktury výchozího stavu pomocí TEM a porovnání s mikrostrukturou po cyklickém zatížení. • Pozorování povrchového reliéfu, který vznik díky lokalizaci cyklické plastické deformace - byla odhalena místa iniciace únavových trhlin a byl analyzován mechanismus jejich vzniku. • Měření kinetiky únavových trhlin. Oxidická disperse značně zpevňuje materiály, redukuje cyklické změkčení a stabilizuje mikrostrukturu v celém rozsahu teplot. Byly nalezeny velké rozdíly v životnosti jednotlivých ocelí. Ty byly vysvětleny pomocí rozdílných mechanismů iniciace trhlin a jejich různou rychlostí.