Les travaux de la thèse visent à mettre en place une méthodologie innovante de caractérisation du comportement viscoplastique des matériaux métalliques sous chargement purement inertiel. Sous chargements mécaniques extrêmes (e.g., crash, impact ou explosions), leur comportement mécanique présente en effet pour nombre d’entre eux une sensibilité à la vitesse de déformation. Des approches dites statiquement déterminées sont majoritairement utilisées pour caractériser leur comportement, mais elles requièrent de nombreux essais dont les conditions expérimentales sont souvent contraintes comme par exemple l’homogénéité de la vitesse de déformation qui doit être maintenue constante en temps par exemple. En revanche, des approches dites statiquement indéterminées permettent l’exploitation d’essais mécaniques avec peu d’hypothèses (voire sans) sur les conditions d’essai. Une méthodologie fondée sur un essai d’impact purement intertiel est mise en oeuvre ici pour identifier le comportement viscoplastique de ces matériaux. Avec la Méthode des Champs Virtuels, la méthodologie permet l’identification des paramètres matériaux en exploitant uniquement la mesure des champs de déformation et d’accélération, potentiellement hétérogènes en temps et en espace. Ainsi, celui-ci peut être caractérisé sur une large gamme de déformations et de vitesses de déformation plastiques en procédant à un nombre limité d’expériences. La méthode repose sur le développement d’un simulateur d’images avancé permettant de définir au préalable l’ensemble du dispositif expérimental (géométrie de l’éprouvette et conditions expérimentales). Optimisées numériquement pour prescrire les paramètres d’essai critiques, les réalisations expérimentales menées sur un alliage de Titane utilisé dans l’industrie aéronautique ont permis d’identifier les paramètres d’un modèle de Johnson-Cook sur un spectre de déformations et de vitesses de déformation plastiques pré-déterminé. Les incertitudes de la mesure sont également intégrées et analysées dans ce travail. / This thesis aims at developing an innovative methodology for viscoplastic material behaviour characterization of metallic materials under purely inertial loads. Indeed, their mechanical behaviour under extreme conditions (e.g., crash, impact or explosions) is often rate-dependant. Statically determinate approaches are mainly used to characterize their behaviour. However, they require numerous tests for which testing conditions are strongly constrained, such as the strain rate which has to remain constant in time and space for instance. By contrast, statically undeterminate approaches enable test processing with a few (or without) hypotheses on experimental conditions. In this work, the Image-Based Inertial Impact test methodology has been extended to characterize the viscoplastic behaviour of metallic materials. Owing to the Virtual Fields Method, it enables the identification of constitutive material parameters with the sole knowledge of strain and acceleration fields (possibly heterogeneous in time and space). Therefore, constitutive models can be characterized over a wide range of plastic strain and strain rate, while the number of tests is limited. Tests design notably relies on the development of a synthetic images generator to determine the experimental setup (e.g., specimen geometry or testing conditions). Finally, experiments are carried out with optimized test configurations to identify Johnson-Cook parameters over a predicted range of plastic strain and strain rate for a titanium alloy widely used in aerospace industry. Identification uncertainties are also quantified and analysed in this work.

O Jateamento com granalha (shot peening, em inglês) é um processo de fabricação amplamente utilizado em indústrias mecânicas, automotivas, navais, aeronáuticas e outras indústrias metalúrgicas. O objetivo principal é induzir tensões residuais de compressão para melhorar a vida à fadiga das peças e estruturas. A modelagem e simulação do processo são muito difíceis, pois envolvem a consideração de muitos e complexos aspectos. Este trabalho propõe um método de modelagem tridimensional utilizando o método dos elementos finitos para a simulação numérica desse processo assim como a sua influência na propagação de trinca, considerando efeitos pouco estudados, como o amolecimento do material devido ao aumento da temperatura na peça durante os impactos, ao comportamento elasto-plástico das granalhas e a rugosidade da peça tratada nos parâmetros da trinca. A modelagem proposta para simular o processo de jateamento com granalhas inclui: (i) análise dinâmica explícita, (ii) modelagem tridimensional, (iii) cálculo da velocidade real das granalhas, (iv) modelo de contato com coeficientes de atrito estático e dinâmico entre as áreas em contato, (v) o modelo constitutivo de Johnson-Cook para o comportamento do material alvo, (vi) um comportamento elasto-plástico multilinear para as granalhas, (vii) a consideração da cobertura real de uma área dada da superfície jateada, (viii) a consideração do aumento da temperatura no material durante o processo e (ix) o relaxamento de tensões residuais devido a este aumento de temperatura. As simulações numérico-computacionais para investigar a influência do processo em fenômenos, tais como fadiga e propagação de trinca, necessitou uma nova abordagem para a incorporação das tensões residuais num modelo de elementos finitos. Além disso, foram realizados vários ensaios quase-estáticos e dinâmicos para a determinação dos parâmetros do modelo constitutivo de Johnson-Cook para o aço AISI 5160. Para a avaliação das metodologias propostas, as tensões residuais foram introduzidas e avaliadas em uma mola parabólica automotiva, sendo que as tensões residuais foram avaliadas através da técnica de difração de raios-X, a intensidade e a cobertura do processo de jateamento com granalha na mola foram avaliadas com Lupa e rugosímetro. Também, dados experimentais de ensaios de fadiga relatados na literatura, realizados em corpos de prova tipo CT foram utilizados. A modelagem numérica do processo de jateamento com granalha desenvolvida neste trabalho consegue prever com sucesso os perfis das tensões residuais, com valores bem próximos aos obtidos experimentalmente. A investigação numérica do efeito do processo na vida à fadiga e fratura das peças comprovou a sua influência nos parâmetros de propagação de trinca nas regiões afetadas pelo processo, ocasionando um amplo aumento da vida à fadiga, e confirmou o relaxamento das tensões residuais devido aos ciclos de carregamento conforme as observações experimentais na literatura. / Shot peening is a manufacturing process widely used in the mechanical, automotive, marine, aeronautical and other metallurgical industries. The main purpose is to induce residual compression stresses to improve fatigue life. The modeling and simulation of the process are very difficult as they involve the consideration of many and complex aspects. This work proposes a three-dimensional modelling method using the finite element method for the numerical simulation of this process as well as its influence on crack propagation, considering little studied effects such as softening of the material due to the increase in temperature in the part during impacts , the elastic-plastic behavior of the shot and the roughness of the treated part in the crack parameters. The proposed modelling approach to simulate the shot peening process includes: (i) explicit dynamic analysis, (ii) three-dimensional modeling, (iii) calculation of the real velocity of the shot, (iv) contact model with static and dynamic friction coefficients between the contact areas, (v) the Johnson-Cook constitutive model for target material behavior, (vi) a multilinear elasto-plastic behavior for the shot, (vii) consideration of real coverage in a given area of the peened surface, (viii) consideration of temperature increase in the material during the process and (ix) relaxation of residual stresses due to this rise in temperature. Numerical-computational simulations to investigate the influence of the shot peening process on phenomena, such as fatigue and crack propagation, required a new approach for the incorporation of residual stress in a finite element model. In addition, several quasi-static and dynamic tests were carried out to determine the parameters of the constitutive Johnson-Cook model for AISI 5160 steel. To assess the proposed methodologies, the residual stresses were introduced and evaluated in an automotive parabolic spring, with the residual stresses being evaluated by the X-ray diffraction technique, the intensity and coverage of the shot peening process for the spring were evaluated with magnifying glass and roughness gauge. Also, fatigue tests available in the literature, carried out on types of CT specimens, were used. The numerical modeling of the shot peening process developed in this work can successfully predict the residual stress profiles, with values close to those obtained experimentally. The numerical investigation of the effect of the process in the fatigue life and fracture of the pieces proved its influence in the parameters of crack propagation in the regions affected by the process, causing a wide increase of the fatigue life, and confirmed the relaxation of the residual stresses due to the cycles loading according to experimental observations in the literature.

The PhD thesis deals with the influence of temperature and strain rate on the mechanical behaviour of the Ti-6Al-4V titanium alloy. After verification tests under static loading conditions, the samples were deformed at high strain rates and elevated temperatures, using device for Hopkinson pressure bar test. The result is dependence of stress and strain rate on strain in the temperature range of 20 to 500°C. The deformed shape of specimen from the Taylor anvil test is compared with the results of the simulation in the Ansys – LS Dyna software. The parameters of Johnson-Cook equation were determined from these experiments. Also, the influence of loading conditions on the microstructure was studied. Both optical and scanning electron microscopes were used for the observations. During the research, some adjustments to the experimental devices were made in order to suppress the high-frequency components and noise in the recorded pulses. A functional tensile test adapter for the Hopkinson test was developed; it is registered under No. 2007/008 at the Technology Transfer Office of BUT.