Afin d'augmenter leur productivité, certains industriels de la découpe mécanique s'intéressent à un procédé émergeant : le cisaillage grande vitesse. Pour ce procédé, la vitesse du poinçon atteint 10m/s alors que cette vitesse ne dépasse pas 0,1 m/s pour le cisaillage conventionnel. Cependant, même si la qualité des découpes obtenues se rapproche celle du cisaillage fin, l'apparition de phénomènes dynamiques mal compris rend aujourd'hui délicat le déploiement du cisaillage grande vitesse. Dans ce travail de thèse nous proposons d'aller vers une meilleure maîtrise de ce procédé en utilisant aussi bien des moyens expérimentaux que numériques. Ainsi un dispositif expérimental instrumenté a été mis au point afin d'observer finement les phénomènes présents lors de la découpe. Ce dispositif conserve des similitudes avec les moyens industriels et comprend notamment un poinçon dont la section varie et une matrice solidaire d'un tube de Hopkinson pour la mesure des efforts de cisaillage. Cette mesure a comprend un traitement spécifique afin de corriger des effets dynamiques présents dans la matrice. Ce traitement, qui nécessite une calibration du banc, a été validé grâce à une modélisation numérique unidimensionnelle. Des observations du faciès de rupture ont permis de mettre en évidence la présence de bandes de cisaillement adiabatiques, signature d'une augmentation localisée importante de la température. Par ailleurs, une modélisation thermomécanique du comportement de l'acier C40 (loi de Johnson-Cook) a été réalisée et utilisée dans un code de simulation utilisant une approche C-NEM (Constrained Natural Element Method) pour reproduire les cisaillages observés sur le banc. Une étude comparative simulation/expérimentation a ainsi pu être effectuée.

Dans cette thèse, nous avons étudié, dans une première partie, l'effet d'onde de choc dans les matériaux cellulaires (mousses, nids d'abeilles et sphères creuses). Une nouvelle technique expérimentale originale avec les barres de Hopkinson pour étudier l'effet d'onde de choc dans de tels matériaux complètée par une mesure locale et par la modélisation éléments de tels effets sont présentées. Dans la seconde partie, nous avons mis en place une nouvelle technique de la mesure de la perforation dynamique en utilisant aussi la technique de la mesure avec les barres de Hopkinson : la perforation inversée. Cette technique permet de rendre possible de comparer directement l'histoire de force vs déplacement dynamique avec la quasi statique.

Ce rapport est une synthèse du travail d'analyse exploratoire du procédé de mise en forme des produits en bétons de type bloc. Celui ci consiste à mouler le bloc par compression assistée de vibrations. Un essai d'analyse de la compactibilité du béton frais est mis au point. Le compactage du matériau est réalisé sous l'action d'impacts répétés d'une masse tombante. Cet essai Proctor est instrumenté via la technique de mesure dynamique aux barres de Hopkinson. L'efficacité du compactage sous impacts est quantifiée. La mesure de contrainte durant le premier impact nous permet de détecter un changement de rhéologie et de l'analyser. Un essai complémentaire est conçu. Il consiste à compacter le matériau sous compression et vibration. Les mécanismes du compactage et l'influence des paramètres sur la densification sont analysés. Par analogie entre la vibration et la température, des essais de caractérisation du comportement viscoplastique du béton frais vibré sont réalisés.

The study consists mainly of two parts. The first part is related to the dynamic strength enhancement of honeycombs under uniaxial compression. We firstly study numerically this particular phenomenon of thin-walled structure by using three micro-size FE models and this allows us to reveal the role played by lateral inertia in the dynamic enhancement. Further more, the dynamic enhancement of a series of honeycombs with different cell-size, cell-wall thickness and base material is studied experimentally and the influence of these geometric parameters and the base material on honeycomb strength as well as the dynamic enhancement rate is investigated. The second part of this study concerns the biaxial behavior of honeycombs under combined shear-compression. We firstly present a combined dynamic shear-compression loading device basing on a large-diameter Nylon Split Hopkinson Pressure Bar system. Then, a series of quasi-static and dynamic experiments on an aluminium honeycomb is performed with loading angles ranging from 0o to 60o (part of shear more and more important). It shows a strong effect of the additional shear loading to honeycomb overall strength. A notable strength enhancement under impact loading is observed for all the honeycomby b specimens. Images captured during tests permit for the determination of the two co-existing deforming patterns under combined shear-compression. Finally, the combined shear-compression tests on honeycombs are reproduced by a numerical virtual model and the separated normal and shear behaviors of honeycombs under combined shear-compression are obtained. A crushing envelope in normal strength vs. shear strength plane was obtained on the basis of these simulations, which shows an isotropic expansion behavior from the quasi-static loading to the dynamic loading.

No description available.

The aim of this thesis is to provide microstructural and mechanical characterisation of α-β titanium alloys exposed to a range of thermo-mechanical conditions, in particular under-going high rate deformation at elevated temperatures, representative of the Linear Friction Welding (LFW) manufacturing process. Three α-β titanium alloys provided by Rolls-Royce are studied: Ti-64 blade, disc and Ti-6246 disc. Ti-64 and Ti-6246 show complex deformation behaviour with strain, strain rate and temperature, especially near the transus temperature, where the low temperature α phase is transformed into the high temperature β phase. The microstructure and mechanical properties evolve in an interconnected fashion, and understanding this mutual influence is necessary to better predict the behaviour of these alloys. Characterisation of the mechanical properties was performed through uniaxial compression tests at strain rates from 0.001 to 3000 s^-1, using an Instron screw-driven machine at quasi-static rates, a servo-hydraulic machine at medium rates and a Split-Hopkinson Pressure Bar and a drop-weight tower at high strain rates. The tests were performed over a range of temperatures from room temperature to 1300 °C. The main focus was on high strain rate and high temperature tests, with the development of a gravity driven direct impact Hopkinson bar, referred as a drop-weight system, which is intended to evaluate the mechanical response of metals to high strain rate loading at temperatures up to c. 1300 °C. The design and principles of operation of the system are presented, along with calibration and validation data. Preliminary tests were performed on stock Ti-64, heated at two rates: 1 and 20 °C s^-1. The evolution of the mechanical properties was analysed, focussing on the strain rate, temperature and phases dependencies. Characterisation of the microstructure was realised by performing interrupted compression tests, first at room temperature, three plastic strains, 4%, 10% and 20%, and two different strain rates, 0.001 and 2000 s^-1; then at 4% plastic strain, a strain rate of 2000 s^-1 and three elevated temperatures, 700, 900 and 1100 °C. A better understanding of the microstructure evolution with strain, strain rates and temperature, including the macrotexture and microtexture of the specimens, was obtained using Electron Backscatter Diffraction (EBSD) to characterise the texture of the undeformed and deformed materials. The better understanding of the flow stress and microstructural evolution of both Ti-64 and its individual α and β phases with various strain rates and temperatures is intended to be used in the development of more accurate models representing the behaviour of these alloys. Predicting the microstructure evolution and then the mechanical properties of a material is essential to optimise the final mechanical properties of the alloys when welded by manufacturing processes such as the LFW process.

Above true strain rates of $10^4$ s$^{-1}$ FCC metals exhibit a rapid increase in strength. Understanding of the physical mechanisms behind this strength transition is hindered by the number and interdependence of candidate mechanisms. Broadly, contributions to strength can be split into `instantaneous' effects and the more permanent `structural' ones. In this thesis a series of experiments are presented which are designed to separate the two types of contribution. Chapter 2 outlines the basics of dislocation plasticity, based on the seminal works of Taylor and Orowan. It then progresses on to discuss recent experimental and theoretical work on the understanding of slip as avalanche behaviour. Chapter 3 summarises traditional modelling approaches for instantaneous strength contributions which are routinely applied below $10^4$ s$^{-1}$. It then continues on to outline a number of different approaches which have been adopted to attempt to explain and model the strength transition. Chapter 4 outlines the methods used in the earliest stages of the study: Instron and split Hopkinson pressure bar methods. Both methods are well established, and cover the majority of the range of rates under study. Emphasis is made on minimising experimental sources of error, and subsequently accounting for those which are unavoidable. Finally, the specimen material is introduced and is shown to be fit for purpose. Chapter 5 presents a set of mechanical tests of specimens at strain rates between $10^4-10^5$~s$^{-1}$. The softening of the specimens with increased temperature is observed to increase with strain rate, both in absolute terms and when normalised to the 300 K measurement for each strain rate. The observations are most easily explained if the strength transition is due to an increase in early stage work hardening, however, some anomalous behaviours remain. Chapter 6 introduces a new experimental technique; direct impact Hopkinson pressure bars, required to perform experiments shown to be necessary by the results of Chapter 5. Photon Doppler velocimetry is applied to the projectiles used in experiments, removing one of the most significant flaws of the technique, and creating a more confident basis with which to perform further experimental work. Chapter 7 presents a series of `jump tests' at ambient temperatures. Specimens are deformed at strain rates ranging from $10^{-2}$ to $10^5$~s$^{-1}$ to a fixed strain of 0.1, then reloaded to yield at a strain rate of $10^{-1}$. The yield point at reload is shown to have the same rapid upturn as seen when the specimens were deforming at high rates, providing strong evidence that the increase in strength is due to changes in the underlying dislocation structure, rather than a dynamic effect, as it remains even when the high strain rate is removed. Chapter 8 continues on from the conclusions of Chapter 7. Jump tests are expanded to a variety of temperatures and strains, to provide a more complete characterisation of metal behaviour. No dramatic change in the saturation of work hardening is observed to coincide with the increase in early stage work hardening. Chapter 9 discusses discrepancies between contemporary high rate models and recent developments in the understanding of plasticity being an avalanche process. Potential consequences of incorporating avalanche plasticity into high rate models are explored. Particular attention is paid to Brown's observation that based on quasi static observations of avalanche behaviour, the formation of dislocation avalanches will begin to fail at strain rates of approximately $10^4$ s$^{-1}$. Consequences of the progressive breakdown of avalanche behaviour are discussed with respect to the experimental observations presented in earlier chapters. In Chapter 10, we will discuss the key conclusions of the work. Finally, a number of avenues are proposed for building upon the current work both theoretically and experimentally.

As defensas rodoviárias têm a finalidade de redirecionar com segurança um veículo fora de controle de uma colisão frontal ou trajetória mais perigosa. Secundariamente, a absorção de energia através da deformação do sistema de contenção ou outro método de dissipação da energia de impacto é ressaltado como um benefício em prol da segurança dos ocupantes. Considerando as premissas anteriores e os índices de severidade ao ocupante ASI, THIV e PHD, os desempenhos de uma defensa metálica e outras defensas de concreto são então classificados. Além disso, investiga-se o mecanismo de falha das conexões parafusadas e a sua influência no resultado do impacto de um automóvel leve contra uma defensa metálica. Importância é dada à modelagem do comportamento do material da defensa metálica sob baixas e altas taxas de deformação. Dessa forma, a necessidade de avaliar as propriedades dinâmicas do material motivou o projeto e construção de uma Barra de Hopkinson para testes de tração e compressão até 5000s-1. Adicionalmente, um modelo analítico simplificado da defensa metálica sob ação de uma força estática foi equacionado para validar um modelo em elementos finitos. Um estudo paramétrico da falha da conexão parafusada foi levantado através de diversas simulações estáticas e também do impacto de um veículo leve em uma defensa metálica de acordo com a norma EN 1317. Os resultados das simulações de impacto utilizando um modelo de veículo leve e diferentes sistemas de contenção foram comparados em função dos índices de severidade ao ocupante, indicando que a defensa metálica é mais segura do que uma defensa de concreto com perfil New Jersey ou vertical. / The main function of a road guardrail is to redirect an out of control vehicle avoiding a frontal collision or a dangerous veering off the road trajectory. Secondarily, the energy absorption measured by barrier deformation or any other energy dissipation method is beneficial to the car occupant safety. Considering the previous tasks and some severity occupant index like ASI, THIV and PHD, the performance of a guardrail and other concrete barriers are classified. Besides, it is investigated the fail mechanism of bolted connections and its influence on the guardrail impact result of an automobile. Special attention was taken into the material behavior modeling under low and high strain rates. Thereby, the need of accessing dynamic material properties motivated the design and manufacture of a Hopkinson Bar set-up for tension and compression tests up to 5000s-1. In addition, a simplified analytical model of a guardrail subjected to a static force was settled in order to validate a guardrail finite element model. A parametric study of the bolted connection failure was performed through several impact simulations of a light car model and a guardrail according to EN 1317 standard. The impact simulation results using a light vehicle car model and different barriers types were compared through the occupant severity index showing that the guardrail is a safer system than concrete barrier with New Jersey or vertical profile.

This master’s thesis deals with the problem of measurement for thermomechanical parameters during metal forming under higher deformation rate. The first part works up general literary studies, comprising a summary of measurement methods for required parameters. There is described a principle of their function and usage. Further assessed the current situation and recommendation of appropriate methods for the dynamic processes of forming, especially their testing. The second part is devoted to the measurement for dynamic features of the material. This is a problem specified by Split Hopkinson preassure bar test. The test is described, including the mathematical evaluation process, in the theoretical part. In the practical part, there is a detailed description of the process and evaluation of the real test with aluminum alloy AlMg4, 5Mn ,07-EN AW 5083 performed within the framework of the junior project.

Blades used on brushcutters and lawn mowers are subjected to a wide variety of working conditions. Besides continuous loads from cutting grass, the blades are also subjected to accidental impacts of branches, stones and structures. Due to exceptionally high rotational velocities, these types of impacts involve blade deformation at high strain rates. This master’s thesis aims to improve understanding and predictability of blade properties for design of future blades. The project is aimed at characterization of the mechanical response of steel used for brushcutter blades and developing a simulation model of a blade impact load case. Thus, the problem was divided into two main parts: firstly, material characterization, and secondly, numerical modeling. The objective of the material characterization part was to determine the rate dependence of the flow stress for two hardened steels. Experimental compression tests were performed at quasi-static strain rates (10-4 - 10-2 s-1) and at high strain rates (102 - 104 s-1) in order to characterize the rate dependence of each material. The objective of the numerical modeling part was to develop simulation models of an impact load case for the purpose of recreating tests performed with an experimental test setup. The simulation models were aimed to include material models for the blade based on the experimental tests performed for the two hardened steels. In preparation for the compression tests, cylindrical specimens were acquired through electrical discharge machining involving material removal from blades intended for brushcutters. Compression tests at high strain rates were performed utilizing a split-Hopkinson pressure bar apparatus which resulted in strain rates in the order of 1000 s-1 and 3000 s-1. Compression tests at quasi-static strain rates were performed with an electro-mechanical loading machine and implementation of two-dimensional digital image correlation for strain measurements. With this method, strain rates in the order of 5 · 10-2 s-1 and 5 · 10-4 s-1 were achieved. The acquired results from the experimental tests included the response of the two materials at four different strain rates in the form of true stress-true strain curves. The results were indicative of small strain rate dependency for each of the two hardened steels with a slight increase in yield stress for increasing strain rates. Both materials exhibited closely similar characteristics. At quasi-static rates, the response of both materials exhibited work-hardening of closely similar characteristics. At high strain rates, the response of both materials exhibited a close to identical decrease in stress for values of strain exceeding 10 %. This behavior was suggested to be a consequence of adiabatic heating. At all four achieved strain rates, the results were indicative of a higher yield stress with higher subsequent stresses for one of the hardened steels in comparison to the other. The impact load case aimed to be simulated involved one swing of a brushcutter against a 25 mm diameter steel rod according to standard SS-EN ISO 11806-1:2011. The steel rod was specified to be impacted horizontally by the blade at an approaching translational velocity of 1 m/s and a blade rotational velocity of 8500 rpm. The multi-physics simulation software LS-DYNA was used to develop simulation models which consisted of two main parts, the blade and the rod and included two different blade geometries. As a result of a study regarding the suitability of different discretization techniques, the decision was made to implement the mesh-free particle method Smoothed Particle Galerkin (SPG) and to perform coupling with the finite element method (FEM). Two material models were developed based on the measured stress-strain response obtained through high strain rate compression testing. Several numerical models of the impact load case were produced, all of which entailed different sets of parameters. These included selection of blade material, failure strain, rod length and blade angle relative to the horizontal plane. Finally, two models were developed which were opposite in terms of assigned element formulation for the blade tip and the rod and otherwise identical. The results of the different models were then compared, namely in terms of resulting material failure of the blade after impact. It was concluded that SPG was the most suitable method of choice for the impact load case aimed to be simulated due to its ability to handle large deformation and the inclusion of the a bond-based failure mechanism. Furthermore, implementation of the SPG method resulted in deformation and failure considered to be of greater agreement to experimental test results compared to FEM.