This thesis refers to a simulation of an adhesive joint used to bond two metal sheets of a component of the side skirt bracket implemented in trucks. The adhesive joint must support fatigue and mixed-mode loading. The principal goal is the implementation of a novel material model, which governs the damage produced by a mixed-mode fatigue loading in a rubber adhesive layer. Two approaches to define the material model are implemented: the filament model and the principal strain model. The models are fitted against experiments, which have been performed parallel to the development of this thesis by the Mechanics of Materials (MoM) research group of the University of Skövde. The models incorporate fitting parameters with the aim of adjusting the models against experimental results. Simulations are performed using the Finite Element (FE) software, ABAQUS, and the material models are implemented using UMAT subroutines. The filament model is inaccurate and it is considered unable to model the mixed-mode behaviour of the adhesive joint. The principal strain model is considered a well-established method to define the damage and to predict the fatigue life of the adhesive under fatigue in mixed-mode loading.

This thesis deals with some aspects of crack growth in the presence of cyclic loading, i.e. fatigue. The cyclic load cases studied here are primary of non-proportional mixed mode type. Under non-proportional loading the principal stress directions rotate and, generally, the ratio between the principal stresses vary. A new criterion has been presented for prediction of incipient crack path direction after changes in load from steady Mode I to non-proportional loading. The criterion is based on FE-simulations which are used to compute the actual elasto-plastic stress state in the vicinity of the crack tip. The predictions of the criterion capture several phenomena observed in the literature, which indicates that plasticity effects have to be included in a criterion for crack path predictions under non-proportional loading. The effects of Mode II overloads on subsequent Mode I crack growth have been studied relatively little in the literature. Also, the results deviates substantially. In the present thesis, this load case has been investigated in detail, both experimentally and analytically. The results show that the Mode I crack growth rate decreases after a single Mode II load, if the R-ratio is not as high as to keep the entire Mode I load cycle above the closure level. This is based on the fact, shown in this thesis, that the reduction is caused by crack closure due to tangential displacement of crack-surface irregularities. A new loading device is presented. With this device, it is possible to apply sequential loading in Mode I and Mode II in an automated way, without having to dismount the specimens. This loading device is used to study the influence of periodic Mode II loading on Mode I crack growth. The main parameters concerning the influence of periodic Mode II loading on Mode I crack growth are; (i) the Mode I R-ratio, (ii) the Mode II magnitude and (iii) the Mode II periodicity, M (number of Mode I loads for every Mode II load). The mechanisms involved are mainly RICC (Roughness-Induced Crack Closure) and a Mode II mechanism that increases the growth rate temporary at every Mode II load. Hence, the latter becomes more significant for low M-values. The higher the Mode I R-ratio the smaller is the reduction. / QC 20101004

Les avalanches de plaque représentent un risque naturel majeur dont la prévision demeure très difficile. Le manque de lois constitutives fiables à l’échelle du matériau rend difficiles les tentatives de modélisation de ce phénomène. Plus spécifiquement, la réponse mécanique de la neige durant et après la rupture, dans des régimes de chargements rapides , demeure relativement méconnue. La nature particulièrement fragile du matériau au sein de ce régime de déformation rend ardue la réalisation d’expériences et complique l’observation à l’échelle microstructurale.Dans ce travail de thèse, un modèle numérique de neige fondé sur la Méthode des Éléments Discrets a été développé en tant qu’alternative aux expériences. Le modèle nous permet de simuler la réponse de la neige à des chargements mécaniques en tenant compte de la microstructure réelle du matériau grâce à l’intégration d’images acquises par microtomographie à rayons X en entrée du modèle. La neige est considérée comme un matériau granulaire cohesif, et une méthode originale a été développée afin de modéliser la forme de chaque grain. Les grains individuels sont ensuite assemblés pour reconstituer la matrice de la neige grâce à la prise en compte de lois de contact cohésives.Le modèle a été utilisé afin d’explorer la réponse mécanique macroscopique de différent échantillons de neige à un chargement mixte normal-cisaillant. Trois modes de rupture ont été observés dans tous les échantillons de neige testés, en fonction du niveau de contrainte normale appliquée : une rupture en cisaillement localisée pour des niveaux de contrainte normale faibles (mode A), un effondrement normal induit par rupture en cisaillement à des niveaux intermédiaires de contrainte normale (mode B) et un effondrement normal pour des valeurs de contrainte normale élevées (mode C). Ces différents modes de rupture produisent une enveloppe de rupture fermée dans l’espace des contraintes, ce pour les différents types de neige étudiés.Les mécanismes internes conduisant à l’effondrement normal des échantillons ont été étudiés plus en détail à l’échelle microscopique. Il a été montré que ce mode de rupture était associé à un mécanisme de flambement des chaînes de force. En outre, la stabilité de ces chaînes de force semble être contrôlée par les contacts entre les éléments des chaînes et les grains environnants. La rupture de ces contacts, observée dans les modes B et C, autorise le développement du flambement des chaînes de force et aboutit à l’effondrement volumique. / Dry slab snow avalanches represent a major natural hazard that is extremely difficult to manage. Attempts to model this phenomenon are hindered by the lack of a constitutive law that would describe the mechanical behaviour of snow on a material scale. In particular, relatively little is known on the failure and post-failure response of snow at high loading-rates. The highly fragile nature of the material in this deformation regimerenders experimental investigation difficult and complicates observation at the microstructural level.As an alternative to experiments, a Discrete Element Method-based numerical model of snow is developed in this thesis. The model enables us to simulate the response of snow to mechanical loading, while accounting for actual snow microstructure by using X-ray attenuation images of snow microstructure as input. Snow is considered as a cohesive granular material and an original methodology is developed in order to model the shape of each grain. Individual grains are bound into the snow matrix by modelling cohesion between neighbouring grains.The model is then used to explore the macroscopic mechanical response of different snow samples to mixed-mode loading. Three typical modes of failure are observed in all tested snow samples, depending on the level of applied normal stress: a localized shear failure at low normal stress (mode A), a shear failure-induced volumetric collapse at intermediate levels of normal stress (mode B), and a normal failure and collapse for high values of normal stress (mode C). The observed failure modes result in closed failure envelopes and no qualitative difference is observed between the mechanical responses of different snow types.The internal mechanisms that lead to volumetric collapse are further examined on the microscale. Force chain buckling is identified as a trigger of this material instability. Additionally, force chain stability appears to be controlled by the contacts between the force chain members and the surrounding grains. The failure in these contacts, which is evidenced in modes B and C, allows force chain buckling to develop and results in subsequent volumetric collapse.

科学研究費補助金 研究種目:基盤研究(B)(2) 課題番号:07455052 研究代表者:田中 啓介 研究期間:1995-1996年度