Thesis (M.S. in Mechanical Engineering)--Tufts University, 2000. / Title from PDF title screen. "PB2008-110256." Includes bibliographical references (p. 80-82). Also available online.

Evaluation of the performance of a product and its components under impact loading is one of the key considerations in design. In order to assess resistance to damage or ability to absorb energy through plastic deformation of a structural component, impact testing is often carried out to obtain the 'Force - Displacement' response of the deformed component. In this context, it may be noted that load cells and accelerometers are commonly used as sensors for capturing impact responses. A drop-weight impact testing set-up consisting of a moving impactor head with a lightweight piezoresistive accelerometer and a strain gage based compression load cell mounted on it is used to carry out the impact tests. The basic objective of the present study is to assess the accuracy of responses recorded by the said transducers, when these are mounted on a moving impactor head. In the present work, a novel approach of theoretically evaluating the responses obtained from this drop-weight impact testing set-up for different axially loaded specimen has been executed with the formulation of an equivalent lumped parameter model (LPM) of the test set-up. For the most common configuration of a moving impactor head mounted load cell system in which dynamic load is transferred from the impactor head to the load cell, a quantitative assessment is made of the possible discrepancy that can result in load cell response. Initially, a 3-DOF (degrees-of-freedom) LPM is considered to represent a given impact testing set-up with the test specimen represented with a nonlinear spring. Both the load cell and the accelerometer are represented with linear springs, while the impacting unit comprising an impactor head (hammer) and a main body with the load cell in between are modelled as rigid masses. An experimentally obtained force-displacement response is assumed to be a nearly true behaviour of a specimen. By specifying an impact velocity to the rigid masses as an initial condition, numerical solution of the governing differential equations is obtained using Implicit (Newmark-beta) and Explicit (Central difference) time integration techniques. It can be seen that the model accurately reproduces the input load-displacement behaviour of the nonlinear spring corresponding to the tested component, ensuring the accuracy of these numerical methods. The nonlinear spring representing the test specimen is approximated in a piecewise linear manner and the solution strategy adopted and implemented in the form of a MATLAB script is shown to yield excellent reproduction of the assumed load-displacement behaviour of the test specimen. This prediction also establishes the accuracy of the numerical approach employed in solving the LPM system. However, the spring representing the load cell yields a response that qualitatively matches the assumed input load-displacement response of the test specimen with a lower magnitude of peak load. The accelerometer, it appears, may be capable of predicting more closely the load experienced by a specimen provided an appropriate mass of the impactor system i.e. impacting unit, is chosen as the multiplier for the acceleration response. Error between input and computed (simulated) responses is quantified in terms of root mean square error (RMSE). The present study additionally throws light on the dependence of time step of integration on numerical results. For obtaining consistent results, estimation of critical time step (increment) is crucial in conditionally stable central difference method. The effect of the parameters of the impact testing set-up on the accuracy of the predicted responses has been studied for different combinations of main impactor mass and load cell stiffness. It has been found that the load cell response is oscillatory in nature which points out to the need for suitable filtering for obtaining the necessary smooth variation of axial impact load with respect to time as well as deformation. Accelerometer response also shows undulations which can similarly be observed in the experimental results as well. An appropriate standard SAE-J211 filter which is a low-pass Butterworth filter has been used to remove oscillations from the computed responses. A load cell is quite capable of predicting the nature of transient response of an impacted specimen when it is part of the impacting unit, but it may substantially under-predict the magnitudes of peak loads. All the above mentioned analysis for a 3 DOF model have been performed for thin-walled tubular specimens made of mild steel (hat-section), an aluminium alloy (square cross-section) and a glass fibre-reinforced composite (circular cross-section), thus confirming the generality of the inferences drawn on the computed responses. Further, results obtained using explicit and implicit methodologies are compared for three specimens, to find the effect, if any, on numerical solution procedure on the conclusions drawn. The present study has been further used for investigating the effects of input parameters (i.e. stiffness and mass of the system components, and impact velocity) on the computed results of transducers. Such an investigation can be beneficial in designing an impact testing set-up as well as transducers for recording impact responses. Next, the previous 3 DOF model representing the impact testing set-up has been extended to a 5 DOF model to show that additional refinement of the original 3 DOF model does not substantially alter the inferences drawn based on it. In the end, oscillations observed in computed load cell responses are analysed by computing natural frequencies for the 3 DOF lumped parameter model. To conclude the present study, a 2 DOF LPM of the given impact testing set-up with no load cell has been investigated and the frequency of oscillations in the accelerometer response is seen to increase corresponding to the mounting resonance frequency of the accelerometer. In order to explore the merits of alternative impact testing set-ups, LPMs have been formulated to idealize test configurations in which the load cell is arranged to come into direct contact with the specimen under impact, although the accelerometer is still mounted on the moving impactor head. One such arrangement is to have the load cell mounted stationary on the base under the specimen and another is to mount the load cell on the moving impactor head such that the load cell directly impacts the specimen. It is once again observed that both these models accurately reproduce the input load-displacement behaviour of the nonlinear spring corresponding to the tested component confirming the validity of the model. In contrast to the previous set-up which included a moving load cell not coming into contact with the specimen, the spring representing the load cell in these present cases yields a response that more closely matches the assumed input load-displacement response of a test specimen suggesting that the load cell coming into direct contact with the specimen can result in a more reliable measurement of the actual dynamic response. However, in practice, direct contact of the load cell with the specimen under impact loading is likely to damage the transducer, and hence needs to be mounted on the moving head, resulting in a loss of accuracy, which can be theoretically estimated and corrected by the methodology investigated in this work.

Carbon fabric-reinforced polymer (CFRP) composites are widely used in aerospace, automotive and construction structures thanks to their high specific strength and stiffness. They can also be used in various products in sports industry. Such products can be exposed to different in-service conditions such as large bending deformations caused by quasi-static and dynamic loading. Composite materials subjected to such bending loads can demonstrate various damage modes - matrix cracking, delamination and, ultimately, fabric fracture. Damage evolution in composites affects both their in-service properties and performance that can deteriorate with time. Such damage modes need adequate means of analysis and investigation, the major approaches being experimental characterisation and numerical simulations. This work deals with a deformation behaviour and damage in carbon fabric-reinforced polymer (CFRP) laminates caused by quasi-static and dynamic bending. Experimental tests are carried out first to characterise the behaviour of a CFRP material under tension, in-plane shear and large-deflection bending in quasi-static conditions. The dynamic behaviour of these materials under large-deflection bending is characterised by Izod-type impact tests employing a pendulum-type impactor. A series of impact tests is performed on the material at various impact energy levels up to its fracture, to obtain a transient response of the woven CFRP laminate. Microstructural examination of damage is carried out by optical microscopy and X-ray micro computed tomography (Micro-CT). The damage analysis revealed that through thickness matrix cracking, inter-ply delaminations, intra-ply delamination such as tow debonding, and fabric fracture was the prominent damage modes. These mechanical tests and microstructural studies are accompanied by advanced numerical models developed in a commercial code Abaqus. Among those models are (i) 2D FE models to simulate experimentally observed inter-ply delamination, intra-ply fabric fracture and their subsequent interaction under quasi-static bending conditions and (ii) 3D FE models based on multi-body dynamics used to analyse interacting damage mechanisms in CFRP under large-deflection dynamic bending conditions. In these models, multiple layers of bilinear cohesive-zone elements are placed at the damage locations identified in the Micro CT study. Initiation and progression of inter-laminar delamination and intra-laminar ply fracture are studied by employing cohesive elements. Stress-based criteria are used for damage initiation while fracture-mechanics techniques are employed to capture its progression in composite laminates. The developed numerical models are capable to simulate the studied damage mechanisms as well as their subsequent interaction observed in the tests and microstructural damage analysis. In this study, a novel damage modelling technique based on the cohesive-zone method is proposed for analysis of interaction of various damage modes, which is more efficient than the continuum damage mechanics approach for coupling between failure modes. It was observed that the damage formation in the specimens was from the front to the back at the impact location in the large-deflection impact tests, unlike the back-to-front one in drop-weight tests. The obtained results of simulations showed a good agreement with experimental data, thus demonstrating that the proposed methodology can be used for simulations of discrete damage mechanisms and their interaction during the ultimate fracture of composites in bending. The main outcome of this thesis is a comprehensive experimental and numerical analysis of the deformation and fracture behaviours of CFRP composites under large-deflection bending caused by quasi-static and dynamic loadings. Recommendations on further research developments are also suggested.

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Orientador: Antonio Celso Fonseca de Arruda / Dissertação (mestrado) - Universidade Estadual de Campinas, Faculdade de Engenharia Mecânica / Made available in DSpace on 2018-08-20T08:11:17Z (GMT). No. of bitstreams: 1 Tivelli_Erick_M.pdf: 5369905 bytes, checksum: b9254f481c50f8e409adfc4b024d1c79 (MD5) Previous issue date: 2012 / Resumo: O presente trabalho analisou experimentalmente a utilização de latas de alumínio como absorvedor de energia de impacto. Foram realizados ensaios de compressão estáticos e dinâmicos objetivando correlacionar as deformações das latas com a energia absorvida. Foram analisadas a influência de fatores como, preenchimento da lata (ar ou vermiculita expandida) e disposição do arranjo para receber o impacto nas condições de latas separadas ou agrupadas. O levantamento das características da deformação que estão vinculadas com a absorção do impacto permitem especificar o tipo ideal da estrutura a ser impactada para diferentes aplicações. Os resultados do estudo viabilizaram a utilização das latas de alumínio, na condição de absorvedores de energia com deformação controlada, em barreiras de trenó de impacto / Abstract: The present study examined experimentally the use of aluminum beverage cans as absorbing impact energy elements. Crushing tests were performed aiming to correlate static and dynamic deformations of the cans with the energy absorbed. The study evaluated several conditions for forming a barrier capable of absorbing impact energy during impact tests on the sled. Static and dynamic crushing tests were performed aiming a better understanding of the behavior of the cans in such situations, and also analyzed the influence of factors such as filling the can (air or expanded vermiculite) and arrangement of the impact barrier, this tested the can as a honeycomb and in separate conditions. The study of the characteristics of deformation that are linked to allow the absorption of impact specify the ideal type of structure to be impacted for different applications. The results obtained in this work enabled the use of aluminum cans as agents of energy absorbers for the sled test / Mestrado / Materiais e Processos de Fabricação / Mestre em Engenharia Mecânica

Sublevel caving (SLC) is a mass mining method relying on the flowability of the blasted material. The ore is blasted in slices against caved material which is mainly waste rock. The result of the confined blast is greatly influenced by the interaction between the blasted material and the caved material. During blasting both materials change characteristics; the blasted material increases its porosity and compressibility due to breakage and swelling while the caved material is compacted and decreases in porosity and compressibility. The understanding of the mechanisms involved in this process is of significant importance. The behavior of the caved material (confining material) was studied in laboratory under dynamic loading. A new apparatus was developed to conduct impact tests to simulate blasting conditions. The tested material was a blend of crushed waste rock from drift development in the Kiirunavaara mine with maximum particle size 32 mm. The material was tested for two conditions, i.e. dry and wet (pendular state), and with different impact velocities (low (5 m/s), medium (8 m/s) and high (10-12 m/s)). During the impact tests, two types of measurements were taken; dynamic measurements based on the recordings from the installed accelerometers on the machine and static measurements pre- and post-impact. Additionally, the angle of repose, the impact duration, and the fragmentation was measured. In addition to the laboratory tests, small-scale blasting tests were carried out to investigate the burden behavior in confined conditions. The blasted specimen was a cuboid magnetic mortar block and the confining material was crushed concrete with maximum particle size 16 mm. The blocks were instrumented with custom-made incremental displacement sensor. After the analysis of the results from the above experimental work, two confined pillar tests (test #1 and test #2) were carried out at the Kiirunavaara mine. The preparation work for the pillar tests involved the development of instrumentation and installation techniques. The experimental configuration contained two blastholes and measurement holes in between the blastholes drilled from the neighboring drift. Test #1 mainly focused on the evaluation of the instrumentation and techniques while test #2 was focused on the interaction between the blasted burden and the confining material. The confining material in test #1 was a blend of ore and waste material from drift development at the Kiirunavaara mine. The characteristics of the material were unknown. Test #2 was split into two parts, the confining material in the first part was the same as in the laboratory impact tests and the second part of the pillar was confined by caved masses. The instrumentation was installed in the burden of the pillars and was equipped with accelerometers and displacement sensor. Additional instrumentation was also installed in the confining material. The burden in the small-scale blasting tests reached maximum velocity 29 m/s and maximum displacement 12.6 mm. In pillar tests, the burden movement was in the range of 0.9 to 1.1 m. In both pillar tests, burden erosion material was observed in the gap between the intact and the blasted burden. This material was finer compared to the blasted burden. The origin of this material was from the vicinity of the blastholes. The results of the laboratory tests showed that the wet material exhibited larger compaction zone than that of the dry material. The wet material showed apparent cohesion close to the impact surface of the tested material. A similar observation was made in test #2 where an agglomeration of the confining material, as a result of apparent cohesion, was observed on the surface of the blasted burden. The displacement data from the instrumentation in the burden and inside the confining material showed that the compaction zone follows an inverse exponential behavior. After the blast steeper angles of repose were measured indicating higher frictional forces between the particles. Moreover, the evidence of apparent cohesion and a larger angle of repose indicated the introduction of tensile strength in the material. The mass of the confining material was compressed elastically and plastically during the blast. After the blast, the material recovered its elastic deformation and pushed the blasted burden backward as observed in the small-scale blasting tests and the pillar tests. At this stage, the burden erosion material was compacted. Hence, there were 3 materials, i.e. burden erosion material, burden and confining material, which were compacted with different compaction rates. This condition promotes interlocking of the particles in the materials. If this behavior is correlated with a production SLC ring, then it indicates disturbances in flowability of the blasted material.

Submitted by Claudinei Pracidelli (cpracide@ipen.br) on 2016-06-22T11:45:07Z No. of bitstreams: 0 / Made available in DSpace on 2016-06-22T11:45:07Z (GMT). No. of bitstreams: 0 / Tese (Doutorado em Tecnologia Nuclear) / IPEN/T / Instituto de Pesquisas Energeticas e Nucleares - IPEN-CNEN/SP

Submitted by Claudinei Pracidelli (cpracide@ipen.br) on 2016-06-22T11:45:07Z No. of bitstreams: 0 / Made available in DSpace on 2016-06-22T11:45:07Z (GMT). No. of bitstreams: 0 / O comportamento dos materiais cerâmicos quanto à resistência ao choque térmico é um tema de grande interesse, devido às aplicações em que a confiabilidade frente a variações bruscas de temperatura é necessária. Neste trabalho foi estudado como a variação na proporção dos aditivos Y2O3:Al2O3 e diferentes parâmetros no processamento do carbeto de silício sinterizado via fase líquida como, tipo e temperatura de sinterização, podem influenciar na resistência ao choque térmico deste material. As misturas foram preparadas com 90%SiC+10%Y2O3:Al2O3 em mol, variando as proporções molares dos óxidos entre 2:1 e 1:4, com e sem prévia reação dos aditivos. As misturas foram compactadas e sinterizadas em forno resistivo de grafite nas temperaturas de 1750°C, 1850°C e 1950°C e, por prensagem a quente, a 1750°C e 1850°C, sendo avaliadas quanto à densificação. Após análise dos resultados preliminares, a sinterização sem pressão e as misturas com proporções 1:3 e 1:4 de Y2O3:Al2O3 previamente reagidos foram selecionadas para o estudo da resistência ao choque térmico. Os ciclos térmicos foram realizados com aquecimento em temperaturas de 600°C, 750°C e 900°C e resfriamento brusco em água em temperatura ambiente. A avaliação das amostras quanto à resistência ao choque térmico, feita por meio da determinação de módulo de elasticidade, porosidade, resistência à flexão e por análise microestrutural de trincas. As amostras sinterizadas na temperatura de 1950°C são as que apresentam o melhor desempenho em relação à resistência ao choque térmico, enquanto a variação na proporção Y2O3:Al2O3 de 1:3 para 1:4 não altera significativamente esta propriedade. Nas condições utilizadas, a temperatura máxima de aplicação do SiC sinterizado via fase líquida deve ser limitada a 750°C, permitindo seu uso como trocadores de calor, rolamentos, mancais de bombas submersas, turbinas a gás e sensor de motores automotivos e aeronáuticos. / Tese (Doutorado em Tecnologia Nuclear) / IPEN/T / Instituto de Pesquisas Energeticas e Nucleares - IPEN-CNEN/SP

Submitted by Maria Eneide de Souza Araujo (mearaujo@ipen.br) on 2017-03-10T17:07:28Z No. of bitstreams: 0 / Made available in DSpace on 2017-03-10T17:07:28Z (GMT). No. of bitstreams: 0 / Este estudo teve como objetivo avaliar a adaptação marginal em restaurações classe II em dentina e esmalte dental utilizando um sistema adesivo universal de acordo com três técnicas diferentes de aplicação: Autocondicionante, condicionamento seletivo e condicionamento total, através do sistema de tomografia por coerência óptica (OCT), antes e após ao envelhecimento por termociclagem (TC). Preparos classe II foram confeccionados nas paredes mesial e distal, em 30 molares hígidos humanos, com término da cavidade em esmalte e em dentina. Todos os espécimenes foram restaurados (adesivo Single Bond Universal e resina composta Filtek Z350 XT) nas três técnicas de aplicação. Os dentes foram distribuídos aleatoriamente em três grupos (n=10), sendo um para cada técnica de aplicação adesiva: Grupo I: autocondicionante, Grupo II: condicionamento seletivo e Grupo III: condicionamento total; em seguida os grupos foram avaliados antes e depois a termociclagem pelo sistema de tomografia por coerência ótica. De posse dos corpos de prova devidamente restaurados, partimos para os procedimentos de termociclagem (1000 ciclos de 1 minuto com intervalo de 30 segundos) e a avaliação pelo sistema de Tomografia por Coerência Óptica. Em seguida, as amostras foram examinadas por meio de imagens geradas pelo OCT e os dados foram submetidos ao teste estatístico não-paramétricos de Kruskal-Wallis e Dunn (p<0.05). Foi observada diferença estatisticamente significante da adaptação marginal entre os grupos com término em esmalte (p= 0.0073); para os grupos com término em dentina, não foi observada diferença estatisticamente significante na adaptação marginal (p=0.2063). Conclui-se que o OCT foi, então, capaz de diagnosticar a microinfiltração marginal nas restaurações em cavidades classe II. Existe deterioração das margens e alteração de padrão de infiltração marginal com as diferentes técnicas adesivas dos preparos classe II restauradas com resina em esmalte. Atribui-se à termociclagem a falha de vedamento marginal observada nos espécimes após em esmalte. / Dissertação (Mestrado em Tecnologia Nuclear) / IPEN/D / Instituto de Pesquisas Energeticas e Nucleares - IPEN-CNEN/SP