In this thesis, a new modeling methodology applicable to adhesively bonded joints for crash simulations is presented. Using this approach, adhesive joints can be modeled without using minute solid elements thus reducing the size of the model. Moreover, coarse mesh can be used for substrates in the overlap region of a joint. Both of these improvements together yield significant reduction in simulation run times in crash analysis when compared to solid element representation of adhesive. The modeling can also capture effects of strain rate for a given ambient temperature. In order to develop the efficient modeling procedure mentioned above, experimental, analytical and numerical studies have been carried out. Mechanical behaviors of adhesively bonded joints are studied with the help of double lap shear (DLS) coupon tests conducted at different extension rates and temperatures. The joint specimens are made from dual-phase (DP) steel coupons bonded with epoxy resin. Tests are also carried out to ascertain the behaviors of these component materials at different extension rates and temperatures. A new semi-analytical solution procedure is developed considering material nonlinearity to predict mechanical behaviors of adhesively bonded DLS joints. The joint behaviors using the semi-analytical approach are predicted separately using the Von Mises and exponent Drucker-Prager yield criteria. The predicted force versus extension curves using semi-analytical solution are compared with test results. It is also hypothesized here that, the semi-analytical solution procedure can be used as a base to develop efficient modeling procedures of adhesively bonded joints in FEA. In finite element analysis, both adhesive and substrates are modeled as elastic-plastic materials. It is shown that the shell-solid model of the DLS joint, in which substrates are modeled using shell elements and adhesive is modeled using solid elements, can accurately predict the mechanical behavior of the joint. Both exponent Drucker-Prager and Von Mises material models in ABAQUS are used to calculate force versus extension curves. Numerical and experimental forces versus extension curves are compared. A new methodology for efficient modeling of adhesively bonded joints in LS-DYNA using equivalent material properties in the joint overlap region is proposed. Various models using this methodology are assessed by comparing their results with shell-solid model and test results. Finally, it is also shown that strain rate effects can be included in the efficient modeling approach.

Orientador: Marcos Valério Ribeiro / Resumo: A utilização de materiais compósitos em componentes do setor aeronáutico vem crescendo muito nos últimos anos. Isso se deve ao fato destes materiais apresentarem boas propriedades mecânicas, aliadas a sua baixa massa específica. Dentre estes, os laminados metal fibra, são uma classe de materiais que vem ganhando destaque. Contudo seu emprego na maioria dos casos, requer a confecção de furos, algo que é muito complexo e pode causar danos ao material. Portanto, o objetivo desta pesquisa foi estudar o processo de furação em cheio de um laminado de metal fibra de alumínio 2024-T3/epóxi/fibra de vidro apoiado no alumínio 7075, aplicando diferentes parâmetros de usinagem para avaliar a influência na qualidade dos furos e o desgaste das ferramentas, correlacionando com a potência consumida, vibração, força de avanço, variações dimensionais nos furos e alteração das propriedades mecânicas do material. Para tal, o material foi processado via moldagem por compressão a quente e caracterizado por meio dos ensaios de cisalhamento interlaminar (ILSS), cisalhamento por compressão (CST) e Lap shear. Posteriormente, foram realizados processos de furação utilizando 4000, 6000 e 8000 rpm, bem como avanços de 0,05; 0,1 e 0,2 mm/rot. Após a análise dos resultados, pode-se concluir que os parâmetros influenciaram nos dados de potência, vibração e força de avanço, bem como houve variação significativa nos diâmetros obtidos, sendo que o melhor resultado ocorreu para combinação de 6000 rpm com 0,05mm... (Resumo completo, clicar acesso eletrônico abaixo) / Abstract: The use of composite materials in aeronautical components has been increased in the last years. This is due to these material presente good mechanical properties, allied with low specific mass. Among them, the fiber metal laminated (FML) are a class of materials that has been gaining prominence. However, its use in most cases requires the drilling of holes, which is very complex and can cause damage to the material. Therefore, the objective of this research was to study the conventional drilling process in aeronautical aluminum structures reinforced with fiber metal laminates. Applying different machining parameters, to evaluate the delamination and the wear tools, correlating with the power consumed, vibration, advance force, dimensional variations in the holes and variation of the mechanical properties on material. For this, the material was processed by hot compression molding and characterized by interlaminar shear stress (ILSS), compression shear test (CST) and Lap-shear. Afterwards, drilling processes were carried out using 4000, 6000 and 8000 rpm, as well as an advance of 0.05; 0.1 and 0.2 mm / rot. After the analysis of the results, it was possible to conclude that the parameters influenced the data of power, vibration and force of advance, as well as there was significant variation in the diameters obtained, being the best result occurred for a combination of 6000 rpm with 0,05mm / rot. It can also be stated that there is a tendency of shear strength of the Lap Shear... (Complete abstract click electronic access below) / Mestre

Les interactions hôte-pathogène sont un jeu vaste et complexe entre agent pathogène et hôtepour la victoire de la bataille de la pathogenèse. Plusieurs organismes modèles sont étudiéspour illustrer les mécanismes impliqués dans ces interactions. Dans ma thèse, j'ai utilisé lesplanaires comme un organisme modèle pour explorer les interactions hôte-pathogène. Comme les différents organismes modèles peuvent mettre enévidence les différentes caractéristiques de l'immunité, j'ai décidé de tirer avantage del'absence de connaissances sur l'immunité des planaires en explorant l'inexplorée. Dans monprojet, j'ai infecté les planaires avec 16 bactéries pathogènes : les planaires y sont très résistantes. Pour en explorer lemécanisme j'ai effectué un profilage du transcriptome à partir deplanaires infectées, suivie par un criblage par ARN interférence des gènes up-régulés. J'aidécouvert les gènes qui régissent la résistance antibactérienne dans les planaires, et de façonintéressante, le criblage a permis de mettre en évidence un gène, MORN2, dont la fonctionimmunologique était complètement inconnue. L'induction et l'extinction de l'expression de MORN2dans les macrophages ont révélé que MORN2 contrôle l'internalisation, la réplication et letrafic des bactéries à l'intérieur de la cellule. Dans mon étude, j'ai démontré que MORN2 estun composant de la phagocytose associée à LC3 et qu'il peut surmonter le blocage de lafusion phagolysosomale imposée par les bactéries pathogènes. Ainsi ma thèse met en avantl'importance d'utiliser des organismes modèles inhabituels afin de dévoiler des mécanismesinexplorées et des molécules impliquées dans les interactions hôte-pathogène. / Host-pathogen interaction is a vast and complex interplay between pathogen and hostto conquer the battle of pathogenesis. Several model organisms are being studied to illustratethe mechanisms involved in these interactions. In my thesis I have used planarians as a modelorganism to explore host-pathogen interactions. As different model organismscan highlight different features of immunity I decided to take advantage of lack of knowledgeabout planarian immunity and get benefits from exploring unexplored. In my project I haveinfected planarians with 16 pathogenic bacteria and I found that in contrary to othercommonly used model organisms such as Drosophila, C. elegans and zebrafish the planariansare highly resistant to bacterial infections. To explore the mechanism behind this resistance Iperformed infection induced transcriptome profiling followed by RNA interference screeningof up-regulated gens. I discovered genes governing antibacterial resistance in planarians andinterestingly the screening highlighted a gene MORN2 of which the immunological functionwas completely unknown. The human ortholog of MORN2 is then further assessed for itsantimicrobial function. Induced expression and down regulation of MORN2 in macrophagesrevealed that MORN2 controls uptake, replication and trafficking of bacteria inside the cell.In my study I demonstrated that MORN2 is a component of LC3-associated phagocytosis andit can overcome phagosome maturation blockage imposed by pathogenic bacteria. Thus mythesis propounds the importance of using unusual model organisms to unveil unexploredmechanisms and molecules involved in host-pathogen interactions.

The plasma environment of an active comet provides a unique setting for plasma physics research. The complex interaction of newly created cometary ions with the flowing plasma of the solar wind gives rise to a plethora of plasma physics phenomena, that can be studied over a large range of activity levels as the distance to the sun, and hence the influx of solar energy, varies. In this thesis, we have used measurements of the spacecraft potential by the Rosetta Langmuir probe instrument (LAP) to study the evolution of activity of comet 67P/Churyumov-Gerasimenko as it approached the sun from 3.6 AU in August 2014 to 2.1 AU in March 2015. The measurements are validated by cross-calibration to a fully independent measurement by an electrostatic analyzer, the Ion Composition Analyzer (ICA), also on board Rosetta. The spacecraft was found to be predominantly negatively charged during the time covered by our investigation, driven so by a rather high electron temperature of ~5 eV resulting from the low collision rate between electrons and the tenuous neutral gas. The spacecraft potential exhibited a clear covariation with the neutral density as measured by the ROSINA Comet Pressure Sensor (COPS) on board Rosetta. As the spacecraft potential depends on plasma density and electron temperature, this shows that the neutral gas and the plasma are closely coupled. The neutral density and negative spacecraft potential were higher in the northern hemisphere, which experienced summer conditions during the investigated period due to the nucleus spin axis being tilted toward the sun. In this hemisphere, we found a clear variation of spacecraft potential with comet longitude, exactly as seen for the neutral gas, with coincident peaks in neutral density and spacecraft potential magnitude roughly every 6 h, when sunlit parts of the neck region of the bi- lobed nucleus were in view of the spacecraft. The plasma density was estimated to have increased during the investigated time period by a factor of 8-12 in the northern hemisphere and possibly as much as a factor of 20-44 in the southern hemisphere, due to the combined effects of seasonal changes and decreasing heliocentric distance. The spacecraft potential measurements obtained by LAP generally exhibited good correlation with the estimates from ICA, confirming the accuracy of both of these instruments for measurements of the spacecraft potential.

<div>In the past decade, high-strength reinforcement (fy > 60 ksi) has become more prevalent and more widely accepted. Building codes such as ACI 318-14 do not address the use of highstrength reinforcement for proper development and splicing of reinforcement. Furthermore, research on development of high-strength reinforcement is limited. The objective of the study is to develop a suitable expression for the development and splicing of high-strength reinforcement.</div><div>Of particular interest is evaluating the influence of splice length and confinement on bond strength as well as evaluating the effectiveness of high-strength transverse reinforcement on bond strength. The study tested 22 large-scale concrete beams reinforced with ASTM A615</div><div>Grade 100 deformed steel bars: 11 specimens without transverse reinforcement within the splice region (unconfined) and 11 specimens with transverse reinforcement within the splice region (confined). Splice lengths varied from 40 bar diameters to 120 bar diameters, which are some of the largest ever tested. The effect of the test variables which were systematically studied, found</div><div>that splice strength is nonlinearly related with splice length and can be represented by a power equation. Furthermore, it was found that high-strength transverse reinforcement does not improve bond strength compared with the use of Grade 60 transverse reinforcement. Considering the test results and review of historical test results, an analytical investigation was conducted which developed a simple expression for estimating the capacity of both unconfined</div><div>and confined beams. The results are compared with the current building code design expressions as well as other proposed bond strength equations. The research conducted here provides the basis for development of a design expression that will allow for the incorporation of highstrength reinforcement in future building codes.</div>

Z-pinning is a through-thickness reinforcement technology for polymer composite materials that has been developed and commercialised over the past fifteen years. The through-thickness reinforcement of composites with thin metallic or fibrous pins aids in suppressing delamination, improving impact damage tolerance and increasing joint strength. Z-pins are applied to the composite part during its manufacture. Pins are embedded within sheets of foam and placed over the unconsolidated part. Subsequently, the foam is compacted and the pins transferred into the part, which is usually an uncured prepreg. In this manner, large numbers of pins can be inserted quickly and easily. The pinned composite is then cured using conventional processes. The use of z-pins is currently limited to several high performance composite structures, most notably Formula One racing cars and F/A-18 E/F (Superhornet) fighter aircraft, although the technology has potential applications in a d iverse variety of aerospace and non-aerospace composite structures. A limited understanding of the mechanical performance of z-pinned parts under high load and fatigue loading conditions currently hinders the application of z-pinned composites. The aim of this PhD project is to investigate the mechanical properties, strengthening mechanics and failure mechanisms of z-pinned carbon/epoxy laminates and joints. The effect of z-pin reinforcement on the tensile and flexural properties of laminates under monotonic and fatigue loading is studied. The sensitivity of these properties to the volume content and diameter of the z-pins is systematically studied by experimentation and analytical modelling. This PhD also evaluates the efficacy of z-pins in improving the load-bearing properties of carbon/epoxy lap joints. Improvements to the room temperature and elevated temperature properties of z-pinned lap joints under monotonic and fatigue tensile loading were determined. The effect of strain rate on the load-bearing properties of z-pinned lap joints was also evaluated. A further aim of the PhD project was to assess the z-pin manufacturing process and the microstructural damage caused by that process. The outcome of this study augments the analysis of the me chanical properties of z-pinned laminates and joints.

assessed and strengthened. Performance evaluation of deficient buildings has become a major concern due to devastating earthquakes in the past. In order to justify new provisions in design and assessment codes, experiments and analyses are inherently necessary. In this thesis study, investigations into the behaviour of two deficient reinforced concrete frames built at Middle East Technical University&rsquo / s Structural and Earthquake Laboratory and tested via pseudo-dynamic tests were made. These frames were modelled on the OpenSees platform by following methods of analyses outlined in the Turkish Earthquake Code of 2007 (TEC 2007) and ASCE/SEI-41-06. Both deficient frames were essentially the same, with the only difference being the presence of insufficient lap splices, which was the focus of the study. Time history performance assessments were conducted in accordance to TEC 2007&rsquo / s damage state limits and ASCE/SEI 41-06&rsquo / s performance limits. The damages observed matched the performance levels estimated through the procedure outlined in TEC 2007 rather well. Specific to the specimen with lap splice deficiencies, ASCE/SEI 41-06 was overly conservative in its assessments. TEC 2007&rsquo / s requirements for lap splice lengths were found to be conservative in the laboratory and are able to tolerate deficiencies up to 25% of the required length. With respect to mathematical models, accounting for materials in deficient systems by using nominal but reduced strength properties is not very efficient and unless joint deformations are explicitly accounted for, local deformations cannot be captured.

This study aims to design a novel inserted welding tool to friction stir spot weld SS400 low carbon steel sheets of 4mm thickness. In order to enhance the efficiency of frictional heat generation and to enhance the quality of the welding spot, the welding tool based on a cylindrical tungsten carbide and is inserted by a SS400 low carbon cylinder. The welding apparatus composed of a vertical milling machine and a welding platform that can keep the load between tool and workpiece constant. The plunge load is 8kN and there's no inclination angle on the tools. Welding temperature and the tool plunge depth are measured by thermelcouples and a displacement meter. ¡@¡@At the tool rotational speed of spindle of 900rpm and welding for 60 seconds, the temperature rising rate of the tools with 5 mm and 10 mm inserted material are 5.28 times and 6.31 times greater than the one without insert. While they are 1.36 and 1.42 times greater than at 1200rpm.At the tool rotational speed of spindle of 900rpm and welding for 300 seconds, themaximun welding temperature the tools with 5 mm and 10 mm inserted material can reach are 59¢J and 412¢J higher than the one without insert. While they can reach 35.6¢J and 197.6¢J greater than at 1200rpm. According to the tensile test, the shear failure loads of clad steel plates increase 11.3kN and 15.5kN by using tools with 5 mm and 10 mm inserted material at 900rpm for 60 seconds, and increase 7.6kN and 18.3kN by using tools with 5 mm and 10 mm inserted material at 1200rpm.

In this study, a novel assembled-type tool was used to weld SS400 low-carbon steel plate using the friction stir spot welding. The welding tool was made of tungsten carbide embedded a circular rod made of the low-carbon steel. The superiority of this embedded material not only could effectively promote the interface temperature of the joint, but also the thickness of stir zone. Compared to previous studies, this novel tool can significantly improve the manufacturing cost and the trimming time. The welding apparatus composed of a vertical milling machine and a welding platform. The operating conditions of welding were as followings: the diameter of embedded material, the welding speed, and the vertical load. During the welding process, the interface temperature of the joint, the tool plunge depth, and the vertical load were simultaneously measured by the K-type thermocouple, a displacement sensor, and a load cell. Experimental results revealed that the interface temperature, the thickness of the stir zone, and the tensile strength of the welding joint was proportional to the diameter of the embedded material. The best welding condition is the embedded material diameter of 10mm, the vertical load of 8kN, the welding speed of 1200rpm, and the welding time of 100 seconds.

Minimum requirements for lap splices in reinforced concrete members, stated in building codes of TS-500 and ACI-318, have a certain factor of safety. These standards have been prepared according to research results conducted previously and they are being updated according to results of recent studies. However the reliability of lap splices for minimum requirements needs to be investigated. For this purpose, 6 beam specimens were prepared according to minimum provisions of these standards. The test results were investigated by analytical procedures and also a parametric study was done to compare two standards. For smaller diameter bars both standards give safe results. Results showed that the minimum clear cover given in TS500 is insufficient for lap spliced bars greater than or equal to 26 mm diameter.