To support the study of potential utilization of the emerging silicon carbide (SiC) devices, two SiC active switches, namely 1.2 kV, 5 A SiC JFET manufactured by SiCED, and 1.2 kV, 20 A SiC MOSFET by CREE, have been investigated systematically in this thesis. The static and switching characteristics of the two switches have firstly been characterized to get the basic device information. Specific issues in the respective characterization process have been explored and discussed. Many of the characterization procedures presented are generic, so that they can be applied to the study of any future SiC unipolar active switches. Based on the characterization data, different modeling procedures have also been introduced for the two SiC devices. Considerations and measures about model improvement have been investigated and discussed, such as predicting the MOSFET transfer characteristics under high drain-source bias from switching waveforms. Both models have been verified by comparing simulation waveforms with the experimental results. imitations of each model have been explained as well. In order to capture the parasitic ringing in the very fast switching transients, a modeling methodology has also been proposed considering the circuit parasitics, with which a device-package combined simulation can be conducted to reproduce the detailed switching waveforms during the commutation process. This simulation, however, is inadequate to provide deep insights into the physics behind the ringing. Therefore a parametric study has also been conducted about the influence of parasitic impedances on the device's high-speed switching behavior. The main contributors to the parasitic oscillations have been identified to be the switching loop inductance and the device output junction capacitances. The effects of different parasitic components on the device stresses, switching energies, as well as electromagnetic interference (EMI) have all been thoroughly analyzed, whose results exhibit that the parasitic ringing fundamentally does not increase the switching loss but worsens the device stresses and EMI radiation. Based on the parametric study results, this thesis finally compares the difference of SiC JFET and MOSFET in their respective switching behavior, comes up with the concept of device switching speed limit under circuit parasitics, and establishes a general design guideline for high-speed switching circuits on device selection and layout optimization. / Master of Science

Yes / This paper presents the bending tests of four ultra-high performance concrete (UHPC) frame beams and one normal strength concrete (NSC) frame beam, all reinforced with steel-FRP composite bars (SFCBs). A comprehensive analysis was carried out, encompassing evaluation of the failure mode, crack propagation, bearing capacity, deformation, strain response, and plastic rotational capacity of the frame beams. Investigating the effects of concrete type, reinforcement type, and beam-end reinforcement ratio on the flexural performance of the frame beams was a key aspect of this study. A three-dimensional finite element (FE) model of the frame beam was established and rigorously verified. The developed model enabled a detailed parametric analysis involving the steel ratio, the yield strength of the inner core steel bar, the elastic modulus of the FRP, and the ultimate tensile strength of the SFCB. The results indicated a consistent failure mode of all frame beams: crushing of concrete at the beam-end, initiating a sequence of plastic hinge occurrence starting at the beam-end and then progressing to mid-span. The substitution of normal strength concrete with UHPC significantly enhanced various aspects of the frame beams, including the flexural capacity, deformation, ductility, ultimate energy dissipation, and plastic rotational capacity, while inhibiting the generation and expansion of cracks. Notably, the plastic rotation angle of SFCB-UHPC frame beams was 4.9 times greater than those of steel-UHPC frame beams, emphasizing the effectiveness of SFCB in enhancing the beam-end plastic rotational capacity. A decrease in the beam-end reinforcement ratio significantly reduced the flexural capacity, ultimate energy dissipation, and beam-end plastic rotational capacity, while improving ductility. Additionally, the study established a formula for calculating the equivalent plastic hinge length, utilizing the relative compressive zone height and effective section height of the beam-end controlling section as variables, which demonstrated good alignment between predicted and experimental results. / The authors would like to acknowledge the financial support from the High-End Foreign Experts Project of Ministry of Science and Technology, China (G2022014054L), the Natural Science Foundation of Jiangsu Province, China (BK20201436), the Science and Technology Project of Jiangsu Construction System (2023ZD104, 2023ZD105), the Science and Technology Project of Gansu Construction System (JK2021-19), the Science and Technology Cooperation Fund Project of Yangzhou City and Yangzhou University (YZ2022194) and the Science and Technology Project of Yangzhou Construction System (202309, 202312), Graduate Research and Innovation Projects of Jiangsu Province (KYCX24_3750), Jiangsu Provincial Government Scholarship Project (2024), Excellent Doctoral Dissertation Fund of Yangzhou University (2024). / The full-text of this article will be released for public view at the end of the publisher embargo - 12 months after publication.

Stiffeners attached to composite panels and shells may significantly increase the overall buckling load of the resultant stiffened structure. Initially, an extensive literature review was conducted over the past ten years of published work wherein research was conducted on grid stiffened composite structures and stiffened panels, due to their applications in weight sensitive structures. Failure modes identified in the literature had been addressed and divided into a few categories including: buckling of the skin between stiffeners, stiffener crippling and overall buckling. Different methods have been used to predict those failures. These different methods can be divided into two main categories, the smeared stiffener method and the discrete stiffener method. Both of these methods were used and compared in this thesis. First, a buckling analysis was conducted for the case of a grid stiffened composite pressure vessel. Second, a buckling analysis was conducted under the compressive load on the composite stiffened panels for the case of one, two and three longitudinal stiffeners and then, using different parameters, stiffened panels under combined compressive and shear load for the case of one longitudinal centric stiffener and one longitudinal eccentric stiffener, two stiffeners and three stiffeners. / Master of Science / Aircraft in flight is subjected to different loads due to maneuvers and gust, external forces cause internal loads, which depends on the location of the panel in the aircraft, those internal loads, may result in the buckling of the panel. There is an imminent need for structural efficiency, strong and lightweight material. Stiffened composite panels is a promising technology capable of addressing those needs. Composite stiffened panels have many advantages including but not limited to, small manufacturing cost, high stability, great energy absorption, superior damage tolerance etc. The main failure modes for stiffened composite panels is buckling. Buckling failure modes could be of a global nature, local skin buckling or stiffener/rib crippling, predicting those failure is of high practical importance and a predominant design criterion. An extensive literature review on buckling of stiffened composite panels was conducted in this thesis. Buckling analysis as well as a parametric study of grid stiffened composite cylindrical shell for a pressure vessel was conducted, an analytical solution was derived and verified using ABAQUS, a Finite Element Software. Buckling analysis as well as a parametric study of stiffened panels with longitudinal stiffeners, under different structural situations, was also conducted and results verified.

Yes / Hot spotting is a thermal localisation phenomenon in which multiple hot regions form on a brake disc surface during high energy and/or high speed braking events. As an undesired problem, hot spots can result in high order brake judder, audible drone and thermal cracking. This paper presents a finite element model for hot spot modelling which introduces the classical axisymmetric assumptions to the brake pad in 3D by scaling the material properties combined with a subroutine to simulate the heat generation instead of modelling the rotation of the brake pad. The results from the initial feasibility models showed significant improvement in computing efficiency with acceptable accuracy when compared to a traditional FE model without such simplifications. This method was then applied to the 3D simulation of hot spotting on a realistic ventilated brake disc/pad pair and the results showed good correlation with experiments. In order to improve the understanding of the hot spotting mechanism, parametric studies were performed including the effects of solid and ventilated disc geometry, rotational speed and energy, pins, disc run-out, and brake pad length. Based on the analysis of the results, it was identified that the vents and pins affected the hot spot distribution. Speed was shown to be more important on the hot spot generation time and distribution than either the pressure or total energy input. Brake disc run-out was shown to affect the magnitude of both hot spot temperature and height due to the non-linear relationship between local deformation, contact pressure and heat generation. Finally, increasing the brake pad length generated fewer hot spots but the temperature of each hot spot increased.

Yes / To investigate the flexural performance of steel-UHPC (ultra-high performance concrete) composite beams with welded steel shear keys (SSK), eight specimens were experimental studied by four-point bending test. The finite element (FE) models were established based on the experimental results, then, the failure mode, load, deflection, strain and relative interface slip were parametric analyzed. The influences of strength, dimensions and configuration of upper concrete slab, steel beams as well as SSK on flexural performance, in terms of load-deflection response, ductility and ultimate energy dissipation, were studied. The experimental results show that steel-UHPC composite beams have superior bearing capacity, deformation capacity, ductility and energy dissipation ability when compared with steel-NSC (normal strength concrete) composite counterparts. Increasing the height of upper concrete slab has a significant effect on improving bending capacity and flexural stiffness, while increasing the width has a significant effect on enhancing deformation, ductility and ultimate energy dissipation. Increasing the yield strength, thickness of web and flange of steel beams has significant effect on improving bending capacity. Reducing the SSK spacing or increasing the yield strength of SSK, height and thickness slightly improve the cracking, yield and ultimate loads, reduce deflections, enhance the flexural stiffness, slightly weakens the ductility and ultimate energy dissipation. Besides, four types of failure modes were defined, based on reasonable assumptions, formulae for bearing capacity were proposed, and the predicted results fit well with experimental results. The results can be taken as reference for the design and application of steel-UHPC composite beams in long-span and heavy-load structures. / The authors would like to acknowledge the financial support to the work by the Natural Science Foundation of Jiangsu Province, China (BK20201436), High-End Foreign Experts Project of Ministry of Science and Technology, China (G2022014054L), Science and Technology Project of Jiangsu Construction System (2021ZD06, 2018ZD047), Science and Technology Cooperation Fund Project of Yangzhou City and Yangzhou University (YZU212105, YZ2022194), Science and Technology Project of Yangzhou Construction System (202309, 202312, 202204).

No description available.

In this thesis, parametric study and design of Vivaldi antennas and arrays are studied. The parameters of single element antennas and arrays are investigated regarding their effects on the design. The return loss responses and radiation patterns are considered in the parametric study. The results of simulations realized using Ansoft HFSS, a high frequency electromagnetic field simulation program, are shown and discussed. Two different Vivaldi antennas operating in 8.5-10.5 GHz frequency band with return loss responses better than 15 dB are designed based on the results of parametric study. Stripline to slotline transition is used in the feeding section of both antennas. In the same manner, two different 8-element uniform linear arrays operating in 8.5-10.5 GHz with half power beam widths smaller than 12&amp / #730 / and side lobe levels smaller than 13 dB are designed. Binomial and Dolph-Chebyshev feeding techniques are also investigated in order to improve half power beamwidths and side lobe levels of the designed arrays. The designed single element Vivaldi antennas and a linear array of Vivaldi antennas are fabricated. The return loss response and radiation patterns of the fabricated antennas and the array are measured and compared with the simulation results.

Buildings with torsional irregularity represent the main focus of many current investigations. However, despite this volume of research, there is no established framework that describes adequately the seismic vulnerability of reinforced concrete shear wall systems. In this study, the three-dimensional behavior of a particular shear-wall structure under earthquake effects was examined with regard to the nonlinear behavior of the reinforced concrete assembly and the parameters that characterize the structure exposed to seismic motion for damage assessment. A three story reinforced concrete shear-wall building was analyzed using the finite element method based ANSYS software. The scaled model building was subjected to shaking table tests at Saclay, France. The project was led by the Atomic Energy Agency (CEA Saclay, France) under the &ldquo / SMART 2008 Project.&rdquo / The investigation was conducted in two phases. In the first phase, the results of the finite element method and experiments were examined, and were reported in this study. For time history analysis, micro-modeling was preferred due to allowing inclusion the nonlinear effects of concrete and steel for analysis. The guiding parameters (acceleration, displacement, strain) of analytical results are compared with the corresponding values that were measured in the experiments to be able to quantify the validity of models and simulation. For the comparison of v the numerical model results with the experimental results FDE (Frequency Domain Error) method was used. After comparison of the numerical model results with the experimental results, the second phase of the SMART 2008 Project was undertaken. The second phase consisted of two parts summarized as &ldquo / Sensitivity Study&rdquo / and &ldquo / Vulnerability Analyses&rdquo / . However, in this report only the sensitivity study and fragility analyses will be reported. Sensitivity study was done to understand which parameters affect the response of the structure. Twelve parametric cases were investigated under two different ground motions. Different behavior parameters were investigated. The effective damping coefficient was found to affect the structural response at 0.2 g design level as well as at 0.6 g over-design level. At the design level, it was observed that elasticity modulus of concrete and additional masses on the specimen determined as effective on the calculated results. To derive the failure probabilities of this structure under various earthquake forces for the given limit states, fragility curves were obtained. Different seismic indicators such as PGA (Peak ground acceleration), PGV (Peak ground velocity), PGD (Peak ground displacement) and CAV (Cumulative absolute velocity) were used as seismic indicators and MISD (Maximum interstory drift) were used as damage indicator for fragility curves. In all 30 time history analyses were done. Regression analyses using least squares method were performed to determine the median capacity and its deviation. Correlation coefficients of the time history data versus fitted curves obtained from the regression analyses changes between 0.65 and 0.99. The lower cases were for PGD- MISD graphs. The scatter of the fragility curves calculated for each damage limit was slightly wider. HAZUS MH MR1 (2003) damage states were also used for the calculation of the fragility curves and compared with the SMART 2008 damage states.

Durant le vol d'un aéronef, la collision avec un oiseau est un risque important que les autorités de certification imposent de prendre en compte. Dans le cas du choc sur pointe avant, la protection du fond pressurisé est assurée par un bouclier. La compréhension du comportement d'une telle structure sandwich sous impact est essentielle pour permettre l'amélioration des boucliers existants. Ces travaux ont pour buts de comprendre l'influence des différents paramètres de conception du bouclier sur son comportement et sur la protection de la cible, et de mettre en place une méthodologie pour réaliser une telle étude. Pour cela, un modèle éléments finis générique est créé pour être utilisé dans l'étude paramétrique. Une méthode de mesure de la déformée est proposée pour permettre la comparaison rapide d'un grand nombre de cas et la compréhension du comportement de chaque bouclier. Elle s'appuie sur la décomposition de la déformée en trois modes : Indentation, Flexion et Écrasement. Une étude de criblage est ensuite réalisée pour classer les paramètres de définition par ordre d'influence. L'étude paramétrique est réalisée sur les six paramètres les plus influents. Un plan d'expérience de type carré Latin est choisi et sept grandeurs différentes sont suivies. Le cadre des processus gaussiens est utilisé pour créer des modèles réduits, qui sont utilisés pour étudier l'évolution du comportement du bouclier sur l'ensemble du domaine à l'aide d'analyses de sensibilité. Les effets de chaque paramètre sont identifiés et expliqués. Enfin, une méthode pour l'utilisation de ces modèles réduits dans le cadre d'optimisations est proposée. / During an aircraft flight, the possible collision with a bird is a major threat, and the certification authorities require to take ît into account. In the case of a nose strike, the pressurized bulkhead is protected by a shield. Understanding the behaviour under impact of such a sandwich structure is essential. This work has two main goals: understanding the design parameters influence on the shield behaviour, and propose a methodology to conduct this study. Firstly, a generic finite element model is created to be used in a parametric study. A tool to measure the shield deformation is proposed to make it possible to easily compare the behaviour of different shields and to help understanding the behaviour of a shield. This tool is based on the projection ofthe shield deformation on a basis comprising three modes: Indentation, Bendîng and Crushing. A screening study is then conducted to rank the design parameters with respect to their influence. A parametric study is then conducted on the six first parameters. A Latin hyper-square is used for the design of experiment and seven different quantifies are studied. The Gaussian processes framework is used to create surrogates models. Global sensitivity analyses are then conducted to study the variation of the shield behaviour in the whole design space. The effects of each parameterare measured and explained. Finally, a method to minimize the shield mass, using the surrogate models to enforce minimal target protection criteria, is presented.

O comportamento estrutural de veículos de transporte coletivo, quando submetido a eventos de impacto, é de grande relevância na engenharia automobilística, pois principalmente o ônibus, vem se tornando um dos meios de transporte de elevada importância, sendo que seu uso vem aumentando a cada ano. No entanto, as estruturas de ônibus que circulam nas estradas brasileiras não são capazes de resistir, sem causar danos aos passageiros, a eventos de impacto em acidentes, o que pode ser verificado em pesquisas divulgadas pela Agência Nacional de Transportes Terrestres (ANTT) em 2007, que mostra a evolução de acidentes e vítimas envolvendo ônibus, que cada ano aumentam consideravelmente. Neste contexto, pretende-se desenvolver um absorvedor de impacto que aumente a capacidade de absorção da energia de impacto e evite a invasão da região de sobrevivência dos passageiros, e desta forma diminuindo o número de vítimas em acidentes. Serão abordados neste trabalho eventos de impacto semi-frontal, justificado pela gravidade dos acidentes desse tipo nas estradas, sendo este o tipo de acidente que deixa um maior número de vítimas, pois geralmente parte da estrutura lateral do ônibus é removida, expondo os passageiros no período de impacto. Esse efeito é conhecido como “Efeito Abridor de Latas”. O modelo numérico deste trabalho será formado por elementos unifilares, sendo a estrutura do ônibus formada por vigas flexíveis e/ ou rígidas, unidas através de juntas não lineares rotacionais e translacionais. A rigidez de cada junta não linear é obtida a partir de métodos analíticos que descrevem o comportamento do tubo de parede fina quando submetido a impacto. / The structural behavior of transportation vehicles when subjected to events of impact is of great relevance in automotive engineering, mainly because the bus has become a highly important alternative means of transportation, and its use is increasing every year. However, the structures of the buses circulating on Brazilian roads are not able to withstand strong impact, without causing passengers’ injury in events where accidents occur, which can be shown in surveys released by the National Transport Agency (ANTT) in 2007, presenting that the great incidence of accidents with victims involving buses is increasing considerably every year. In this context, the development of an impact absorber that had the capability to increase the impact energy absorption and prevent the invasion of part of bus on the region where passengers are located (reducing the number of fatalities in accidents) are the objectives of this work. In this work, a semi-frontal impact will be presented and studied due to the severity of such accident, as the side of the bus structure is removed, exposing the passengers during the impact. This is the effect known as “Can opener effect”. The numerical model of this study will consist of a single-wire element, with a bus structure formed by flexible and/or rigid beams joined by nonlinear rotational and translational joints. The rigidity of each nonlinear joint is obtained by analytical methods describing the behavior of a thin-walled tube subjected to an impact force.