22 resultados para Orthogonal polynomials of a discrete variable
Resumo:
This article presents a mathematical method for producing hard-chine ship hulls based on a set of numerical parameters that are directly related to the geometric features of the hull and uniquely define a hull form for this type of ship. The term planing hull is used generically to describe the majority of hard-chine boats being built today. This article is focused on unstepped, single-chine hulls. B-spline curves and surfaces were combined with constraints on the significant ship curves to produce the final hull design. The hard-chine hull geometry was modeled by decomposing the surface geometry into boundary curves, which were defined by design constraints or parameters. In planing hull design, these control curves are the center, chine, and sheer lines as well as their geometric features including position, slope, and, in the case of the chine, enclosed area and centroid. These geometric parameters have physical, hydrodynamic, and stability implications from the design point of view. The proposed method uses two-dimensional orthogonal projections of the control curves and then produces three-dimensional (3-D) definitions using B-spline fitting of the 3-D data points. The fitting considers maximum deviation from the curve to the data points and is based on an original selection of the parameterization. A net of B-spline curves (stations) is then created to match the previously defined 3-D boundaries. A final set of lofting surfaces of the previous B-spline curves produces the hull surface.
Resumo:
Advanced control techniques like V2, Vout hysteresis or V2Ic can strongly reduce the required output capacitance in PowerSoC converters. Techniques to analyze power converters based on the analysis of the frequency response are not suitable for ripple-based controllers that use fast-scale dynamics to control the power stage. This paper proves that the use of discrete modeling together with Floquet theory is a very powerful tool to model the system and derive stable region diagrams for sensitivity analysis. It is applied to V 2Ic control, validating experimentally that Floquet theory predicts accurately subharmonic oscillations. This method is applied to several ripplebased controllers, providing higher accuracy when it is compared with other techniques based on the frequency response. The paper experimentally validates the usefulness of the discrete modeling and the Floquet theory on a 5 MHz Buck converter with a V 2Ic control.
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Los ensayos virtuales de materiales compuestos han aparecido como un nuevo concepto dentro de la industria aeroespacial, y disponen de un vasto potencial para reducir los enormes costes de certificación y desarrollo asociados con las tediosas campañas experimentales, que incluyen un gran número de paneles, subcomponentes y componentes. El objetivo de los ensayos virtuales es sustituir algunos ensayos por simulaciones computacionales con alta fidelidad. Esta tesis es una contribución a la aproximación multiescala desarrollada en el Instituto IMDEA Materiales para predecir el comportamiento mecánico de un laminado de material compuesto dadas las propiedades de la lámina y la intercara. La mecánica de daño continuo (CDM) formula el daño intralaminar a nivel constitutivo de material. El modelo de daño intralaminar se combina con elementos cohesivos para representar daño interlaminar. Se desarrolló e implementó un modelo de daño continuo, y se aplicó a configuraciones simples de ensayos en laminados: impactos de baja y alta velocidad, ensayos de tracción, tests a cortadura. El análisis del método y la correlación con experimentos sugiere que los métodos son razonablemente adecuados para los test de impacto, pero insuficientes para el resto de ensayos. Para superar estas limitaciones de CDM, se ha mejorado la aproximación discreta de elementos finitos enriqueciendo la cinemática para incluir discontinuidades embebidas: el método extendido de los elementos finitos (X-FEM). Se adaptó X-FEM para un esquema explícito de integración temporal. El método es capaz de representar cualitativamente los mecanismos de fallo detallados en laminados. Sin embargo, los resultados muestran inconsistencias en la formulación que producen resultados cuantitativos erróneos. Por último, se ha revisado el método tradicional de X-FEM, y se ha desarrollado un nuevo método para superar sus limitaciones: el método cohesivo X-FEM estable. Las propiedades del nuevo método se estudiaron en detalle, y se concluyó que el método es robusto para implementación en códigos explícitos dinámicos escalables, resultando una nueva herramienta útil para la simulación de daño en composites. Virtual testing of composite materials has emerged as a new concept within the aerospace industry. It presents a very large potential to reduce the large certification costs and the long development times associated with the experimental campaigns, involving the testing of a large number of panels, sub-components and components. The aim of virtual testing is to replace some experimental tests by high-fidelity numerical simulations. This work is a contribution to the multiscale approach developed in Institute IMDEA Materials to predict the mechanical behavior of a composite laminate from the properties of the ply and the interply. Continuum Damage Mechanics (CDM) formulates intraply damage at the the material constitutive level. Intraply CDM is combined with cohesive elements to model interply damage. A CDM model was developed, implemented, and applied to simple mechanical tests of laminates: low and high velocity impact, tension of coupons, and shear deformation. The analysis of the results and the comparison with experiments indicated that the performance was reasonably good for the impact tests, but insuficient in the other cases. To overcome the limitations of CDM, the kinematics of the discrete finite element approximation was enhanced to include mesh embedded discontinuities, the eXtended Finite Element Method (X-FEM). The X-FEM was adapted to an explicit time integration scheme and was able to reproduce qualitatively the physical failure mechanisms in a composite laminate. However, the results revealed an inconsistency in the formulation that leads to erroneous quantitative results. Finally, the traditional X-FEM was reviewed, and a new method was developed to overcome its limitations, the stable cohesive X-FEM. The properties of the new method were studied in detail, and it was demonstrated that the new method was robust and can be implemented in a explicit finite element formulation, providing a new tool for damage simulation in composite materials.
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Services in smart environments pursue to increase the quality of people?s lives. The most important issues when developing this kind of environments is testing and validating such services. These tasks usually imply high costs and annoying or unfeasible real-world testing. In such cases, artificial societies may be used to simulate the smart environment (i.e. physical environment, equipment and humans). With this aim, the CHROMUBE methodology guides test engineers when modeling human beings. Such models reproduce behaviors which are highly similar to the real ones. Originally, these models are based on automata whose transitions are governed by random variables. Automaton?s structure and the probability distribution functions of each random variable are determined by a manual test and error process. In this paper, it is presented an alternative extension of this methodology which avoids the said manual process. It is based on learning human behavior patterns automatically from sensor data by using machine learning techniques. The presented approach has been tested on a real scenario, where this extension has given highly accurate human behavior models,
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Genetic algorithms (GA) have been used for the minimization of the aerodynamic drag of a train subject to front wind. The significant importance of the external aerodynamic drag on the total resistance a train experiments as the cruise speed is increased highlights the interest of this study. A complete description of the methodology required for this optimization method is introduced here, where the parameterization of the geometry to be optimized and the metamodel used to speed up the optimization process are detailed. A reduction of about a 25% of the initial aerodynamic drag is obtained in this study, what confirms GA as a proper method for this optimization problem. The evolution of the nose shape is consistent with the literature. The advantage of using metamodels is stressed thanks to the information of the whole design space extracted from it. The influence of each design variable on the objective function is analyzed by means of an ANOVA test.
Resumo:
Impact response surfaces (IRSs) depict the response of an impact variable to changes in two explanatory variables as a plotted surface. Here, IRSs of spring and winter wheat yields were constructed from a 25-member ensemble of process-based crop simulation models. Twenty-one models were calibrated by different groups using a common set of calibration data, with calibrations applied independently to the same models in three cases. The sensitivity of modelled yield to changes in temperature and precipitation was tested by systematically modifying values of 1981-2010 baseline weather data to span the range of 19 changes projected for the late 21st century at three locations in Europe.
Optimización de cimentaciones directas de medianería y esquina mediante modelos de elementos finitos
Resumo:
Existe un amplio catálogo de posibles soluciones para resolver la problemática de las zapatas de medianería así como, por extensión, las zapatas de esquina como caso particular de las anteriores. De ellas, las más habitualmente empleadas en estructuras de edificación son, por un lado, la utilización de una viga centradora que conecta la zapata de medianería con la zapata del pilar interior más próximo y, por otro, la colaboración de la viga de la primera planta trabajando como tirante. En la primera solución planteada, el equilibrio de la zapata de medianería y el centrado de la respuesta del terreno se consigue gracias a la colaboración del pilar interior con su cimentación y al trabajo a flexión de la viga centradora. La modelización clásica considera que se logra un centrado total de la reacción del terreno, con distribución uniforme de las tensiones de contacto bajo ambas zapatas. Este planteamiento presupone, por tanto, que la viga centradora logra evitar cualquier giro de la zapata de medianería y que el pilar puede, por ello, considerarse perfectamente empotrado en la cimentación. En este primer modelo, el protagonismo fundamental recae en la viga centradora, cuyo trabajo a flexión conduce frecuentemente a unas escuadrías y a unas cuantías de armado considerables. La segunda solución, plantea la colaboración de la viga de la primera planta, trabajando como tirante. De nuevo, los métodos convencionales suponen un éxito total en el mecanismo estabilizador del tirante, que logra evitar cualquier giro de la zapata de medianería, dando lugar a una distribución de tensiones también uniforme. Los modelos convencionales existentes para el cálculo de este tipo de cimentaciones presentan, por tanto, una serie de simplificaciones que permiten el cálculo de las mismas, por medios manuales, en un tiempo razonable, pero presentan el inconveniente de su posible alejamiento del comportamiento real de la cimentación, con las consecuencias negativas que ello puede suponer en el dimensionamiento de estos elementos estructurales. La presente tesis doctoral desarrolla un contraste de los modelos convencionales de cálculo de cimentaciones de medianería y esquina, mediante un análisis alternativo con modelos de elementos finitos, con el objetivo de poner de manifiesto las diferencias entre los resultados obtenidos con ambos tipos de modelización, analizar cuáles son las variables que más influyen en el comportamiento real de este tipo de cimentaciones y proponer un nuevo modelo de cálculo, de tipo convencional, más ajustado a la realidad. El proceso de investigación se desarrolla mediante una etapa experimental virtual que utiliza como modelo un pórtico tipo de edificación, ortogonal, de hormigón armado, con dos vanos y número variable de plantas. Tras identificar el posible giro de la cimentación como elemento clave en el comportamiento de las zapatas de medianería y de esquina, se adoptan como variables de estudio aquellas que mayor influencia puedan tener sobre el citado giro de las zapatas y sobre la rigidez del conjunto del elemento estructural. Así, se han estudiado luces de 3 m a 7 m, diferente número de plantas desde baja+1 hasta baja+4, resistencias del terreno desde 100 kN/m2 hasta 300 kN/m2, relaciones de forma de la zapata de medianería de 1,5 : 1 y 2 : 1, aumento y reducción de la cuantía de armado de la viga centradora y variación del canto de la viga centradora desde el mínimo canto compatible con el anclaje de la armadura de los pilares hasta un incremento del 75% respecto del citado canto mínimo. El conjunto de pórticos generados al aplicar las variables indicadas, se ha calculado tanto por métodos convencionales como por el método de los elementos finitos. Los resultados obtenidos ponen de manifiesto importantes discrepancias entre ambos métodos que conducen a importantes diferencias en el dimensionamiento de este tipo de cimentaciones. El empleo de los métodos tradicionales da lugar, por un lado, a un sobredimensionamiento de la armadura de la viga centradora y, por otro, a un infradimensionamiento, tanto del canto de la viga centradora, como del tamaño de la zapata de medianería y del armado de la viga de la primera planta. Finalizado el análisis y discusión de resultados, la tesis propone un nuevo método alternativo, de carácter convencional y, por tanto, aplicable a un cálculo manual en un tiempo razonable, que permite obtener los parámetros clave que regulan el comportamiento de las zapatas de medianería y esquina, conduciendo a un dimensionamiento más ajustado a las necesidades reales de este tipo de cimentación. There is a wide catalogue of possible solutions to solve the problem of party shoes and, by extension, corner shoes as a special case of the above. From all of them, the most commonly used in building structures are, on one hand, the use of a centering beam that connects the party shoe with the shoe of the nearest interior pillar and, on the other hand, the collaboration of the beam of the first floor working as a tie rod. In the first proposed solution, the balance of the party shoe and the centering of the ground response is achieved thanks to the collaboration of the interior pillar with his foundation along with the bending work of the centering beam. Classical modeling considers that a whole centering of the ground reaction is achieved, with uniform contact stress distribution under both shoes. This approach to the issue presupposes that the centering beam manages to avoid any rotation of the party shoe, so the pillar can be considered perfectly embedded in the foundation. In this first model, the leading role lies in the centering beam, whose bending work usually leads to important section sizes and high amounts of reinforced. The second solution, consideres the collaboration of the beam of the first floor, working as tie rod. Again, conventional methods involve a total success in the stabilizing mechanism of the tie rod, that manages to avoid any rotation of the party shoe, resulting in a stress distribution also uniform. Existing conventional models for calculating such foundations show, therefore, a series of simplifications which allow calculation of the same, by manual means, in a reasonable time, but have the disadvantage of the possible distance from the real behavior of the foundation, with the negative consequences this could bring in the dimensioning of these structural elements. The present thesis develops a contrast of conventional models of calculation of party and corner foundations by an alternative analysis with finite element models with the aim of bring to light the differences between the results obtained with both types of modeling, analysis which are the variables that influence the real behavior of this type of foundations and propose a new calculation model, conventional type, more adjusted to reality. The research process is developed through a virtual experimental stage using as a model a typical building frame, orthogonal, made of reinforced concrete, with two openings and variable number of floors. After identifying the possible spin of the foundation as the key element in the behavior of the party and corner shoes, it has been adopted as study variables, those that may have greater influence on the spin of the shoes and on the rigidity of the whole structural element. So, it have been studied lights from 3 m to 7 m, different number of floors from lower floor + 1 to lower floor + 4, máximum ground stresses from 100 kN/m2 300 kN/m2, shape relationships of party shoe 1,5:1 and 2:1, increase and decrease of the amount of reinforced of the centering beam and variation of the height of the centering beam from the minimum compatible with the anchoring of the reinforcement of pillars to an increase of 75% from the minimum quoted height. The set of frames generated by applying the indicated variables, is calculated both by conventional methods such as by the finite element method. The results show significant discrepancies between the two methods that lead to significant differences in the dimensioning of this type of foundation. The use of traditional methods results, on one hand, to an overdimensioning of the reinforced of the centering beam and, on the other hand, to an underdimensioning, both the height of the centering beam, such as the size of the party shoe and the reinforced of the beam of the first floor. After the analysis and discussion of results, the thesis proposes a new alternative method, conventional type and, therefore, applicable to a manual calculation in a reasonable time, that allows to obtain the key parameters that govern the behavior of party and corner shoes, leading to a dimensioning more adjusted to the real needings of this type of foundation.