965 resultados para Pérez, Antonio, 1540-1611
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La relación entre la tradición oral y la literatura escrita existe desde antiguo. En este caso, las cancioncillas, las retahílas que acompañan a este tradicional, y universal, juego infantil de Las cuatro esquinas sirven al novelista Mario Vargas Llosa como núcleo generador del relato El paraíso en la otra esquina a la vez que como epítome de la andadura vital de Paul Gauguin. Esta relación entre la vida y la canción nos permite profundizar en la historia del juego de Las cuatro esquinas desde sus orígenes hasta el siglo xxi
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El trabajo presenta resultados de la exploración del campo de velocidades en estelas de distintos modelos de barreras porosas, con vistas a suposible utilización para proteger plantaciones o zonas habitadas de los efectos perniciosos del viento. Los ensayos se han hecho en túnel aerodinámico y, para las medidas, se ha utilizado un anemómetro de hilo caliente. Se ha medido: la velocidad media temporal, el nivel de turbulencia y, en algunos casos, el transporte turbulento y la inclinación del vector velocidad, en cuatro secciones distintas corriente abajo de cada barrera. El trabajo está dividido en ocho capítulos. En el primero se discute la posible utilidad de las barreras en agricultura. En el segundo se revisan ciertas características de las estelas turbulentas de diferentes obstáculos,con el fin de contrastar los resultados obtenidos con otros análogos. En el capítulo tercero se describen los métodos de medida. El cuarto presenta el grueso de los resultados, y los cuatro siguientes: la influencia del número de Reynolds, rugosidad del suelo, perfil del viento incidente y presencia de las paredes y techo del túnel, respectivamente. Los ensayos muestran que los perfiles de velocidades correspondientes a secciones situadas a cierta distancia de la barrera (mayor de seis a ocho veces la altura de ésta) se asemejan a los de un semichorro de baja velocidad que descarga paralelamente a una corriente más rápida. Los perfiles próximos y las condiciones iniciales del semichorro dependen de la configuración de la barrera. El modelo del semichorro equivalente permite calcular las características de la estela a distancias mayores que las que es posible reproducir en los experimentos. Por otra parte, sugiere ciertas modificaciones de la forma de la barrera para aumentar la longitud de la zona protegida del viento. La rugosidad del suelo y la existencia de perfiles de viento distintos del uniforme y más ajustados a la realidad, contribuyen a disminuir la longitud de la zona protegida. Esta observación está de acuerdo con los resultados de otros autores. Se observa que el nivel de turbulencia es muy sensible a las características geométricas de la barrera, lo que sugiere la posibilidad de controlar la capa límite sobre el terreno y, por tanto, el transporte de calor y masa en provecho de la productividad de cultivo. El trabajo que se presenta es parte de un programa más amplio, que tiene por objeto transmitir tecnología avanzada a ciertos dominios de interés para la agricultura y la industria.
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La presente comunicación se enmarca en un estudio financiado por el Consejo Superior de Deportes (CSD) (Ref. 007/UPB10/12). Uno de los objetivos específicos del estudio, en el que se basa la comunicación, es ampliar el conocimiento sobre la influencia de los estilos de vida físicamente activos y sedentarios en la percepción subjetiva de la salud y el bienestar de la juventud española.
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Tit. tomado de principio de texto
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Numerical simulations of axisymmetric reactive jets with one-step Arrhenius kinetics are used to investigate the problem of deflagration initiation in a premixed fuel–air mixture by the sudden discharge of a hot jet of its adiabatic reaction products. For the moderately large values of the jet Reynolds number considered in the computations, chemical reaction is seen to occur initially in the thin mixing layer that separates the hot products from the cold reactants. This mixing layer is wrapped around by the starting vortex, thereby enhancing mixing at the jet head, which is followed by an annular mixing layer that trails behind, connecting the leading vortex with the orifice rim. A successful deflagration is seen to develop for values of the orifice radius larger than a critical value a c in the order of the flame thickness of the planar deflagration δL. Introduction of appropriate scales provides the dimensionless formulation of the problem, with flame initiation characterised in terms of a critical Damköhler number Δc=(a d/δL)2, whose parametric dependence is investigated. The numerical computations reveal that, while the jet Reynolds number exerts a limited influence on the criticality conditions, the effect of the reactant diffusivity on ignition is much more pronounced, with the value of Δc increasing significantly with increasing Lewis numbers. The reactant diffusivity affects also the way ignition takes place, so that for reactants with the flame develops as a result of ignition in the annular mixing layer surrounding the developing jet stem, whereas for highly diffusive reactants with Lewis numbers sufficiently smaller than unity combustion is initiated in the mixed core formed around the starting vortex. The analysis provides increased understanding of deflagration initiation processes, including the effects of differential diffusion, and points to the need for further investigations corporating detailed chemistry models for specific fuel–air mixtures.
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The group vaporization of a monodisperse fuel-spray jet discharging into a hot coflowing gaseous stream is investigated for steady flow by numerical and asymptotic methods with a two-continua formulation used for the description of the gas and liquid phases. The jet is assumed to be slender and laminar, as occurs when the Reynolds number is moderately large, so that the boundary-layer form of the conservation equations can be employed in the analysis. Two dimensionless parameters are found to control the flow structure, namely the spray dilution parameter 1, defined as the mass of liquid fuel per unit mass of gas in the spray stream, and the group vaporization parameter e, defined as the ratio of the characteristic time of spray evolution due to droplet vaporization to the characteristic diffusion time across the jet. It is observed that, for the small values of e often encountered in applications, vaporization occurs only in a thin layer separating the spray from the outer droplet-free stream. This regime of sheath vaporization, which is controlled by heat conduction, is amenable to a simplified asymptotic description, independent of ε,in which the location of the vaporization layer is determined numerically as a free boundary in a parabolic problem involving matching of the separate solutions in the external streams, with appropriate jump conditions obtained from analysis of the quasi-steady vaporization front. Separate consideration of dilute and dense sprays, corresponding, respectively, to the asymptotic limits λ<<1 and λ>>1, enables simplified descriptions to be obtained for the different flow variables, including explicit analytic expressions for the spray penetration distance.
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Conditions are identified under which analyses of laminar mixing layers can shed light on aspects of turbulent spray combustion. With this in mind, laminar spray-combustion models are formulated for both non-premixed and partially premixed systems. The laminar mixing layer separating a hot-air stream from a monodisperse spray carried by either an inert gas or air is investigated numerically and analytically in an effort to increase understanding of the ignition process leading to stabilization of high-speed spray combustion. The problem is formulated in an Eulerian framework, with the conservation equations written in the boundary-layer approximation and with a one-step Arrhenius model adopted for the chemistry description. The numerical integrations unveil two different types of ignition behaviour depending on the fuel availability in the reaction kernel, which in turn depends on the rates of droplet vaporization and fuel-vapour diffusion. When sufficient fuel is available near the hot boundary, as occurs when the thermochemical properties of heptane are employed for the fuel in the integrations, combustion is established through a precipitous temperature increase at a well-defined thermal-runaway location, a phenomenon that is amenable to a theoretical analysis based on activation-energy asymptotics, presented here, following earlier ideas developed in describing unsteady gaseous ignition in mixing layers. By way of contrast, when the amount of fuel vapour reaching the hot boundary is small, as is observed in the computations employing the thermochemical properties of methanol, the incipient chemical reaction gives rise to a slowly developing lean deflagration that consumes the available fuel as it propagates across the mixing layer towards the spray. The flame structure that develops downstream from the ignition point depends on the fuel considered and also on the spray carrier gas, with fuel sprays carried by air displaying either a lean deflagration bounding a region of distributed reaction or a distinct double-flame structure with a rich premixed flame on the spray side and a diffusion flame on the air side. Results are calculated for the distributions of mixture fraction and scalar dissipation rate across the mixing layer that reveal complexities that serve to identify differences between spray-flamelet and gaseous-flamelet problems.
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It has been reasoned that the structures of strongly cellular flames in very lean mixtures approach an array of flame balls, each burning as if it were isolated, thereby indicating a connection between the critical conditions required for existence of steady flame balls and those necessary for occurrence of self-sustained premixed combustion. This is the starting assumption of the present study, in which structures of near-limit steady sphericosym-metrical flame balls are investigated with the objective of providing analytic expressions for critical combustion conditions in ultra-lean hydrogen-oxygen mixtures diluted with N2 and water vapor. If attention were restricted to planar premixed flames, then the lean-limit mole fraction of H2 would be found to be roughly ten percent, more than twice the observed flammability limits, thereby emphasizing the relevance of the flame-ball phenomena. Numerical integrations using detailed models for chemistry and radiation show that a onestep chemical-kinetic reduced mechanism based on steady-state assumptions for all chemical intermediates, together with a simple, optically thin approximation for water-vapor radiation, can be used to compute near-limit fuel-lean flame balls with excellent accuracy. The previously developed one-step reaction rate includes a crossover temperature that determines in the first approximation a chemical-kinetic lean limit below which combustión cannot occur, with critical conditions achieved when the diffusion-controlled radiation-free peak temperature, computed with account taken of hydrogen Soret diffusion, is equal to the crossover temperature. First-order corrections are found by activation-energy asymptotics in a solution that involves a near-field radiation-free zone surrounding a spherical flame sheet, together with a far-field radiation-conduction balance for the temperature profile. Different scalings are found depending on whether or not the surrounding atmosphere contains wáter vapor, leading to different analytic expressions for the critical conditions for flame-ball existence, which give results in very good agreement with those obtained by detailed numerical computations.
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Este trabajo pretende aportar algunos elementos a la historia de la natación, un campo concreto de la actividad humana en su aspecto físico. No es realmente historia, en el sentido científico del término, en cuanto que los aspectos analizados no han sido interpretados en sus causas mediatas, ni se han tenido en cuenta criterios sociológicos o económicos. La evolución de los récords de natación que aquí se recoge es primordialmente descriptiva. Sin embargo, la metodología seguida y los aspectos complementarios que se abordan bien pueden considerarse como datos auxiliares para una "historia total" de la natación mundial, aún por hacer. El capítulo 1 trata de las dificultades que se presentan en la delimitación del concepto de récord. En el capítulo 2 se recoge la evolución histórica del concepto de récord mundial en natación. El capítulo 3 analiza las dificultades metodológicas en el tratamiento de los datos. El capítulo 4 presenta una síntesis gráfica de la evolución de los récords mundiales, basada en el análisis de los parámetros previamente definidos. Se extraen algunas características generales que servirán para fijar los límites de una breve discusión de los resultados y presentar una serie de conclusiones, que se exponen en el capítulo 5. Se incluye un repertorio de apéndices, en los cuales se aclaran muchas cuestiones que se manejan ampliamente a lo largo del trabajo y en los que recojo asimismo una serie de agrupaciones de los récords mundiales que facilitan su estudio. Se presenta también un capítulo de bibliografía utilizada.
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This work presents the main theories and models formulated with the purpose of offering a global overview on the acquisition of knowledge and skills involved in the initial development of expert competence. Setting from this background, we developed an empirical work whose main purpose is to define those factors in a complex learning situation such as chapter-sized in a knowledge-rich domain. The results obtained in a sample of Master students reveal that the several variables intervening, such as the qualitative organization of knowledge, intellectual ability, motivation, the deliberate use of strategies, and a rich learning environment, contribute in an independent way to provide an explanation for the acquired knowledge.
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GPLSI Compendium App se trata de una aplicación móvil que hará las veces de un sistema de gestión y difusión de contenidos digitales, en la que el usuario podrá realizar resúmenes de textos de diferentes webs, tales como artículos o noticias, y posteriormente compartir esos resúmenes en sus redes sociales o a través del correo. Se le proporcionarán varios métodos de resumen, así como las descripciones y un pequeño tutorial de cómo utilizar la aplicación.
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Mode of access: Internet.
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Mode of access: Internet.
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Mode of access: Internet.