Album pintoresco universal : colección de artículos relativos a toda clase de ciencias y artes, parte recopilados de las obras europeas mas acreditadas y parte originales escritos por los principales escritores españoles como son Don Pedro de Madrazo, Don Eugenio de Ochoa, Don Pedro Pidal, Don Patricio de la Escosura, Don Antonio María Segovia... : adornado con exquisitas láminas intercaladas en el texto.

Contiene: T. I (1842. 576 p.) -- T. II (1842. 570 p.)

Cartas físico-matemáticas de Teodosio a Eugenio : que para inteligencia y complemento de la recreacion filosófica /

H. de grab. pleg.: "Navia sc.", "Navarro sc.", "Bausdi sc.", "Asensio f."

Le guerre d'Italia del principe Eugenio di Savoia descritte e commentate.

Mode of access: Internet.

Poesias de Don Eugenio de Tapia.

Mode of access: Internet.

Eugenio Oneghin : lyric opera in three acts /

The libretto, by the composer and K. S. Shilovskiĭ is based on Pushkin's poem. Cf. Loewenberg. Annals of opera.

Obras dramáticas de Manuel Bretón de los Herreros, Juan Eugenio Hartzenbusch, Antonio García Gutiérrez y Tomás Rodríquez Rubí.

Edited by Manuel P. Delgado.

El señor Eugenio Martínez socio de Coucafe

El señor Eugenio Martínez socio de Coucafe. Calarcá. C. 1990.

Eugenio de Ochoa (1815-1872). El hombre de letras en la España de Isabel II

El nombre de Eugenio de Ochoa siempre aparece en los libros sobre la cultura española del siglo XIX, aunque pocas veces con un papel protagonista. Su lugar en la historia de la literatura se halla asociado a otros personajes o a empresas periodísticas de importancia que son recordadas por los nombres de esos otros: El Artista, Federico Madrazo, Pedro Madrazo, Juan Eugenio Hartzenbusch, Victor Hugo, Balzac… Y así Ochoa es siempre el co-creador de una revista, el cuñado de, el amigo de, el traductor de, el editor de… Esta posición secundaria ha restado atractivo al estudio de un hombre que desempeñó un papel fundamental en la conexión de la cultura española con Europa, tanto por ser el vehículo por el que llegaron a España muchos autores contemporáneos como por llevar a cabo el recorrido contrario, mostrando al continente el patrimonio cultural nacional. Sin embargo, esa faceta de intermediario, y no la de literato, contemplada desde una perspectiva más centrada en el contexto y menos en el canon literario tradicional, ofrece unas posibilidades de análisis extremadamente interesantes. Además, la gran pluralidad de sus actividades le convirtió en su tiempo en un observador privilegiado de la realidad cultural y política del país. Ahí se halla el objetivo que ha guiado la realización de este trabajo. Por medio del estudio de su figura se ha pretendido llevar a cabo un análisis de la cultura española del siglo XIX, partiendo de un enfoque sociológico de la misma y prestando más atención a las prácticas en el campo literario que al contenido de la creación. Esa es la razón que explica que, metodológicamente, el trabajo se apoye en dos pilares, cada uno de los cuales sirve de soporte a las dos partes centrales del mismo: la reflexión acerca del “hombre de letras” en el reinado de Isabel II y el papel desempeñado por el mediador cultural en el proceso de transferencia de conocimientos e imágenes nacionales en la Europa del siglo XIX. Al comienzo de cada uno de estos bloques se realiza una reflexión más detallada sobre ambas líneas de análisis que, por supuesto, no son las únicas y no agotan el tema...

Active flow control bump design using hybrid Nash-game coupled to evolutionary algorithms

In this paper, the optimal design of an active flow control device; Shock Control Bump (SCB) on suction and pressure sides of transonic aerofoil to reduce transonic total drag is investigated. Two optimisation test cases are conducted using different advanced Evolutionary Algorithms (EAs); the first optimiser is the Hierarchical Asynchronous Parallel Evolutionary Algorithm (HAPMOEA) based on canonical Evolutionary Strategies (ES). The second optimiser is the HAPMOEA is hybridised with one of well-known Game Strategies; Nash-Game. Numerical results show that SCB significantly reduces the drag by 30% when compared to the baseline design. In addition, the use of a Nash-Game strategy as a pre-conditioner of global control saves computational cost up to 90% when compared to the first optimiser HAPMOEA.

Reduction of environmental effects of civil aircraft through multi-objective flight plan optimisation

With rising environmental alarm, the reduction of critical aircraft emissions including carbon dioxides (CO2) and nitrogen oxides (NOx) is one of most important aeronautical problems. There can be many possible attempts to solve such problem by designing new wing/aircraft shape, new efficient engine, etc. The paper rather provides a set of acceptable flight plans as a first step besides replacing current aircrafts. The paper investigates a green aircraft design optimisation in terms of aircraft range, mission fuel weight (CO2) and NOx using advanced Evolutionary Algorithms coupled to flight optimisation system software. Two multi-objective design optimisations are conducted to find the best set of flight plans for current aircrafts considering discretised altitude and Mach numbers without designing aircraft shape and engine types. The objectives of first optimisation are to maximise range of aircraft while minimising NOx with constant mission fuel weight. The second optimisation considers minimisation of mission fuel weight and NOx with fixed aircraft range. Numerical results show that the method is able to capture a set of useful trade-offs that reduce NOx and CO2 (minimum mission fuel weight).

Hybrid-Game Strategies for multi-objective design optimization in engineering

A number of Game Strategies (GS) have been developed in past decades. They have been used in the fields of economics, engineering, computer science and biology due to their efficiency in solving design optimization problems. In addition, research in multi-objective (MO) and multidisciplinary design optimization (MDO) has focused on developing robust and efficient optimization methods to produce a set of high quality solutions with low computational cost. In this paper, two optimization techniques are considered; the first optimization method uses multi-fidelity hierarchical Pareto optimality. The second optimization method uses the combination of two Game Strategies; Nash-equilibrium and Pareto optimality. The paper shows how Game Strategies can be hybridised and coupled to Multi-Objective Evolutionary Algorithms (MOEA) to accelerate convergence speed and to produce a set of high quality solutions. Numerical results obtained from both optimization methods are compared in terms of computational expense and model quality. The benefits of using Hybrid-Game Strategies are clearly demonstrated

Active transonic aerofoil design optimization using robust multiobjective evolutionary algorithms

The use of adaptive wing/aerofoil designs is being considered, as they are promising techniques in aeronautic/ aerospace since they can reduce aircraft emissions and improve aerodynamic performance of manned or unmanned aircraft. This paper investigates the robust design and optimization for one type of adaptive techniques: active flow control bump at transonic flow conditions on a natural laminar flow aerofoil. The concept of using shock control bump is to control supersonic flow on the suction/pressure side of natural laminar flow aerofoil that leads to delaying shock occurrence (weakening its strength) or boundary layer separation. Such an active flow control technique reduces total drag at transonic speeds due to reduction of wave drag. The location of boundary-layer transition can influence the position and structure of the supersonic shock on the suction/pressure side of aerofoil. The boundarylayer transition position is considered as an uncertainty design parameter in aerodynamic design due to the many factors, such as surface contamination or surface erosion. This paper studies the shock-control-bump shape design optimization using robust evolutionary algorithms with uncertainty in boundary-layer transition locations. The optimization method is based on a canonical evolution strategy and incorporates the concepts of hierarchical topology, parallel computing, and asynchronous evaluation. The use of adaptive wing/aerofoil designs is being considered, as they are promising techniques in aeronautic/ aerospace since they can reduce aircraft emissions and improve aerodynamic performance of manned or unmanned aircraft. This paper investigates the robust design and optimization for one type of adaptive techniques: active flow control bump at transonic flow conditions on a natural laminar flow aerofoil. The concept of using shock control bump is to control supersonic flow on the suction/pressure side of natural laminar flow aerofoil that leads to delaying shock occurrence (weakening its strength) or boundary-layer separation. Such an active flow control technique reduces total drag at transonic speeds due to reduction of wave drag. The location of boundary-layer transition can influence the position and structure of the supersonic shock on the suction/pressure side of aerofoil. The boundarylayer transition position is considered as an uncertainty design parameter in aerodynamic design due to the many factors, such as surface contamination or surface erosion. This paper studies the shock-control-bump shape design optimization using robust evolutionary algorithms with uncertainty in boundary-layer transition locations. The optimization method is based on a canonical evolution strategy and incorporates the concepts of hierarchical topology, parallel computing, and asynchronous evaluation. Two test cases are conducted: the first test assumes the boundary-layer transition position is at 45% of chord from the leading edge, and the second test considers robust design optimization for the shock control bump at the variability of boundary-layer transition positions. The numerical result shows that the optimization method coupled to uncertainty design techniques produces Pareto optimal shock-control-bump shapes, which have low sensitivity and high aerodynamic performance while having significant total drag reduction.

Advanced Computational Intelligence System for inverse aeronautical design optimisation

Abstract—Computational Intelligence Systems (CIS) is one of advanced softwares. CIS has been important position for solving single-objective / reverse / inverse and multi-objective design problems in engineering. The paper hybridise a CIS for optimisation with the concept of Nash-Equilibrium as an optimisation pre-conditioner to accelerate the optimisation process. The hybridised CIS (Hybrid Intelligence System) coupled to the Finite Element Analysis (FEA) tool and one type of Computer Aided Design(CAD) system; GiD is applied to solve an inverse engineering design problem; reconstruction of High Lift Systems (HLS). Numerical results obtained by the hybridised CIS are compared to the results obtained by the original CIS. The benefits of using the concept of Nash-Equilibrium are clearly demonstrated in terms of solution accuracy and optimisation efficiency.