. This paper is the second part of a short course on the utilisation of Evolutionary Algorithms as an effective means to solve the Aerofoil Design Problem in Aerodynamics. In it their application to both Direct and Inverse Aerofoil Design Problem is described, and results are given. Finally, several possible parallel models for Evolutionary Algorithms are discussed, and the results of the application of one of them to the above problem are presented. Keywords: Evolutionary Algorithms, Aerofoil Design Optimisation, Direct Design, Inverse Design, Parallel Evolutionary Algorithms. 1 Introduction In Part I we have briefly described some of the most important instances of Evolutionary Algorithms (EAs), and we have clearly shown their differenc...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
AbstractThis paper presents the recent developments in hierarchical genetic algorithms (HGAs) to spe...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
This thesis presents a modern evolutionary technique for design and optimisation in aeronautics, wi...
AbstractDifferent evolutionary algorithms, by their very nature, will have different search trajecto...
Different evolutionary algorithms, by their very nature, will have different search trajectory chara...
Performance optimisation of aerodynamic shapes plays a critical role in aeronautics and the automati...
Abstract: Search for safety and high efficiency is the driving force in the aerospace industry. This...
An application of hybrid optimization techniques to airfoil design with Navier-Stokes equations is h...
An aerodynamic shape optimization method that uses an evolutionary algorithm known at Differential E...
This paper introduces the necessity of qualitative views on the evolutionary optimisation of airfoil...
Optimisation is a challenge for computerized multidisciplinary design. With multidisciplinary design...
AbstractHierarchical evolutionary algorithms based on genetic algorithms (GAs) and Nash strategy of ...
Unmanned Aerial Vehicle (UAV) design tends to focus on sensors, payload and navigation systems, as t...
This paper describes the optimal synthesis of the internal mechanism for a morphing aerofoil. The ac...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
AbstractThis paper presents the recent developments in hierarchical genetic algorithms (HGAs) to spe...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
This thesis presents a modern evolutionary technique for design and optimisation in aeronautics, wi...
AbstractDifferent evolutionary algorithms, by their very nature, will have different search trajecto...
Different evolutionary algorithms, by their very nature, will have different search trajectory chara...
Performance optimisation of aerodynamic shapes plays a critical role in aeronautics and the automati...
Abstract: Search for safety and high efficiency is the driving force in the aerospace industry. This...
An application of hybrid optimization techniques to airfoil design with Navier-Stokes equations is h...
An aerodynamic shape optimization method that uses an evolutionary algorithm known at Differential E...
This paper introduces the necessity of qualitative views on the evolutionary optimisation of airfoil...
Optimisation is a challenge for computerized multidisciplinary design. With multidisciplinary design...
AbstractHierarchical evolutionary algorithms based on genetic algorithms (GAs) and Nash strategy of ...
Unmanned Aerial Vehicle (UAV) design tends to focus on sensors, payload and navigation systems, as t...
This paper describes the optimal synthesis of the internal mechanism for a morphing aerofoil. The ac...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
AbstractThis paper presents the recent developments in hierarchical genetic algorithms (HGAs) to spe...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...