Search for safety and high efficiency is the driving force in the aerospace industry. This paper reports on application of a relatively new and very promising evolutionary algorithm SOMA with the intent to answer the question on optimal wing geometry. We describe aerodynamic model of the wing, the evolutionary optimisation process and results we obtained. In this contribution present a modern, high performance global optimisation algorithm applied on real engineering application resulting into a set of evolutionary-designed wings which we developed in cooperation with a leading civil aircraft design bureau and manufacturer
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
A novel population structured genetic algorithm (sGA) with embedded potential flow vortex ring pane...
AbstractHierarchical evolutionary algorithms based on genetic algorithms (GAs) and Nash strategy of ...
Abstract: Search for safety and high efficiency is the driving force in the aerospace industry. This...
This thesis presents a modern evolutionary technique for design and optimisation in aeronautics, wi...
Wing shape is an important factor affecting the aerodynamic performance of wings of monocopters and ...
Abstract — Evolutionary Algorithms are often used as an optimization tool. We use this ability here ...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
The design of aircraft wings can be examined in two ways, namely, by aerodynamic analysis and by str...
One of most important challenges in Unmanned (Combat) Aerial Vehicles (UCAV) is improvement of survi...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
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...
Abstract An efficient formulation for the robust shape optimization of aerodynamic objects is introd...
This paper describes the practical application of Hierarchical Asynchronous Parallel Evolutionary Al...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
A novel population structured genetic algorithm (sGA) with embedded potential flow vortex ring pane...
AbstractHierarchical evolutionary algorithms based on genetic algorithms (GAs) and Nash strategy of ...
Abstract: Search for safety and high efficiency is the driving force in the aerospace industry. This...
This thesis presents a modern evolutionary technique for design and optimisation in aeronautics, wi...
Wing shape is an important factor affecting the aerodynamic performance of wings of monocopters and ...
Abstract — Evolutionary Algorithms are often used as an optimization tool. We use this ability here ...
The content of the presented thesis is advanced optimization of the aerofoil wing of a general aircr...
The design of aircraft wings can be examined in two ways, namely, by aerodynamic analysis and by str...
One of most important challenges in Unmanned (Combat) Aerial Vehicles (UCAV) is improvement of survi...
An optimization code called Optima has been developed at the International Centre for Numerical Meth...
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...
Abstract An efficient formulation for the robust shape optimization of aerodynamic objects is introd...
This paper describes the practical application of Hierarchical Asynchronous Parallel Evolutionary Al...
The drag coefficient and the laminar-to-turbulent transition for the aerofoil component of a wing mo...
A novel population structured genetic algorithm (sGA) with embedded potential flow vortex ring pane...
AbstractHierarchical evolutionary algorithms based on genetic algorithms (GAs) and Nash strategy of ...