Variants of the multi-objective particle swarm optimisation (MOPSO) algorithm are investigated, mainly focusing on swarm topology, to optimise the well-known 2D airfoil design problem. The topologies used are global best, local best, wheel, and von Neumann. The results are compared to the non-dominated sorting genetic algorithm (NSGA-II) and multi-objective tabu search (MOTS) algorithm, and it is found that the attainment surfaces achieved by some of the MOPSO variants completely dominate those of NSGA-II. In general, the MOPSO algorithms also significantly improve diversity of solutions compared to MOTS. The MOPSO algorithm proves its ability to exploit promising solutions in the presence of a large number of infeasible solutions, making i...
In design optimisation problems, it is essential to ensure the convergence to the optimal design spa...
This research proposes, implements and analyses a novel framework for multiobjective optimisation t...
This paper presents a study to design, analyze and optimize an airfoil trailing edge, i.e., shape mo...
Variants of the multi-objective particle swarm optimisation (MOPSO) algorithm are investigated, main...
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...
The research focuses on the aerodynamic design of airfoils for a Multi-Mission Unmanned Aerial Vehic...
The multi-objective particle swarm optimization algorithm (MOPSO) has been applied and modified for ...
The process of aerodynamic shape optimisation requires the development of intelligent models to addr...
High-fidelity aerodynamic design problems are not easily managed, and identifying all Pareto-optimal...
A significant challenge to the application of evo-lutionary multiobjective optimization (EMO) for tr...
Intelligent shape optimisation architecture is developed, validated and applied in the design of hig...
The Particle Swarm Optimization (PSO) method is sensitive to convergence at a sub-optimum solution f...
In this paper, an improved bare-bones multi-objective particle swarm algorithm is proposed to solve ...
In the modern engineering design cycle the use of computational tools becomes a neces- sity. The com...
In design optimisation problems, it is essential to ensure the convergence to the optimal design spa...
This research proposes, implements and analyses a novel framework for multiobjective optimisation t...
This paper presents a study to design, analyze and optimize an airfoil trailing edge, i.e., shape mo...
Variants of the multi-objective particle swarm optimisation (MOPSO) algorithm are investigated, main...
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...
The research focuses on the aerodynamic design of airfoils for a Multi-Mission Unmanned Aerial Vehic...
The multi-objective particle swarm optimization algorithm (MOPSO) has been applied and modified for ...
The process of aerodynamic shape optimisation requires the development of intelligent models to addr...
High-fidelity aerodynamic design problems are not easily managed, and identifying all Pareto-optimal...
A significant challenge to the application of evo-lutionary multiobjective optimization (EMO) for tr...
Intelligent shape optimisation architecture is developed, validated and applied in the design of hig...
The Particle Swarm Optimization (PSO) method is sensitive to convergence at a sub-optimum solution f...
In this paper, an improved bare-bones multi-objective particle swarm algorithm is proposed to solve ...
In the modern engineering design cycle the use of computational tools becomes a neces- sity. The com...
In design optimisation problems, it is essential to ensure the convergence to the optimal design spa...
This research proposes, implements and analyses a novel framework for multiobjective optimisation t...
This paper presents a study to design, analyze and optimize an airfoil trailing edge, i.e., shape mo...