Skip to main navigation Skip to search Skip to main content

A comparison of multi-objective optimisation metaheuristics on the 2D airfoil design problem

Research output: Contribution to journalArticlepeer-review

Abstract

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 it well suited to problems of this nature.

Original languageEnglish
JournalANZIAM Journal
Volume54
Issue numberSUPPL
DOIs
Publication statusPublished - 1 Dec 2012
Externally publishedYes

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

  1. SDG 3 - Good Health and Well-being
    SDG 3 Good Health and Well-being
  2. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy
  3. SDG 9 - Industry, Innovation, and Infrastructure
    SDG 9 Industry, Innovation, and Infrastructure
  4. SDG 11 - Sustainable Cities and Communities
    SDG 11 Sustainable Cities and Communities
  5. SDG 12 - Responsible Consumption and Production
    SDG 12 Responsible Consumption and Production
  6. SDG 13 - Climate Action
    SDG 13 Climate Action
  7. SDG 17 - Partnerships for the Goals
    SDG 17 Partnerships for the Goals

Keywords

  • 2D airfoil design
  • MOPSO
  • Multi-objective particle swarm optimization

Fingerprint

Dive into the research topics of 'A comparison of multi-objective optimisation metaheuristics on the 2D airfoil design problem'. Together they form a unique fingerprint.

Cite this