Detail publikace

Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation

MÜLLER, J.

Anglický název

Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation

Typ

článek v časopise ve Scopus, Jsc

Jazyk

en

Originální abstrakt

Advanced optimisation of the aerofoil wing of a general aircraft is the main subject of this paper. Meta-heuristic optimisation techniques, especially swarm algorithms, were used. Subsequently, a new variant denoted as aerofoil particle swarm optimisation (aPSO) was developed from the original particle swarm optimisation (PSO). A parametric model based on B-spline was used to optimise the initial aerofoil. The simulation software Xfoil was calculating basic aerodynamic features (lift, drag, moment).

Anglický abstrakt

Advanced optimisation of the aerofoil wing of a general aircraft is the main subject of this paper. Meta-heuristic optimisation techniques, especially swarm algorithms, were used. Subsequently, a new variant denoted as aerofoil particle swarm optimisation (aPSO) was developed from the original particle swarm optimisation (PSO). A parametric model based on B-spline was used to optimise the initial aerofoil. The simulation software Xfoil was calculating basic aerodynamic features (lift, drag, moment).

Klíčová slova anglicky

Aerofoil Wing; Bezier-PARSEC Model; Metaheuristics; Optimisation; Swarm Algorithms; Wing; Xfoil

Vydáno

30.06.2022

Nakladatel

Brno University of Technology

Místo

Brno, Czech republic

ISSN

1803-3814

Ročník

28

Číslo

1

Strany od–do

63–67

Počet stran

5

BIBTEX


@article{BUT182804,
  author="Jan {Müller},
  title="Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation",
  year="2022",
  volume="28",
  number="1",
  month="June",
  pages="63--67",
  publisher="Brno University of Technology",
  address="Brno, Czech republic",
  issn="1803-3814"
}