Detail publikace

Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation

MÜLLER, J.

Originální název

Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation

Typ

článek v časopise ve Scopus, Jsc

Jazyk

angličtina

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).

Klíčová slova

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

Autoři

MÜLLER, J.

Vydáno

30. 6. 2022

Nakladatel

Brno University of Technology

Místo

Brno, Czech republic

ISSN

1803-3814

Periodikum

Mendel Journal series

Ročník

28

Číslo

1

Stát

Česká republika

Strany od

63

Strany do

67

Strany počet

5

URL

https://mendel-journal.org/index.php/mendel/article/view/187

BibTex

@article{BUT182804,
  author="Jan {Müller}",
  title="Improving Initial Aerofoil Geometry Using Aerofoil Particle Swarm Optimisation",
  journal="Mendel Journal series",
  year="2022",
  volume="28",
  number="1",
  pages="63--67",
  doi="10.13164/mendel.2022.1.063",
  issn="1803-3814",
  url="https://mendel-journal.org/index.php/mendel/article/view/187"
}