Detail publikačního výsledku

Airfoil Optimization Using Genetic Algorithm

FRIEDL, J.

Originální název

Airfoil Optimization Using Genetic Algorithm

Druh

Konferenční sborník (ne stať)

Originální abstrakt

This paper presents airfoil optimization of aeroplane's wing by genetic algorithm. A direct method of computing aerodynamic characteristics is provided by 2 dimensional computer code XFOIL, which is well known in aerospace industry and solves flow around isolated airfoil. A suitable low order parametrization of the airfoil geometry was designed. A computer program for optimization, which involves certain input and output parameters, was assembled and tested. Results are set of airfoils according to different Fitness functions.

Klíčová slova v angličtině

aerodynamics, optimization, airfoil

Autoři

FRIEDL, J.

Vydáno

04.06.2003

Místo

Brno

ISBN

80-214-2411-7

Kniha

Mendel 2003

Svazek

2003

Číslo

6

Strany od

1

Strany počet

5

BibTex

@proceedings{BUT64116,
  editor="Jan {Friedl}",
  year="2003",
  pages="5",
  address="Brno",
  isbn="80-214-2411-7"
}