Detail publikace

Airfoil Optimization Using Direct Method for Computing Aerodynamic Characteristics

FRIEDL, J.

Originální název

Airfoil Optimization Using Direct Method for Computing Aerodynamic Characteristics

Typ

různé

Jazyk

angličtina

Originální abstrakt

This paper is oriented to utilize programs, which are installed at IAE for computing aerodynamic characteristics of airfoils, especially XFOIL program. Firstly a suitable parameterization of airfoil geometry is carried. This airfoil description is included into optimization loop where certain part of the loop is presented by XFOIL program. From this program a data for computing value of cost function are obtained. A set of computations was done for different cases of cost function scheme. For optimization was used modified genetic algorithm.

Klíčová slova

aerodynamics, airfoil, optimization

Autoři

FRIEDL, J.

Vydáno

1. 6. 2003

Místo

Prague

ISBN

80-86059-35-9

Kniha

3rd International Conference on Advanced Engineering Design 2003

Strany počet

1

URL

Letecký ústav, FSI VUT v Brně

BibTex

@misc{BUT67124,
  author="Jan {Friedl}",
  title="Airfoil Optimization Using Direct Method for Computing Aerodynamic Characteristics",
  booktitle="3rd International Conference on Advanced Engineering Design 2003",
  year="2003",
  volume="2003",
  pages="1",
  address="Prague",
  isbn="80-86059-35-9",
  url="Letecký ústav, FSI VUT v Brně",
  note="miscellaneous"
}