Publication detail

Response Surface Method Application to Transonic Business-jet Wing Optimization

POPELA, R. DOUPNÍK, P.

English title

Response Surface Method Application to Transonic Business-jet Wing Optimization

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

The article gives overview of complex aerodynamic optimization approach applied to business-jet aircraft wing design. In the frame of 6th EU FP integrated project CESAR [1] generic business-jet configuration was designed and diverse optimization techniques were applied to airfoil and wing design by members of project consortium. The authors explored particularly response surface method (RSM) potential for global wing aerodynamic optimization. The capability of method to support designer's decisions was assessed and attempt to incorporate basic structural criteria in aerodynamic optimization was made.

Keywords in English

Response surface method (RSM), multidisciplinary optimization, CFD, transonic wing

Released

2010-03-31

Publisher

Asociation of Aviation Manufacturers

Location

Praha

ISSN

1211-877X

Journal

Letecký zpravodaj

Volume

2010

Number

1

Pages from–to

23–27

Pages count

5

BIBTEX


@article{BUT47444,
  author="Robert {Popela} and Petr {Doupník}",
  title="Response Surface Method Application to Transonic Business-jet Wing Optimization",
  journal="Letecký zpravodaj",
  year="2010",
  volume="2010",
  number="1",
  pages="23--27",
  issn="1211-877X"
}