Detail publikace

Response Surface Method Application to Transonic Business-jet Wing Optimization

POPELA, R. DOUPNÍK, P.

Anglický název

Response Surface Method Application to Transonic Business-jet Wing Optimization

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

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.

Klíčová slova anglicky

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

Vydáno

2010-03-31

Nakladatel

Asociation of Aviation Manufacturers

Místo

Praha

ISSN

1211-877X

Časopis

Letecký zpravodaj

Ročník

2010

Číslo

1

Strany od–do

23–27

Počet stran

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"
}