Detail publikace

Response Surface Method Application to Transonic Business-jet Wing Optimization

POPELA, R. DOUPNÍK, P.

Originální název

Response Surface Method Application to Transonic Business-jet Wing Optimization

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

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

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

Autoři

POPELA, R.; DOUPNÍK, P.

Rok RIV

2010

Vydáno

31. 3. 2010

Nakladatel

Asociation of Aviation Manufacturers

Místo

Praha

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Ročník

2010

Číslo

1

Stát

Česká republika

Strany od

23

Strany do

27

Strany počet

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"
}