Publication detail
Response Surface Method Application to Transonic Business-jet Wing Optimization
POPELA, R. DOUPNÍK, P.
Czech title
Aerodynamická optimalizace krídla malého dopravního letounu pomocí metody plochy odezvy
English title
Response Surface Method Application to Transonic Business-jet Wing Optimization
Type
journal article - other
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.
Czech abstract
Práce seznamuje s využitím optimaliza?ních metod p?i návrhu k?ídla malého dopravního letounu kategorie business-jet, se zahrnutím základních konstruk?n? pevnostních omezení. Konkrétn? v ní byly prozkoumány možnosti metody plochy odezvy. Byla prokázána efektivita metody plochy odezvy ve spojení s CFD metodami p?i aerodynamické optimalizaci. Základní pevnostní požadavky byly za?len?ny do optimalizace a byl tak ?ešen reálný multidisciplinární problém. Práce byla ?ešena v rámci evropského projektu CESAR 6. rámcového programu EU.
English 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 Czech
Metoda plochy odezvy, multidisciplinární optimalizace, CFD, transsonické k?ídlo
Keywords in English
Response surface method (RSM), multidisciplinary optimization, CFD, transonic wing
RIV year
2010
Released
31.03.2010
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",
month="March",
pages="23--27",
publisher="Asociation of Aviation Manufacturers",
address="Praha",
issn="1211-877X"
}