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Statements

Subject Item
n2:RIV%2F00216305%3A26210%2F10%3APU86868%21RIV10-MSM-26210___
rdf:type
n5:Vysledek skos:Concept
dcterms:description
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. 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.
dcterms:title
Response Surface Method Application to Transonic Business-jet Wing Optimization Response Surface Method Application to Transonic Business-jet Wing Optimization
skos:prefLabel
Response Surface Method Application to Transonic Business-jet Wing Optimization Response Surface Method Application to Transonic Business-jet Wing Optimization
skos:notation
RIV/00216305:26210/10:PU86868!RIV10-MSM-26210___
n3:aktivita
n14:P
n3:aktivity
P(1M0501)
n3:cisloPeriodika
1
n3:dodaniDat
n13:2010
n3:domaciTvurceVysledku
n12:4704665 n12:1844199
n3:druhVysledku
n9:J
n3:duvernostUdaju
n6:S
n3:entitaPredkladatele
n8:predkladatel
n3:idSjednocenehoVysledku
285039
n3:idVysledku
RIV/00216305:26210/10:PU86868
n3:jazykVysledku
n17:eng
n3:klicovaSlova
Response surface method (RSM), multidisciplinary optimization, CFD, transonic wing
n3:klicoveSlovo
n4:transonic%20wing n4:multidisciplinary%20optimization n4:Response%20surface%20method%20%28RSM%29 n4:CFD
n3:kodStatuVydavatele
CZ - Česká republika
n3:kontrolniKodProRIV
[BF5F9D7DB4EE]
n3:nazevZdroje
Letecký zpravodaj
n3:obor
n18:JU
n3:pocetDomacichTvurcuVysledku
2
n3:pocetTvurcuVysledku
2
n3:projekt
n7:1M0501
n3:rokUplatneniVysledku
n13:2010
n3:svazekPeriodika
2010
n3:tvurceVysledku
Popela, Robert Doupník, Petr
s:issn
1211-877X
s:numberOfPages
5
n16:organizacniJednotka
26210