COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING

dc.contributor.author	Lahuta , Martin
dc.contributor.author	Pátek , Zdeněk
dc.contributor.author	Szöllös , András
dc.date.accessioned	2017-02-09T09:36:27Z
dc.date.available	2017-02-09T09:36:27Z
dc.date.issued	2014
dc.identifier.citation	Acta Polytechnica. 2014, vol. 54, no. 6, p. 420-425.
dc.identifier.issn	1210-2709 (print)
dc.identifier.issn	1805-2363 (online)
dc.identifier.uri	http://hdl.handle.net/10467/67171
dc.description.abstract	An optimization method consisting of genetic and evolution optimization algorithm and a solver using nonlinear aerodynamics was applied on design of low-speed wing. Geometric parameterization of wing uses standard geometric quantities commonly used for the description of wing geomtery. The method seems to provide good teliable results at low computer capacity requirements.	en
dc.format.mimetype	application/pdf
dc.language.iso	eng
dc.publisher	České vysoké učení technické v Praze	cs
dc.publisher	Czech Technical University in Prague	en
dc.relation.ispartofseries	Acta Polytechnica
dc.relation.uri	https://ojs.cvut.cz/ojs/index.php/ap/article/view/2270
dc.rights	Creative Commons Attribution 4.0 International License	en
dc.rights.uri	http://creativecommons.org/licenses/by/4.0/
dc.title	COMPUTATIONAL AERODYNAMIC OPTIMIZATION OF LOW-SPEED WING
dc.type	article	en
dc.date.updated	2017-02-09T09:36:27Z
dc.identifier.doi	10.14311/AP.2014.54.0420
dc.rights.access	openAccess
dc.type.status	Peer-reviewed
dc.type.version	publishedVersion

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