Original title: Multicriteria Design of Sailplane Airfoils
Translated title: Vícekriteriální návrh leteckých profilů pro kluzáky
Authors: Popelka, Lukáš ; Matějka, M. ; Nožička, J. ; Uruba, Václav
Document type: Papers
Conference/Event: International Symposium on Transport Phenomena /16./, Praha (CZ), 2005-08-29 / 2005-09-01
Year: 2005
Language: eng
Abstract: [eng] [cze]
The article presents results of multicriteria aerodynamic design of airfoils suited for sailplanes. Airfoils for root and tip wing section as well as for empennage has been designed. Wind tunnel testing has proved the feasibility of such approach. The use of turbulators has been proposed on two older airfoils. Příspěvek uvádí výsledky matematického modelování a experimentálního výzkumu aerodynamiky leteckých profilů. Vícekriteriální návrh je zaměřen na sportovní kluzáky.
Keywords: airfoil design; transitional separation bubble
Project no.: CEZ:AV0Z20760514 (CEP), IAA2076403 (CEP)
Funding provider: GA AV ČR
Host item entry: ISTP-16 Book of Abstracts, ISBN 80-86786-04-8

Institution: Institute of Thermomechanics AS ČR (web)
Document availability information: Fulltext is available at the institute of the Academy of Sciences.
Original record: http://hdl.handle.net/11104/0114733

Permalink: http://www.nusl.cz/ntk/nusl-32617


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Research > Institutes ASCR > Institute of Thermomechanics
Conference materials > Papers