LoginProceedings Vol. 21 (2015)
ENGINEERING MECHANICS 2015
21st INTERNATIONAL CONFERENCE
May 11 – 14, 2015, Svratka, Czech Republic
;
May 11 – 14, 2015, Svratka, Czech Republic
Editors: Jiří Náprstek and Cyril Fischer
Copyright © 2015 Institute of Theoretical and Applied Mechanics, Academy of Sciences of the Czech Republic, v.v.i., Prague
ISBN 978-80-86246-42-0 (printed, Extended Abstracts)
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
list of papers scientific commitee
Wing Geometry Design Using Glauert's Method
T. Koutník
pages 150 - 151, full text
pages 150 - 151, full text
Glauert’s solution of Prandtl’s lifting line theory is a quick method widely used for analysis of the spanwise lift distribution on planar wings. In this article, its use on an inverse problem is demonstrated. The concept is tested by morphing the initial rectangular wing planform to reach demanded lift distribution. Results are compared with theoretical assumptions, solution obtained from CFD simulation and tunnel measurement results.
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Text and facts may be copied and used freely, but credit should be given to these Proceedings.
All papers were reviewed by members of the scientific committee.
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