Proceedings Vol. 21 (2015)
ENGINEERING MECHANICS 2015
May 11 – 14, 2015, Svratka, Czech Republic
Copyright © 2015 Institute of Theoretical and Applied Mechanics, Academy of Sciences of the Czech Republic, v.v.i., Prague
ISSN 1805-8248 (printed)
ISSN 1805-8256 (electronic)
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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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