Articles | Volume 5, issue 3
Wind Energ. Sci., 5, 1075–1095, 2020
https://doi.org/10.5194/wes-5-1075-2020
Wind Energ. Sci., 5, 1075–1095, 2020
https://doi.org/10.5194/wes-5-1075-2020
Research article
24 Aug 2020
Research article | 24 Aug 2020

Parametric slat design study for thick-base airfoils at high Reynolds numbers

Julia Steiner et al.

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Latest update: 29 Jun 2022
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Short summary
The manuscript deals with the aerodynamic design of slat elements for thick-base airfoils at high Reynolds numbers using integral boundary layer and computational fluid dynamics models. The results highlight aerodynamic benefits such as high stall angle, low roughness sensitivity, and higher aerodynamic efficiency than standard single-element configurations. However, this is accompanied by a steep drop in lift post-stall and potentially issues related to the structural design of the blade.