Wind Energy Science
Wind Energy Science
WES
Articles | Volume 5, issue 3
Articles | Volume 5, issue 3
https://doi.org/10.5194/wes-5-1075-2020
© Author(s) 2020. This work is distributed under
the Creative Commons Attribution 4.0 License.
https://doi.org/10.5194/wes-5-1075-2020
© Author(s) 2020. This work is distributed under
the Creative Commons Attribution 4.0 License.
Articles | Volume 5, issue 3
Research article
 | 
24 Aug 2020
Research article |  | 24 Aug 2020

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

Julia Steiner, Axelle Viré, Francesco Benetti, Nando Timmer, and Richard Dwight

Viewed

Total article views: 3,504 (including HTML, PDF, and XML)
HTML PDF XML Total BibTeX EndNote
2,322 1,068 114 3,504 145 167
  • HTML: 2,322
  • PDF: 1,068
  • XML: 114
  • Total: 3,504
  • BibTeX: 145
  • EndNote: 167
Views and downloads (calculated since 24 Sep 2019)
Cumulative views and downloads (calculated since 24 Sep 2019)

Viewed (geographical distribution)

Total article views: 3,504 (including HTML, PDF, and XML) Thereof 3,005 with geography defined and 499 with unknown origin.
Country # Views %
  • 1
1
 
 
 
 

Cited

Latest update: 02 Nov 2025
Download
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.
Read more
Share
Altmetrics
Final-revised paper
Preprint