Articles | Volume 9, issue 6
https://doi.org/10.5194/wes-9-1323-2024
https://doi.org/10.5194/wes-9-1323-2024
Research article
 | 
14 Jun 2024
Research article |  | 14 Jun 2024

Swinging motion of a kite with suspended control unit flying turning manoeuvres

Mark Schelbergen and Roland Schmehl

Viewed

Total article views: 736 (including HTML, PDF, and XML)
HTML PDF XML Total BibTeX EndNote
584 123 29 736 17 12
  • HTML: 584
  • PDF: 123
  • XML: 29
  • Total: 736
  • BibTeX: 17
  • EndNote: 12
Views and downloads (calculated since 19 Sep 2023)
Cumulative views and downloads (calculated since 19 Sep 2023)

Viewed (geographical distribution)

Total article views: 736 (including HTML, PDF, and XML) Thereof 717 with geography defined and 19 with unknown origin.
Country # Views %
  • 1
1
 
 
 
 

Cited

Latest update: 29 Jun 2024
Download
Short summary
We present a novel two-point model of a kite with a suspended control unit to describe the characteristic swinging motion of this assembly during turning manoeuvres. Quasi-steady and dynamic model variants are combined with a discretised tether model, and simulation results are compared with measurement data of an instrumented kite system. By resolving the pitch of the kite, the model allows for computing the angle of attack, which is essential for estimating the generated aerodynamic forces.
Altmetrics
Final-revised paper
Preprint