10.18710/YW83LN
Yadala, Srikar
Srikar
Yadala
https://orcid.org/0000-0003-1381-9165
NTNU – Norwegian University of Science and Technology
Dehareng, Simon
Simon
Dehareng
https://orcid.org/0000-0002-3787-3118
NTNU – Norwegian University of Science and Technology, University of Liege
Neunaber, Ingrid
Ingrid
Neunaber
https://orcid.org/0000-0002-3787-3118
NTNU – Norwegian University of Science and Technology, KTH Royal Institute of Technology
Jankee, Girish K.
Girish K.
Jankee
https://orcid.org/0000-0002-9178-1070
NTNU – Norwegian University of Science and Technology
Kaufmann, Rene
Rene
Kaufmann
NTNU – Norwegian University of Science and Technology
Couliou, Marie
Marie
Couliou
https://orcid.org/0000-0002-0760-3547
ONERA, Institut Polytechnique de Paris
Hearst, R. Jason
R. Jason
Hearst
https://orcid.org/0000-0003-2002-8644
NTNU – Norwegian University of Science and Technology
Replication Data for: The effect of turbulence on a flexible finite wing: forces, deflections and the wingtip vortex
DataverseNO
2025
Engineering
Physics
Turbulence
NTNU – Norwegian University of Science and Technology
NTNU – Norwegian University of Science and Technology
Hearst, R. Jason
R. Jason
Hearst
NTNU – Norwegian University of Science and Technology
2025-08-05
2025-09-22
10.1017/JFM.2025.10558
10.18710/YW83LN/VRJWQB
10.18710/YW83LN/YZC06F
10.18710/YW83LN/GDHCOG
10.18710/YW83LN/20QTBZ
10.18710/YW83LN/MHZDDW
10.18710/YW83LN/L8SP8X
2534
4913977
6168446124
1450733561
306154467
5782
text/plain
application/zip
application/zip
application/zip
application/zip
text/plain
1.0
Creative Commons CC0 1.0 Universal Public Domain Dedication.
This dataset contains the data required to reproduce the results in the journal article: "The effect of turbulence on a flexible finite wing: forces, deflections and the wingtip vortex". It contains experimental results obtained in the wake of a flexible finite wing, specifically capturing the wing tip vortex, at different turbulent conditions set using an active turbulence grid. The wing tip vortex was captured using cross-stream stereoscopic particle image velocimetry (PIV). Digital Image Correlation (DIC) was employed to study the deformation of the flexible wing under the different turbulent conditions. The performance of the wing (lift and drag) was measured using a force balance. Characterisation of the turbulent freestream generated by the active grid was carried out using hot-wire anemometry (HWA).