Supporting data belonging to publication: "Lift-Induced Wake Re-Energization for a VAWT-Based Multi-Rotor System"

DOI:10.4121/24529850-7f34-42b6-9f29-fcc1577bb1ae.v1
The DOI displayed above is for this specific version of this dataset, which is currently the latest. Newer versions may be published in the future. For a link that will always point to the latest version, please use
DOI: 10.4121/24529850-7f34-42b6-9f29-fcc1577bb1ae

Datacite citation style

Bensason, David; Broertjes, Thomas; Andrea Sciacchitano; Simao Ferreira, Carlos (2025): Supporting data belonging to publication: "Lift-Induced Wake Re-Energization for a VAWT-Based Multi-Rotor System". Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/24529850-7f34-42b6-9f29-fcc1577bb1ae.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite

Dataset

Delft University of Technology logo

Geolocation

Open-jet wind tunnel facility (OJF), Delft, The Netherlands

Time coverage

2024

Licence

CC BY 4.0

Interoperability

This dataset is intended to support the publication "Lift-Induced Wake Re-Energization for a VAWT-Based Multi-Rotor System" by Broertjes, Bensason, Sciacchitano, and Ferreira, published in the Journal of Physics: Conference series under DOI 10.1088/1742-6596/2767/7/072012 . The data includes the measured wake at four cross-steam planes downstream of a lab-scaled VAWT-based multirotor system. The wake was measured using a thick laser sheet coupled with particle-tracking velocimetry in TU Delft's Open-Jet Facility (OJF). The purpose of this study is to evaluate the impact of a de-coupled wake recovery strategy for MRS using high-lifting wings. Hence, the wake was measured for two cases, namely, the baseline (where no steering is applied) and with wings (where wings are mounted on the MRS to steer the wake). The README.m file should be used to understand the data structure and shared CAD files. The results provide an experimental proof-of-concept of high-lifting wings for enhanced wake recovery of a multi-rotor system and a database for future and ongoing numerical model development.

History

  • 2025-03-17 first online, published, posted

Publisher

4TU.ResearchData

Format

.mat (MATLAB structures), .m (MATLAB script), .ipt (part file in CAD), .iam (assembly file in CAD)

Funding

  • Horizon 2020 (grant code 101007135) European Union's Horizon 2020 research and innovation program

Organizations

TU Delft, Faculty of Aerospace Engineering, Department of Flow Physics and Technology

DATA

Files (3)