The doi 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: 10.4121/20222334

Carrillo Córcoles, Xavier; Mertens, Christoph; Andrea Sciacchitano; van Oudheusden, B.W. (Bas); de Breuker, Roeland et. al. (2023): E001 - Stiffness and Hinge Release Study (October 2021) (Data underlying the publication: Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads). Version 2. 4TU.ResearchData. dataset. https://doi.org/10.4121/20222334.v2

Dataset

x choose version: version 1 - 2023-05-26

• Aerospace Engineering
• Engineering

aeroelasticity, flared folding wingtips, Gust load alleviation, wind tunnel tests

CC BY 4.0

• Flared Folding Wingtips - TU Delft

RefWorks, BibTeX, Reference Manager, Endnote, DataCite, NLM, DC, CFF

by Xavier Carrillo Córcoles , Christoph Mertens , Andrea Sciacchitano , B.W. (Bas) van Oudheusden , Roeland de Breuker , Jurij Sodja

Data set from an aeroelastic wind tunnel study. Five wings with flared folding wingtip, featuring different stiffness properties, are tested in static and dynamic conditions (1-cosine gusts) to assess their gust load alleviation capabilities.

The dataset includes:

• Static measurements: 10 seconds (for statistical evaluation) at different angles of attack (AoA) in both free-hinge and locked-hinge conditions.
• Dynamic measurements: measurements for 1-cosine gusts at different AoA, gust frequency and hinge release thresholds.
• Matlab scripts to read and process the raw data.

• 2023-05-26 first online

• 2023-05-31 published, posted

4TU.ResearchData

.zip file containing .txt data files and .m matlab scripts

Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads

TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures and Materials
TU Delft, Faculty of Aerospace Engineering, Aerodynamics Group