E001 - Stiffness and Hinge Release Study (October 2021) (Data underlying the publication: Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads)
Datacite citation style:
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 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/20222334.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite
Dataset
choose version:
version 2 - 2023-05-31 (latest)
version 1 - 2023-05-26
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.
history
- 2023-05-26 first online, published, posted
publisher
4TU.ResearchData
format
.zip file containing .txt data files and .m matlab scripts
organizations
TU Delft, Faculty of Aerospace Engineering, Department of Aerospace Structures and MaterialsTU Delft, Faculty of Aerospace Engineering, Aerodynamics Group
DATA
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- 13,634 bytesMD5:
ebf0b6b26eb4db323d3a95d0d70f3316
README.txt - 747,878,545 bytesMD5:
a6efee117ad12f2f462b961f25710cde
E001_Dataset.zip -
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