Research output per year
Research output per year
Description
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.
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.
| Date made available | 26 May 2023 |
|---|---|
| Publisher | TU Delft - 4TU.ResearchData |
| Date of data production | 2023 - |
Research output
- 1 Article
-
Effect of Wing Stiffness and Folding Wingtip Release Threshold on Gust Loads
Carrillo Córcoles, X., Mertens, C., Sciacchitano, A., van Oudheusden, B. W., De Breuker, R. & Sodja, J., 2023, (E-pub ahead of print) In: Journal of Aircraft. 60, 6, p. 1917-1936 20 p.Research output: Contribution to journal › Article › Scientific › peer-review
Open AccessFile2 Citations (Scopus)117 Downloads (Pure)