Supplementary data for the publication: Experimental Aeroelastic Characterization of a Very Flexible Wing in Steady and Unsteady Inflow

doi: 10.4121/17817476.v1
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: 10.4121/17817476
Datacite citation style:
Mertens, Christoph (2022): Supplementary data for the publication: Experimental Aeroelastic Characterization of a Very Flexible Wing in Steady and Unsteady Inflow. Version 1. 4TU.ResearchData. dataset. https://doi.org/10.4121/17817476.v1
Other citation styles (APA, Harvard, MLA, Vancouver, Chicago, IEEE) available at Datacite
Dataset
Delft University of Technology logo
usage stats
1294
views
133
downloads
licence
cc-0.png logo CC0
This data set contains experimentally determined aerodynamic loads and structural deflection measurements of the wind tunnel tests of the Delft-Pazy wing conducted in November 2020. The data is intended to be used for validating numerical aeroelastic models. An example FEM model is provided. More information can be found in the linked publication: Experimental Aeroelastic Characterization of a Very Flexible Wing in Steady and Unsteady Inflow (SciTech 2022 conference)
history
  • 2022-01-05 first online, published, posted
publisher
4TU.ResearchData
format
.dat; .txt
organizations
TU Delft, Faculty of Aerospace Engineering, Department of Aerodynamics, Wind Energy, Flight Performance & Propulsion (AWEP)

DATA

files (1)