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

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

Dataset

• Aerospace Engineering

Aeroelasticity, Experimental FSI, Wind Tunnel Measurements

CC0

• Delft-Pazy Wing Data Archive

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

by Christoph Mertens

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)

• 2022-01-05 first online, published, posted

4TU.ResearchData

.dat; .txt

Experimental Aeroelastic Characterization of a Very Flexible Wing in Steady and Unsteady Inflow

TU Delft, Faculty of Aerospace Engineering, Department of Aerodynamics, Wind Energy, Flight Performance & Propulsion (AWEP)