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

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posted on 05.01.2022, 07:47 by Christoph MertensChristoph 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)

History

Publisher

4TU.ResearchData

Format

.dat; .txt

Organizations

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